145 Commits
Author SHA1 Message Date
Oleg Kalachev 142cb9af01 Position control draft 2026-08-01 20:13:48 +03:00
Oleg Kalachev 74b082957e Add threshold for rc sticks move for quitting auto mode 2026-07-21 10:58:22 +03:00
Oleg Kalachev 4582942919 Minor docs update 2026-07-21 10:51:50 +03:00
Oleg Kalachev df14a5678f Don't send discovery message if encrypting is disabled in espnow 2026-07-20 19:01:38 +03:00
Oleg Kalachev 81721abf91 Disable log as it may crash the program 2026-07-20 10:16:30 +03:00
Oleg Kalachev 1276d220a6 Add tilt disarm failsafe 2026-07-18 21:35:13 +03:00
Oleg Kalachev 79c7e282cb Fix esp-now proxy 2026-07-18 14:25:19 +03:00
Oleg Kalachev f031cf3046 Fix printing espnow channel number in wifi command 2026-07-18 14:16:33 +03:00
Oleg Kalachev 60f389a289 Fix espnow proxy 2026-07-18 11:35:20 +03:00
Oleg Kalachev 5c24ce113d Minor docs update 2026-07-18 00:45:19 +03:00
Oleg Kalachev b58c2e7c7a Add auto channel search to espnow-proxy 2026-07-18 00:03:18 +03:00
Oleg Kalachev 2137730a8d Make espnow-proxy output more obvious 2026-07-18 00:03:01 +03:00
Oleg Kalachev 309d2d2e29 Add espnow-proxy build to ci 2026-07-17 23:42:28 +03:00
Oleg Kalachev 0c91ccfab5 Use STA interface in ESP-NOW proxy 2026-07-17 23:39:21 +03:00
Oleg Kalachev 26d53d4ce1 Docs fix 2026-07-17 17:18:07 +03:00
Oleg Kalachev 0366b24ff3 Minor docs fix 2026-07-17 17:06:22 +03:00
Oleg Kalachev 3de4e9ab9a Add info on uploading the firmware to ESP32-S3 Super Mini 2026-07-17 17:04:45 +03:00
Oleg Kalachev f1e024b19a Add instructions on how to set pin numbers for imu 2026-07-17 14:13:02 +03:00
Oleg Kalachev d9be26c5be Disable gyro notch filter by default 2026-07-16 23:21:17 +03:00
Oleg Kalachev f8a4cbfee1 Fix in docs 2026-07-16 17:48:16 +03:00
Oleg Kalachev 658040e652 Merge branch 'master' into robolager2026 2026-07-16 16:54:47 +03:00
Oleg Kalachev 70459df8dd Disable swarming in espnow proxy by default 2026-07-16 11:30:10 +03:00
Oleg Kalachev 61213bb8a1 Unset default motor pins (for safety) 2026-07-15 20:19:02 +03:00
Oleg Kalachev d48b71fb1a Disable voltage lpf by default
(Setting alpha = 1 efficiently disables the filter.)
Filtering does more harm than good in voltage monitoring.
2026-07-15 18:42:34 +03:00
Oleg Kalachev 8917849711 Remove unneeded declaration from the sim 2026-07-15 18:40:51 +03:00
Oleg Kalachev 1cdc7a8641 Fix rc in simulator
Virtual rc is disabled if rxRxPin < 0
2026-07-15 18:40:35 +03:00
Oleg Kalachev 0439407d76 Remove unneeded declaration from the sim 2026-07-15 18:29:36 +03:00
Oleg Kalachev c2005a2ca2 Fix rc in simulator 2026-07-15 17:40:11 +03:00
Oleg Kalachev 6a804862da Fix simulator build with new logging 2026-07-15 14:17:24 +03:00
Oleg Kalachev 590bfe10b0 Minor doc changes 2026-07-15 10:52:52 +03:00
Oleg Kalachev 70af1a1c09 Remove DebugLevel from fqbn in usage article 2026-07-15 10:38:04 +03:00
Oleg Kalachev 9e9dafbdfb Support feed forward rates in mavlink control 2026-07-15 10:11:15 +03:00
Oleg Kalachev 86a4418813 Move debug level definition from fbqn to arduino-cli commaand 2026-07-13 22:05:31 +03:00
Oleg Kalachev d64bf24c6d Add alicanerus' build 2026-07-08 22:29:33 +03:00
Oleg Kalachev 7c53e88963 Add notch filter for the gyro 2026-07-08 16:07:03 +03:00
Oleg Kalachev 28f015569b Add log reset command to cli 2026-07-08 01:07:59 +03:00
Oleg Kalachev fabd5e072d Fixes in the docs 2026-07-04 21:40:39 +03:00
Oleg Kalachev 1ae85ff118 Add argument to motor testing commands for specifying thrust 2026-07-02 22:22:33 +03:00
Oleg Kalachev 83d1c5c68a Implement entirely new logging subsystem
Make topic-based logging mechanics.
Print any log value to console.
Possibility to expose any logging value to mavlink.
2026-06-30 13:03:43 +03:00
Oleg Kalachev 26a0dd65be Minor fixes and updates 2026-06-30 12:19:29 +03:00
Oleg Kalachev 9d439afd80 Store only changed parameters in flash instead of all
Rationale:
1. Parameters NVS storage is limited and storing unchanged parameters is wasteful.
2. This allows changing parameters in the code without having to erase the flash storage.
3. Updating the firmware version may change the parameter defaults.
2026-06-28 17:21:07 +03:00
Oleg Kalachev 64b21a3a6b Show default parameter values in p command output
Also move float comparing logic to a distinct util function.
2026-06-24 06:42:09 +03:00
Oleg Kalachev 545eed8944 Add Nerush and Konstantinos Paraskevas builds 2026-06-19 05:15:17 +03:00
Oleg Kalachev 518abf1555 Simplify rc code
Utilize the new method for getting channel values.
2026-06-14 04:45:42 +03:00
Oleg Kalachev 17df1c5396 Separate repository vscode settings and local vscode settings
Use dangmai.workspace-default-settings externsion for that.
2026-06-11 20:37:35 +03:00
Oleg Kalachev 8e2ffd7c69 Remove core installation when running the sim
Split `dependencies` target to `core` and `libs` targets.
Move additional urls declaration and connection timeout from arduino-cli.yaml to Makefile for simplicity and transparency.
Update ESP32 core url.
Remove arduino-cli.yaml.
2026-06-10 18:10:42 +03:00
Oleg Kalachev 52b74afba6 Bring back espnow tx buffering keeping resends disabled
Buffering is needed for sending large prints, otherwise the espnow internal buffer overflows.
Make onSent always think there was success send, so there won't be any resends.
Print lost espnow packets count on wifi console command.
2026-06-09 03:23:30 +03:00
Oleg Kalachev 0ca2473655 Make each mavlink message rate configured separately
Add parameters:
* MAV_RATE_ATT - ATTITUDE_QUATERNION rate.
* MAV_RATE_RC - RC_CHANNELS_RAW rate.
* MAV_RATE_MOT - ACTUATOR_CONTROL_TARGET rate.
* MAV_RATE_IMU - SCALED_IMU rate.
2026-06-09 02:59:10 +03:00
Oleg Kalachev b4c2fe3988 Print total RAM in sys command 2026-06-09 02:49:39 +03:00
Oleg Kalachev e51b47b798 Add command for setting the wifi mode easier 2026-06-09 02:44:09 +03:00
Oleg Kalachev 71abe1bcdb Minor changes
Simplify the code, print imu temperature
2026-06-09 02:25:20 +03:00
Oleg Kalachev 0f2e384ce6 Don't apply level correction on idle thrust 2026-06-09 02:12:27 +03:00
Oleg Kalachev 5e153a210d Update ESP32-Core to 3.3.10 2026-06-09 02:05:52 +03:00
Oleg Kalachev 9d47bcb82e Minor changes in docs 2026-05-31 18:10:00 +03:00
Oleg Kalachev 1fafc27b39 Make it possible to unassign motor pin using -1 parameter value 2026-05-30 16:57:27 +03:00
Oleg Kalachev faca48ced3 Replace ps and psq commands with st command + minor changes
Re-arrange commands order.
Make command parser consider \r in addition to \n.
2026-05-30 16:51:15 +03:00
Oleg Kalachev a5dbd2c829 Add erase command to makefile 2026-05-30 16:48:12 +03:00
Oleg Kalachev 59f9528d34 Increase buffer for print, make sys output more correct
usStackHighWaterMark is not stack size, it's the minimum stack size
2026-05-30 11:11:35 +03:00
Oleg Kalachev 607b2ff0b7 Add malagis custom pcb version of Flix project to builds 2026-05-28 20:15:09 +03:00
Oleg Kalachev 22c06f76c4 Add Awab Anas' build 2026-05-28 19:29:05 +03:00
Oleg Kalachev 488ceb3004 Set the debug level to error by default to see the errors 2026-05-28 19:25:29 +03:00
Oleg Kalachev b83c9b3845 Consider mavlink connected only when the gcs message is parsed 2026-05-28 18:41:34 +03:00
Oleg Kalachev 2f4b1423e6 Typo and minor code style changes 2026-05-28 18:39:44 +03:00
Oleg Kalachev 4e32414dae Support ESP-NOW connection in pyflix
Set arbitrary pymavlink connection string using device parameter or FLIX_DEVICE env variable.
pyflix@0.16.
2026-05-28 18:22:16 +03:00
Oleg Kalachev a294883dea Make p command show all parameters starting with the arg 2026-05-27 13:58:51 +03:00
Oleg Kalachev cdfba72a0b Fix simulator run
Add missing extern variables.
Fix warning.
2026-05-27 11:03:50 +03:00
Oleg Kalachev 18e81720e0 Add video of pcb version flights to the readme 2026-05-26 14:23:56 +03:00
Oleg Kalachev 91173d06c9 Various minor changes 2026-05-22 08:03:46 +03:00
Oleg KalachevandGitHub fdcc9533b3 Implement ESP-NOW support (#40) 2026-05-21 10:48:31 +03:00
Oleg Kalachev bd2b1bd5de Improve voltage measurement
Apply PWM_VOLT_PIN without reboot.
Check if the voltage pin can be used with ADC when setting up.
Set voltage to NAN, when it's unknown (including pyflix).
pyflix@0.15.
Don't send BATTERY_STATUS when voltage is unknown.
Add dummy voltage to the simulator.
2026-05-18 00:30:42 +03:00
Oleg Kalachev 4530c05b5c Add Flix 1.5 to builds 2026-05-17 06:46:11 +03:00
Oleg Kalachev 3816ae376f Bring back initializing the lpf with the first input value
It's much better for voltage measuring and slightly better for gyro bias estimation.
2026-05-17 06:21:13 +03:00
Oleg Kalachev 72a72fde80 Some docs improvements 2026-05-14 21:59:15 +03:00
Oleg Kalachev e53051a349 Fix console command parsing 2026-05-13 06:00:51 +03:00
Oleg Kalachev f8a9f1f838 Remove reboot requirement when changing RC_RX_PIN 2026-05-13 01:27:01 +03:00
Oleg Kalachev 76af83fc88 Improve firmware overview article 2026-05-13 00:35:43 +03:00
Oleg Kalachev dd176180a7 Update help message
Remove 'welcome to', add copyright and repo link.
2026-05-12 17:50:28 +03:00
Oleg Kalachev 48c33c7050 Fix and improve wifi subsystem
Fix a fault when wifi is disabled (udp can't be used without wifi).
Print RSSI and channel in wifi command.
2026-05-10 22:39:34 +03:00
Oleg Kalachev 35e94f6ea6 Support ESP32-C3
User Serial1 for rc instead of Serial2, as ESP32-C3 has only 2 Serials.
Add CI build for ESP32-C3.
2026-05-10 21:07:20 +03:00
Oleg Kalachev 1f48e379e3 Improve the rc calibration code
More convenient steps order.
Improve the readability a bit.
2026-05-10 19:05:27 +03:00
Oleg Kalachev ee3c6999ab Add mavlink joystick app usage to the docs 2026-05-10 14:50:27 +03:00
Oleg Kalachev 34c6993842 Some fixes in the docs 2026-05-10 02:33:03 +03:00
Oleg Kalachev b62f2f9427 Rename some wifi parameters for better alphabetical sort 2026-05-09 17:55:55 +03:00
Oleg KalachevandMarina Tikhomirova 7dfef17165 Add Ina Tix' build
Co-authored-by: Marina Tikhomirova <Ina.tix@yandex.ru>
2026-05-09 17:49:59 +03:00
Oleg Kalachev 8c8046676b Simplify port definition in Makefile 2026-05-09 17:14:29 +03:00
Oleg Kalachev 702ec9792e Some updates in troubleshooting article 2026-05-09 15:57:25 +03:00
Oleg Kalachev 06e2047097 Make motor testing signal 0.2 instead of full power
Testing with full power is too dangerous and inconvenient.
2026-05-08 00:53:19 +03:00
Oleg Kalachev 87480476c2 Fix motors pwm frequency for esp32s3 etc in the docs 2026-05-08 00:47:29 +03:00
Oleg Kalachev 68271c508c Print firmware build date and time in sys command 2026-05-08 00:31:51 +03:00
Oleg Kalachev e81e84e7fc Some updates to docs 2026-05-07 20:15:55 +03:00
Oleg Kalachev 5f1a938d4f Fix imu rotation definition
The X axis should be pointing to the mounting holes, not pins side.
2026-05-07 19:54:16 +03:00
Oleg Kalachev bd270db493 Reduce angle drift by adding level correction to the estimator
Leverage a priori knowledge that the drone's average attitude is level.
Explanation: https://t.me/opensourcequadcopter/158.
2026-05-05 21:27:47 +03:00
Oleg Kalachev dbf24ea611 Expose lpf alpha of rate pids to parameters
Add parameters: CTL_R_RATE_D_A, CTL_P_RATE_D_A, CTL_Y_RATE_D_A.
2026-05-03 15:04:16 +03:00
Oleg Kalachev 08683d696d Some updates in the usage doc 2026-05-01 15:26:59 +03:00
Oleg Kalachev 9ca6841558 Exit auto mode when sticks moved only when mode switch is not configured 2026-04-29 15:07:44 +03:00
Oleg Kalachev 28da2d3c8e Fix in pyflix documentation
pyflix@0.14
2026-04-28 20:46:49 +03:00
Oleg Kalachev c6632ae6e4 Add info on setting flight modes using rc mode switch 2026-04-28 20:43:52 +03:00
Oleg Kalachev 35ca754583 Fix Vector::rotationVectorBetween implementation for parallel vectors 2026-04-28 15:38:52 +03:00
Oleg Kalachev 2ccda03573 Implement motors output desaturation
So the drone continues stabilization on max thrust.
2026-04-28 13:23:42 +03:00
Oleg Kalachev 485a39e740 Disable wi-fi power save to improve responsiveness 2026-04-27 16:46:36 +03:00
Oleg Kalachev 9bffe5b52f Some fixes in docs 2026-04-26 06:05:02 +03:00
Oleg Kalachev d6a79d6c66 Pass acc data in mG in SCALED_IMU to comply with mavlink standard
https://mavlink.io/en/messages/common.html#SCALED_IMU
pyflix@0.13
2026-04-24 07:42:39 +03:00
Oleg Kalachev 350a82bfed Minor fix 2026-04-23 15:34:54 +03:00
Oleg Kalachev 6e439859bc Move disabling brown-out code to power subsystem 2026-04-23 15:06:07 +03:00
Oleg Kalachev 835b2243e8 Minor fix in sys command
String works with printf %s, but actually it's a UB.
2026-04-23 07:25:59 +03:00
Oleg Kalachev ed4e2d87d1 Fix imu command output
Gyro field contained filtered gyro instead of scaled only gyro.
2026-04-23 07:12:25 +03:00
Oleg Kalachev 51cd5fc691 Implement battery voltage monitoring
Add power subsystem.
Add PWR_VOLT_PIN, PWR_VOLT_SCALE, PWR_VOLT_LPF_A parameters.
Support BATTERY_STATUS mavlink messages streaming.
Add pw cli command.
Add voltage field to pyflix library.
pyflix@0.12.
2026-04-22 11:35:37 +03:00
Oleg Kalachev d8591ea2a9 Fix working with parameters in pyflix examples
PITCH_P parameter was renamed to CTL_P_P
2026-04-18 05:23:47 +03:00
Oleg Kalachev c434107eaf Add parameter for configuring sbus pin number, disable sbus by default 2026-03-27 00:56:34 +03:00
Oleg Kalachev 814427dbfd Minor docs change 2026-03-27 00:40:19 +03:00
Oleg Kalachev 0730ceeffa Add new user builds 2026-02-21 07:12:36 +03:00
Oleg Kalachev a687303062 Make motor parameters apply without reboot
Add callback to parameter definition to call after parameter is changed.
2026-02-19 04:56:12 +03:00
Oleg Kalachev b2daf2587f Minor parameters code simplifications
readOnly is false by default
INFINITY == INFINITY, so remove redundant check
2026-02-19 02:59:38 +03:00
Oleg Kalachev a8c25d8ac0 Minor updates to usage article 2026-02-04 17:52:23 +03:00
Oleg Kalachev 3e49d41986 Make rc channel numbers and calibration params use int instead of float
As parameter subsystems supports int now, and int is much more natural here.
2026-02-02 20:36:22 +03:00
Oleg Kalachev 67430c7aac Several minor changes 2026-02-02 18:46:36 +03:00
Oleg Kalachev 3631743a29 Drop messages from another systems in pyflix
We shouldn't pass messages where system id != our system id. 
This change may be useful when there are many drones in one network.
2026-02-02 18:28:20 +03:00
Oleg Kalachev 3dde380bb7 Add parameters for list of modes bound to rc switch
Parameters: CTL_FLT_MODE_0, CTL_FLT_MODE_1, CTL_FLT_MODE_2.
Also fix a bug with incorrect choosing the mode from controlMode.
2026-01-27 16:38:20 +03:00
Oleg Kalachev 377b21429b Fix error when launching the sim
Also make the parameters WIFI_LOC_PORT and WIFI_REM_PORT work in the sim.
2026-01-27 16:32:52 +03:00
Oleg Kalachev 1ac443d6f8 Add a build by Arky Matsekh 2026-01-27 15:17:58 +03:00
Oleg Kalachev 964c0f7bc1 Make setting parameter in console printing actual parameter value.
In some cases, it would not be equal to the requested value.
2026-01-27 09:28:01 +03:00
Oleg Kalachev 40bdaacedb Make motor subsystem configurable using parameters
Motor pins: MOT_PIN_FL, MOT_PIN_FR, MOT_PIN_RL, MOT_PIN_RR.
PWM configuration: MOT_PWM_FREQ, MOT_PWM_RES, MOT_PWM_STOP, MOT_PWM_MIN, MOT_PWM_MAX.
MOT_PWM_MAX = -1 chooses duty cycle mode for brushed motors (default).
2026-01-27 08:40:52 +03:00
Oleg Kalachev 7d74f3d5cd Minor docs fixes 2026-01-27 07:21:21 +03:00
Oleg Kalachev 9fd35ba361 Simplify lpf filter code
Begin with zero instead of the initializing value, as the latter doesn't make much sense in practice, but complicates the code much.
2026-01-24 09:43:46 +03:00
Oleg Kalachev ca50f75576 Various minor fixes 2026-01-24 09:34:16 +03:00
Oleg Kalachev e47a31f981 Fix mavlink parameter set acknowledgement value
If the parameter is integer the acknowledgement should contain the rounded value.
2026-01-24 09:32:49 +03:00
Oleg Kalachev 7ad3022798 Add parameter for configuring gyro bias lpf
+ reset the filter on `reset` command
2026-01-24 09:31:32 +03:00
Oleg Kalachev 5b654e4d8e Update ESP32-Core to 3.3.6 2026-01-23 02:41:43 +03:00
Oleg Kalachev cf10ec6161 Update MAVLink-Arduino to 2.0.16 2026-01-23 01:11:35 +03:00
Oleg Kalachev 6d01cd2e79 Make failsafe configurable using parameters
SF_RC_LOSS_TIME - time without rc to activate failsafe.
SD_DESCEND_TIME - total time to decrease the throttle to zero.
Make controlTime nan on the start to simplify the logic.
2026-01-22 23:57:52 +03:00
Oleg Kalachev 0abb18c616 Make parameter names case-insensitive
+ minor fix
2026-01-22 23:11:47 +03:00
Oleg Kalachev 30326a5662 Add parameters for configuring the mavlink subsystem
MAV_SYS_ID - mavlink system id.
MAV_RATE_SLOW - rate of slow telemetry (e. g. heartbeats).
MAV_RATE_FAST - rate of fast telemetry (e. g. attitude, imu data).
2026-01-22 23:04:45 +03:00
Oleg Kalachev dd3575174b Add wifi configuration using parameters and cli
Add console commands to setup wifi.
Add a parameter for choosing between STA and AP mode.
Add parameters for udp ports.
Remove WIFI_ENABLED macro.
2026-01-22 22:58:43 +03:00
Oleg Kalachev c0f3301da4 Support integer parameters in addition to floats
The variable pointer is stored as a union field.
If `.integer` field is true, then integer pointer should be used.
Interfaces to parameters (cli and mavlink) keep working using floats.
Setting a non-finite value to int parameter will cause an error.
`.value` field is renamed to `.cache`.
2026-01-22 22:54:05 +03:00
a.golubtsovandOleg Kalachev a6bad3a69b Add log dir creation before log writing 2026-01-22 17:56:23 +03:00
Oleg Kalachev 9a9bd07251 Add correct attitude estimation video to the usage article 2026-01-15 23:46:23 +03:00
Oleg Kalachev 28f5855a57 Re-arrange control.ino declarations to make a bit more sensible
So the control command is above the PID controllers.
2026-01-13 17:43:53 +03:00
Oleg Kalachev 7e24ee30f7 Documentation and book updates
Improve the main list of features.
Use lowercase imu variable for consistency with the firmware code.
Minor fixes.
2026-01-13 17:26:40 +03:00
Oleg Kalachev 2a8faf5759 Fix logo svg slightly 2026-01-08 19:45:08 +03:00
Oleg Kalachev f4e58a652a Add project logo 2026-01-08 17:58:59 +03:00
Oleg Kalachev 6c46328da1 Minor doc fixes 2026-01-04 15:01:53 +03:00
Oleg Kalachev c8e5e08b03 Move all global variable declarations to the appropriate subsystems
As it makes the subsystems code easier to understand.
Declare the most used variables in main sketch file as forward declarations.
Make all control input zero by default (except controlMode).
Minor changes.
2026-01-03 13:28:18 +03:00
Oleg Kalachev a5e3dfcf69 Some updates to the docs 2026-01-03 12:18:47 +03:00
Oleg Kalachev d6e8be0c05 Add parameters for easier IMU orientation definition 2025-12-26 21:14:15 +03:00
Oleg Kalachev 68d16855df Add motors rotation diagram to usage article 2025-12-25 07:22:09 +03:00
81 changed files with 2042 additions and 628 deletions
+4 -2
View File
@@ -23,10 +23,12 @@ jobs:
with:
name: firmware-binary
path: flix/build
- name: Build firmware for ESP32-C3
run: make BOARD=esp32:esp32:esp32c3
- name: Build firmware for ESP32-S3
run: make BOARD=esp32:esp32:esp32s3
- name: Build firmware with WiFi disabled
run: sed -i 's/^#define WIFI_ENABLED 1$/#define WIFI_ENABLED 0/' flix/flix.ino && make
- name: Build espnow-proxy
run: arduino-cli compile --fqbn esp32:esp32:esp32 tools/espnow-proxy
- name: Check c_cpp_properties.json
run: tools/check_c_cpp_properties.py
+3 -2
View File
@@ -4,9 +4,10 @@ build/
tools/log/
tools/dist/
*.egg-info/
.dependencies
.core
.libs
.vscode/*
!.vscode/settings.json
!.vscode/settings.default.json
!.vscode/c_cpp_properties.json
!.vscode/tasks.json
!.vscode/launch.json
+1
View File
@@ -7,6 +7,7 @@
"MD024": false,
"MD033": false,
"MD034": false,
"MD040": false,
"MD059": false,
"MD044": {
"html_elements": false,
+27 -27
View File
@@ -6,19 +6,18 @@
"${workspaceFolder}/flix",
"${workspaceFolder}/gazebo",
"${workspaceFolder}/tools/**",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/**",
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
"~/.arduino15/packages/esp32/hardware/esp32/3.3.10/cores/esp32",
"~/.arduino15/packages/esp32/hardware/esp32/3.3.10/libraries/**",
"~/.arduino15/packages/esp32/hardware/esp32/3.3.10/variants/d1_mini32",
"~/.arduino15/packages/esp32/tools/esp32-libs/3.3.10/include/**",
"~/Arduino/libraries/**",
"/usr/include/gazebo-11/",
"/usr/include/ignition/math6/"
],
"forcedInclude": [
"${workspaceFolder}/.vscode/intellisense.h",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
"~/.arduino15/packages/esp32/hardware/esp32/3.3.10/cores/esp32/Arduino.h",
"~/.arduino15/packages/esp32/hardware/esp32/3.3.10/variants/d1_mini32/pins_arduino.h",
"${workspaceFolder}/flix/cli.ino",
"${workspaceFolder}/flix/control.ino",
"${workspaceFolder}/flix/estimate.ino",
@@ -31,9 +30,10 @@
"${workspaceFolder}/flix/rc.ino",
"${workspaceFolder}/flix/time.ino",
"${workspaceFolder}/flix/wifi.ino",
"${workspaceFolder}/flix/parameters.ino"
"${workspaceFolder}/flix/parameters.ino",
"${workspaceFolder}/flix/safety.ino"
],
"compilerPath": "~/.arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++",
"compilerPath": "~/.arduino15/packages/esp32/tools/esp-x32/2601/bin/xtensa-esp32-elf-g++",
"cStandard": "c11",
"cppStandard": "c++17",
"defines": [
@@ -53,19 +53,18 @@
"name": "Mac",
"includePath": [
"${workspaceFolder}/flix",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
"~/Library/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/include/**",
"~/Library/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.10/cores/esp32",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.10/libraries/**",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.10/variants/d1_mini32",
"~/Library/Arduino15/packages/esp32/tools/esp32-libs/3.3.10/include/**",
"~/Documents/Arduino/libraries/**",
"/opt/homebrew/include/gazebo-11/",
"/opt/homebrew/include/ignition/math6/"
],
"forcedInclude": [
"${workspaceFolder}/.vscode/intellisense.h",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.10/cores/esp32/Arduino.h",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.10/variants/d1_mini32/pins_arduino.h",
"${workspaceFolder}/flix/flix.ino",
"${workspaceFolder}/flix/cli.ino",
"${workspaceFolder}/flix/control.ino",
@@ -78,9 +77,10 @@
"${workspaceFolder}/flix/rc.ino",
"${workspaceFolder}/flix/time.ino",
"${workspaceFolder}/flix/wifi.ino",
"${workspaceFolder}/flix/parameters.ino"
"${workspaceFolder}/flix/parameters.ino",
"${workspaceFolder}/flix/safety.ino"
],
"compilerPath": "~/Library/Arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++",
"compilerPath": "~/Library/Arduino15/packages/esp32/tools/esp-x32/2601/bin/xtensa-esp32-elf-g++",
"cStandard": "c11",
"cppStandard": "c++17",
"defines": [
@@ -103,17 +103,16 @@
"${workspaceFolder}/flix",
"${workspaceFolder}/gazebo",
"${workspaceFolder}/tools/**",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
"~/AppData/Local/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/**",
"~/AppData/Local/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.10/cores/esp32",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.10/libraries/**",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.10/variants/d1_mini32",
"~/AppData/Local/Arduino15/packages/esp32/tools/esp32-libs/3.3.10/include/**",
"~/Documents/Arduino/libraries/**"
],
"forcedInclude": [
"${workspaceFolder}/.vscode/intellisense.h",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.10/cores/esp32/Arduino.h",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.10/variants/d1_mini32/pins_arduino.h",
"${workspaceFolder}/flix/cli.ino",
"${workspaceFolder}/flix/control.ino",
"${workspaceFolder}/flix/estimate.ino",
@@ -126,9 +125,10 @@
"${workspaceFolder}/flix/rc.ino",
"${workspaceFolder}/flix/time.ino",
"${workspaceFolder}/flix/wifi.ino",
"${workspaceFolder}/flix/parameters.ino"
"${workspaceFolder}/flix/parameters.ino",
"${workspaceFolder}/flix/safety.ino"
],
"compilerPath": "~/AppData/Local/Arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++.exe",
"compilerPath": "~/AppData/Local/Arduino15/packages/esp32/tools/esp-x32/2601/bin/xtensa-esp32-elf-g++.exe",
"cStandard": "c11",
"cppStandard": "c++17",
"defines": [
+1
View File
@@ -1,6 +1,7 @@
{
// See https://go.microsoft.com/fwlink/?LinkId=827846 to learn about workspace recommendations.
"recommendations": [
"dangmai.workspace-default-settings",
"ms-vscode.cpptools",
"ms-vscode.cmake-tools",
"ms-python.python"
+23 -12
View File
@@ -1,29 +1,40 @@
BOARD = esp32:esp32:d1_mini32
PORT := $(wildcard /dev/serial/by-id/usb-Silicon_Labs_CP21* /dev/serial/by-id/usb-1a86_USB_Single_Serial_* /dev/cu.usbserial-*)
PORT := $(strip $(PORT))
PORT := $(strip $(wildcard /dev/serial/by-id/usb-Silicon_Labs_CP21* /dev/serial/by-id/usb-1a86_USB_Single_Serial_* /dev/cu.usbserial-* /dev/cu.usbmodem*))
build: .dependencies
arduino-cli compile --fqbn $(BOARD) flix
export ARDUINO_NETWORK_CONNECTION_TIMEOUT := 1h
build: .core .libs
arduino-cli compile --fqbn $(BOARD) --build-property "build.core_debug_level=1" flix
upload: build
arduino-cli upload --fqbn $(BOARD) -p "$(PORT)" flix
erase:
arduino-cli burn-bootloader --fqbn $(BOARD) -p "$(PORT)" -P esptool
monitor:
arduino-cli monitor -p "$(PORT)" -c baudrate=115200
dependencies .dependencies:
arduino-cli core update-index --config-file arduino-cli.yaml
arduino-cli core install esp32:esp32@3.2.0 --config-file arduino-cli.yaml
core .core:
arduino-cli core update-index --additional-urls https://espressif.github.io/arduino-esp32/package_esp32_index.json
arduino-cli core install esp32:esp32@3.3.10 --additional-urls https://espressif.github.io/arduino-esp32/package_esp32_index.json
touch .core
libs .libs:
arduino-cli lib update-index
arduino-cli lib install "FlixPeriph"
arduino-cli lib install "MAVLink"@2.0.16
touch .dependencies
arduino-cli lib install "MAVLink"@2.0.25
touch .libs
upload_proxy: .core .libs
arduino-cli compile --fqbn $(BOARD) tools/espnow-proxy
arduino-cli upload --fqbn $(BOARD) -p "$(PORT)" tools/espnow-proxy
gazebo/build cmake: gazebo/CMakeLists.txt
mkdir -p gazebo/build
cd gazebo/build && cmake ..
build_simulator: .dependencies gazebo/build
build_simulator: .libs gazebo/build
make -C gazebo/build
simulator: build_simulator
@@ -38,6 +49,6 @@ plot:
plotjuggler -d $(shell ls -t tools/log/*.csv | head -n1)
clean:
rm -rf gazebo/build flix/build flix/cache .dependencies
rm -rf gazebo/build flix/build flix/cache .core .libs
.PHONY: build upload monitor dependencies cmake build_simulator simulator log clean
.PHONY: build upload monitor core libs cmake build_simulator simulator log clean
+34 -23
View File
@@ -1,6 +1,9 @@
# Flix
<!-- markdownlint-disable MD041 -->
**Flix** (*flight + X*) — open source ESP32-based quadcopter made from scratch.
<p align="center">
<img src="docs/img/flix.svg" width=180 alt="Flix logo"><br>
<b>Flix</b> (<i>flight + X</i>) — open source ESP32-based quadcopter made from scratch.
</p>
<table>
<tr>
@@ -18,15 +21,13 @@
* Dedicated for education and research.
* Made from general-purpose components.
* Simple and clean source code in Arduino (<2k lines firmware).
* Control using USB gamepad, remote control or smartphone.
* Wi-Fi and MAVLink support.
* Communication using MAVLink protocol over Wi-Fi or ESP-NOW.
* Control with USB gamepad, remote control or smartphone.
* Wireless command line interface and analyzing.
* Precise simulation with Gazebo.
* Python library.
* Python library for scripting and automatic flights.
* Textbook on flight control theory and practice ([in development](https://quadcopter.dev)).
* *Position control (using external camera) and autonomous flights¹*.
*¹ — planned.*
* *Position control (planned)*.
## It actually flies
@@ -46,13 +47,21 @@ See the [user builds gallery](docs/user.md):
<a href="docs/user.md"><img src="docs/img/user/user.jpg" width=500></a>
### PCB
The official PCB *(Flix2)* is in development now. Follow the [project's channel](https://t.me/opensourcequadcopter) to track the progress.
Outdoor flights demo video of the current prototype:
<a href="https://youtu.be/KXlNmvUTi4g"><img width=300 src="https://i3.ytimg.com/vi/KXlNmvUTi4g/maxresdefault.jpg"></a>
## Simulation
The simulator is implemented using Gazebo and runs the original Arduino code:
<img src="docs/img/simulator1.png" width=500 alt="Flix simulator">
## Documentation
## Documentation articles
1. [Assembly instructions](docs/assembly.md).
2. [Usage: build, setup and flight](docs/usage.md).
@@ -70,14 +79,14 @@ Additional articles:
|Type|Part|Image|Quantity|
|-|-|:-:|:-:|
|Microcontroller board|ESP32 Mini|<img src="docs/img/esp32.jpg" width=100>|1|
|IMU (and barometer¹) board|GY91, MPU-9265 (or other MPU9250/MPU6500 board)<br>ICM20948V2 (ICM20948)³<br>GY-521 (MPU-6050)³⁻¹|<img src="docs/img/gy-91.jpg" width=90 align=center><br><img src="docs/img/icm-20948.jpg" width=100><br><img src="docs/img/gy-521.jpg" width=100>|1|
|Boost converter (optional, for more stable power supply)|5V output|<img src="docs/img/buck-boost.jpg" width=100>|1|
|Microcontroller board|ESP32 Mini.<br>ESP32-S3/ESP32-C3 boards are also supported.|<img src="docs/img/esp32.jpg" width=100>|1|
|IMU (and barometer¹) board|GY91, MPU-9265 (or other MPU9250/MPU6500 board)<br>ICM20948V2 (ICM20948)<br>GY-521 (MPU-6050)|<img src="docs/img/gy-91.jpg" width=90 align=center><br><img src="docs/img/icm-20948.jpg" width=100><br><img src="docs/img/gy-521.jpg" width=100>|1|
|*Boost converter (optional, for more stable power supply)*|*5V output*|<img src="docs/img/buck-boost.jpg" width=100>|1|
|Motor|8520 3.7V brushed motor.<br>Motor with exact 3.7V voltage is needed, not ranged working voltage (3.7V — 6V).<br>Make sure the motor shaft diameter and propeller hole diameter match!|<img src="docs/img/motor.jpeg" width=100>|4|
|Propeller|55 mm (alternatively 65 mm)|<img src="docs/img/prop.jpg" width=100>|4|
|MOSFET (transistor)|100N03A or [analog](https://t.me/opensourcequadcopter/33)|<img src="docs/img/100n03a.jpg" width=100>|4|
|Pull-down resistor|10 kΩ|<img src="docs/img/resistor10k.jpg" width=100>|4|
|3.7V Li-Po battery|LW 952540 (or any compatible by the size)|<img src="docs/img/battery.jpg" width=100>|1|
|Propeller|55 mm or 65 mm|<img src="docs/img/prop.jpg" width=100>|4|
|MOSFET (transistor)|UMW 100N03A or [analog](https://t.me/opensourcequadcopter/33).<br>Warning: don't use KIA 100N03A or other manufacturers, they might not work!|<img src="docs/img/100n03a.jpg" width=100>|4|
|Pull-down resistor<br>Voltage measurement resistor|10 kΩ|<img src="docs/img/resistor10k.jpg" width=100>|6|
|3.7V Li-Po battery|LW 952540 (or any compatible by the size).<br>Make sure the battery has enough discharge rate — 25C or more!|<img src="docs/img/battery.jpg" width=100>|1|
|Battery connector cable|MX2.0 2P female|<img src="docs/img/mx.png" width=100>|1|
|Li-Po Battery charger|Any|<img src="docs/img/charger.jpg" width=100>|1|
|Screws for IMU board mounting|M3x5|<img src="docs/img/screw-m3.jpg" width=100>|2|
@@ -137,10 +146,10 @@ You can see a user-contributed [variant of complete circuit diagram](https://mir
|Motor|Position|Direction|Prop type|Motor wires|GPIO|
|-|-|-|-|-|-|
|Motor 0|Rear left|Counter-clockwise|B|Black & White|GPIO12 (*TDI*)|
|Motor 1|Rear right|Clockwise|A|Blue & Red|GPIO13 (*TCK*)|
|Motor 2|Front right|Counter-clockwise|B|Black & White|GPIO14 (*TMS*)|
|Motor 3|Front left|Clockwise|A|Blue & Red|GPIO15 (*TD0*)|
|Motor 0|Rear left|Counter-clockwise|B|Black & White|GPIO12 *(TDI)*|
|Motor 1|Rear right|Clockwise|A|Blue & Red|GPIO13 *(TCK)*|
|Motor 2|Front right|Counter-clockwise|B|Black & White|GPIO14 *(TMS)*|
|Motor 3|Front left|Clockwise|A|Blue & Red|GPIO15 *(TD0)*|
Clockwise motors have blue & red wires and correspond to propeller type A (marked on the propeller).
Counter-clockwise motors have black & white wires correspond to propeller type B.
@@ -151,14 +160,16 @@ You can see a user-contributed [variant of complete circuit diagram](https://mir
|-|-|
|GND|GND|
|VIN|VCC (or 3.3V depending on the receiver)|
|Signal (TX)|GPIO4¹|
|Signal (TX)|GPIO4|
*¹ — UART2 RX pin was [changed](https://docs.espressif.com/projects/arduino-esp32/en/latest/migration_guides/2.x_to_3.0.html#id14) to GPIO4 in Arduino ESP32 core 3.0.*
* Optionally connect the battery voltage divider for voltage monitoring to any ADC1 pin (e. g. *GPIO32* on ESP32, *GPIO3* on ESP32-S3).
ESP32 and ESP32-S3 [can measure](https://docs.espressif.com/projects/arduino-esp32/en/latest/api/adc.html#analogsetattenuation) up to 3.1 V and ESP32-S3/ESP32-C3 can measure up to 2.5 V, so choose the voltage divider resistors accordingly.
## Resources
* Telegram channel on developing the drone and the flight controller (in Russian): https://t.me/opensourcequadcopter.
* Official Telegram chat: https://t.me/opensourcequadcopterchat.
* Official Telegram chat: https://t.me/opensourcequadcopterchat (English / Russian).
* Detailed article on Habr.com about the development of the drone (in Russian): https://habr.com/ru/articles/814127/.
## Disclaimer
-5
View File
@@ -1,5 +0,0 @@
board_manager:
additional_urls:
- https://raw.githubusercontent.com/espressif/arduino-esp32/gh-pages/package_esp32_index.json
network:
connection_timeout: 1h
+6 -4
View File
@@ -28,6 +28,8 @@ Soldered components ([schematics variant](https://miro.com/app/board/uXjVN-dTjoo
<img src="img/assembly/7.jpg" width=600>
See an alternative assembly process photos here: https://drive.google.com/drive/folders/1FG5BH9RCzdf1XmJcC70PymiRMXcz6Fx7?usp=sharing.
## Motor directions
> [!WARNING]
@@ -41,10 +43,10 @@ Motors connection table:
|Motor|Position|Direction|Prop type|Motor wires|GPIO|
|-|-|-|-|-|-|
|Motor 0|Rear left|Counter-clockwise|B|Black & White|GPIO12 (*TDI*)|
|Motor 1|Rear right|Clockwise|A|Blue & Red|GPIO13 (*TCK*)|
|Motor 2|Front right|Counter-clockwise|B|Black & White|GPIO14 (*TMS*)|
|Motor 3|Front left|Clockwise|A|Blue & Red|GPIO15 (*TD0*)|
|Motor 0|Rear left|Counter-clockwise|B|Black & White|GPIO12 *(TDI)*|
|Motor 1|Rear right|Clockwise|A|Blue & Red|GPIO13 *(TCK)*|
|Motor 2|Front right|Counter-clockwise|B|Black & White|GPIO14 *(TMS)*|
|Motor 3|Front left|Clockwise|A|Blue & Red|GPIO15 *(TD0)*|
## Motors tightening
+1 -1
View File
@@ -35,7 +35,7 @@
### Подсистема управления
Состояние органов управления обрабатывается в функции `interpretControls()` и преобразуется в *команду управления*, которая включает следующее:
Состояние органов управления обрабатывается в функции `interpretControls()` и преобразуется в **команду управления**, которая включает следующее:
* `attitudeTarget` *(Quaternion)* — целевая ориентация дрона.
* `ratesTarget` *(Vector)* — целевые угловые скорости, *рад/с*.
+9 -9
View File
@@ -110,7 +110,7 @@ float angle = Vector::angleBetween(a, b); // 1.57 (90 градусов)
#### Скалярное произведение
Скалярное произведение векторов (*dot product*) — это произведение длин двух векторов на косинус угла между ними. В математике оно обозначается знаком `·` или слитным написанием векторов. Интуитивно, результат скалярного произведения показывает, насколько два вектора *сонаправлены*.
Скалярное произведение векторов *(dot product)* — это произведение длин двух векторов на косинус угла между ними. В математике оно обозначается знаком `·` или слитным написанием векторов. Интуитивно, результат скалярного произведения показывает, насколько два вектора *сонаправлены*.
В Flix используется статический метод `Vector::dot()`:
@@ -124,7 +124,7 @@ float dotProduct = Vector::dot(a, b); // 32
#### Векторное произведение
Векторное произведение (*cross product*) позволяет найти вектор, перпендикулярный двум другим векторам. В математике оно обозначается знаком `×`, а в прошивке используется статический метод `Vector::cross()`:
Векторное произведение *(cross product)* позволяет найти вектор, перпендикулярный двум другим векторам. В математике оно обозначается знаком `×`, а в прошивке используется статический метод `Vector::cross()`:
```cpp
Vector a(1, 2, 3);
@@ -144,9 +144,9 @@ Vector crossProduct = Vector::cross(a, b); // -3, 6, -3
В прошивке углы Эйлера сохраняются в обычный объект `Vector` (хоть и, строго говоря, не являются вектором):
* Угол по крену (*roll*) — `vector.x`.
* Угол по тангажу (*pitch*) — `vector.y`.
* Угол по рысканию (*yaw*) — `vector.z`.
* Угол по крену *(roll)* — `vector.x`.
* Угол по тангажу *(pitch)* — `vector.y`.
* Угол по рысканию *(yaw)* — `vector.z`.
Особенности углов Эйлера:
@@ -162,8 +162,8 @@ Vector crossProduct = Vector::cross(a, b); // -3, 6, -3
Помимо углов Эйлера, любую ориентацию в трехмерном пространстве можно представить в виде вращения вокруг некоторой оси на некоторый угол. В геометрии это доказывается, как **теорема вращения Эйлера**. В таком представлении ориентация задается двумя величинами:
* **Ось вращения** (*axis*) — единичный вектор, определяющий ось вращения.
* **Угол поворота** (*angle* или *θ*) — угол, на который нужно повернуть объект вокруг этой оси.
* **Ось вращения** *(axis)* — единичный вектор, определяющий ось вращения.
* **Угол поворота** *(angle* или *θ)* — угол, на который нужно повернуть объект вокруг этой оси.
В Flix ось вращения задается объектом `Vector`, а угол поворота — числом типа `float` в радианах:
@@ -177,7 +177,7 @@ float angle = radians(45);
### Вектор вращения
Если умножить вектор *axis* на угол поворота *θ*, то получится **вектор вращения** (*rotation vector*). Этот вектор играет важную роль в алгоритмах управления ориентацией летательного аппарата.
Если умножить вектор *axis* на угол поворота *θ*, то получится **вектор вращения** *(rotation vector)*. Этот вектор играет важную роль в алгоритмах управления ориентацией летательного аппарата.
Вектор вращения обладает замечательным свойством: если угловые скорости объекта (в собственной системе координат) в каждый момент времени совпадают с компонентами этого вектора, то за единичное время объект придет к заданной этим вектором ориентации. Это свойство позволяет использовать вектор вращения для управления ориентацией объекта посредством управления угловыми скоростями.
@@ -198,7 +198,7 @@ Vector rotation = radians(45) * Vector(1, 2, 3);
<a href="https://github.com/okalachev/flix/blob/master/flix/quaternion.h"><code>quaternion.h</code></a>.<br>
</div>
Вектор вращения удобен, но еще удобнее использовать **кватернион**. В Flix кватернионы задаются объектами `Quaternion` из библиотеки `quaternion.h`. Кватернион состоит из четырех значений: *w*, *x*, *y*, *z* и рассчитывается из вектора оси вращения (*axis*) и угла поворота (*θ*) по формуле:
Вектор вращения удобен, но еще удобнее использовать **кватернион**. В Flix кватернионы задаются объектами `Quaternion` из библиотеки `quaternion.h`. Кватернион состоит из четырех значений: *w*, *x*, *y*, *z* и рассчитывается из вектора оси вращения *(axis)* и угла поворота *(θ)* по формуле:
\\[ q = \left( \begin{array}{c} w \\\\ x \\\\ y \\\\ z \end{array} \right) = \left( \begin{array}{c} \cos\left(\frac{\theta}{2}\right) \\\\ axis\_x \cdot \sin\left(\frac{\theta}{2}\right) \\\\ axis\_y \cdot \sin\left(\frac{\theta}{2}\right) \\\\ axis\_z \cdot \sin\left(\frac{\theta}{2}\right) \end{array} \right) \\]
+27 -27
View File
@@ -87,13 +87,13 @@ Flix поддерживает следующие модели IMU:
#include <FlixPeriph.h>
#include <SPI.h>
MPU9250 IMU(SPI);
MPU9250 imu(SPI);
void setup() {
Serial.begin(115200);
bool success = IMU.begin();
bool success = imu.begin();
if (!success) {
Serial.println("Failed to initialize IMU");
Serial.println("Failed to initialize the IMU");
}
}
```
@@ -108,21 +108,21 @@ void setup() {
#include <FlixPeriph.h>
#include <SPI.h>
MPU9250 IMU(SPI);
MPU9250 imu(SPI);
void setup() {
Serial.begin(115200);
bool success = IMU.begin();
bool success = imu.begin();
if (!success) {
Serial.println("Failed to initialize IMU");
Serial.println("Failed to initialize the IMU");
}
}
void loop() {
IMU.waitForData();
imu.waitForData();
float gx, gy, gz;
IMU.getGyro(gx, gy, gz);
imu.getGyro(gx, gy, gz);
Serial.printf("gx:%f gy:%f gz:%f\n", gx, gy, gz);
delay(50); // замедление вывода
@@ -135,36 +135,36 @@ void loop() {
## Конфигурация гироскопа
В коде Flix настройка IMU происходит в функции `configureIMU`. В этой функции настраиваются три основных параметра гироскопа: диапазон измерений, частота сэмплов и частота LPF-фильтра.
В коде Flix настройка IMU происходит в функции `configureIMU`. В этой функции настраиваются три основных параметра гироскопа: диапазон измерений, частота сэмплирования и частота LPF-фильтра.
### Частота сэмплов
### Частота сэмплирования
Большинство IMU могут обновлять данные с разной частотой. В полетных контроллерах обычно используется частота обновления от 500 Гц до 8 кГц. Чем выше частота сэмплов, тем выше точность управления полетом, но и больше нагрузка на микроконтроллер.
Большинство IMU могут обновлять данные с разной частотой. В полетных контроллерах обычно используется частота обновления от 500 Гц до 8 кГц. Чем выше частота, тем выше точность управления полетом, но и тем больше нагрузка на микроконтроллер.
Частота сэмплов устанавливается методом `setSampleRate()`. В Flix используется частота 1 кГц:
Частота сэмплирования устанавливается методом `setSampleRate()`. В Flix используется частота 1 кГц:
```cpp
IMU.setRate(IMU.RATE_1KHZ_APPROX);
```
Поскольку не все поддерживаемые IMU могут работать строго на частоте 1 кГц, в библиотеке FlixPeriph существует возможность приближенной настройки частоты сэмплов. Например, у IMU ICM-20948 при такой настройке реальная частота сэмплирования будет равна 1125 Гц.
Поскольку не все поддерживаемые IMU могут работать строго на частоте 1 кГц, в библиотеке FlixPeriph существует возможность приближенной настройки частоты сэмплирования. Например, у IMU ICM-20948 при такой настройке реальная частота сэмплирования будет равна 1125 Гц.
Другие доступные для установки в библиотеке FlixPeriph частоты сэмплирования:
* `RATE_MIN` — минимальная частота сэмплов для конкретного IMU.
* `RATE_MIN` — минимальная частота для конкретного IMU.
* `RATE_50HZ_APPROX` — значение, близкое к 50 Гц.
* `RATE_1KHZ_APPROX` — значение, близкое к 1 кГц.
* `RATE_8KHZ_APPROX` — значение, близкое к 8 кГц.
* `RATE_MAX` — максимальная частота сэмплов для конкретного IMU.
* `RATE_MAX` — максимальная частота для конкретного IMU.
#### Диапазон измерений
Большинство MEMS-гироскопов поддерживают несколько диапазонов измерений угловой скорости. Главное преимущество выбора меньшего диапазона — бо́льшая чувствительность. В полетных контроллерах обычно выбирается максимальный диапазон измерений от –2000 до 2000 градусов в секунду, чтобы обеспечить возможность динамичных маневров.
Большинство MEMS-гироскопов поддерживают несколько диапазонов измерений угловой скорости. Главное преимущество выбора меньшего диапазона — бо́льшая чувствительность. В полетных контроллерах обычно выбирается максимальный диапазон измерений от –2000 до 2000 градусов в секунду, чтобы обеспечить возможность быстрых маневров.
В библиотеке FlixPeriph диапазон измерений гироскопа устанавливается методом `setGyroRange()`:
```cpp
IMU.setGyroRange(IMU.GYRO_RANGE_2000DPS);
imu.setGyroRange(imu.GYRO_RANGE_2000DPS);
```
### LPF-фильтр
@@ -172,16 +172,16 @@ IMU.setGyroRange(IMU.GYRO_RANGE_2000DPS);
IMU InvenSense могут фильтровать измерения на аппаратном уровне при помощи фильтра нижних частот (LPF). Flix реализует собственный фильтр для гироскопа, чтобы иметь больше гибкости при поддержке разных IMU. Поэтому для встроенного LPF устанавливается максимальная частота среза:
```cpp
IMU.setDLPF(IMU.DLPF_MAX);
imu.setDLPF(imu.DLPF_MAX);
```
## Калибровка гироскопа
Как и любое измерительное устройство, гироскоп вносит искажения в измерения. Наиболее простая модель этих искажений делит их на статические смещения (*bias*) и случайный шум (*noise*):
Как и любое измерительное устройство, гироскоп вносит искажения в измерения. Наиболее простая модель этих искажений делит их на статические смещения *(bias)* и случайный шум *(noise)*:
\\[ gyro_{xyz}=rates_{xyz}+bias_{xyz}+noise \\]
Для качественной работы подсистемы оценки ориентации и управления дроном необходимо оценить *bias* гироскопа и учесть его в вычислениях. Для этого при запуске программы производится калибровка гироскопа, которая реализована в функции `calibrateGyro()`. Эта функция считывает данные с гироскопа в состоянии покоя 1000 раз и усредняет их. Полученные значения считаются *bias* гироскопа и в дальнейшем вычитаются из измерений.
Для точной работы подсистемы оценки ориентации и управления дроном необходимо оценить *bias* гироскопа и учесть его в вычислениях. Для этого при запуске программы производится калибровка гироскопа, которая реализована в функции `calibrateGyro()`. Эта функция считывает данные с гироскопа в состоянии покоя 1000 раз и усредняет их. Полученные значения считаются *bias* гироскопа и в дальнейшем вычитаются из измерений.
Программа для вывода данных с гироскопа с калибровкой:
@@ -189,23 +189,23 @@ IMU.setDLPF(IMU.DLPF_MAX);
#include <FlixPeriph.h>
#include <SPI.h>
MPU9250 IMU(SPI);
MPU9250 imu(SPI);
float gyroBiasX, gyroBiasY, gyroBiasZ; // bias гироскопа
void setup() {
Serial.begin(115200);
bool success = IMU.begin();
bool success = imu.begin();
if (!success) {
Serial.println("Failed to initialize IMU");
Serial.println("Failed to initialize the IMU");
}
calibrateGyro();
}
void loop() {
float gx, gy, gz;
IMU.waitForData();
IMU.getGyro(gx, gy, gz);
imu.waitForData();
imu.getGyro(gx, gy, gz);
// Устранение bias гироскопа
gx -= gyroBiasX;
@@ -226,9 +226,9 @@ void calibrateGyro() {
// Получение 1000 измерений гироскопа
for (int i = 0; i < samples; i++) {
IMU.waitForData();
imu.waitForData();
float gx, gy, gz;
IMU.getGyro(gx, gy, gz);
imu.getGyro(gx, gy, gz);
gyroBiasX += gx;
gyroBiasY += gy;
gyroBiasZ += gz;
+40 -3
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@@ -38,13 +38,13 @@ Utility files:
### Control subsystem
Pilot inputs are interpreted in `interpretControls()`, and then converted to the *control command*, which consists of the following:
Pilot inputs are interpreted in `interpretControls()`, and then converted to the **control command**, which consists of the following:
* `attitudeTarget` *(Quaternion)* — target attitude of the drone.
* `ratesTarget` *(Vector)* — target angular rates, *rad/s*.
* `ratesExtra` *(Vector)* — additional (feed-forward) angular rates , used for yaw rate control in STAB mode, *rad/s*.
* `ratesExtra` *(Vector)* — additional (feed-forward) angular rates, used for yaw rate control in STAB mode, *rad/s*.
* `torqueTarget` *(Vector)* — target torque, range [-1, 1].
* `thrustTarget` *(float)* — collective thrust target, range [0, 1].
* `thrustTarget` *(float)* — collective motor thrust target, range [0, 1].
Control command is handled in `controlAttitude()`, `controlRates()`, `controlTorque()` functions. Each function may be skipped if the corresponding control target is set to `NAN`.
@@ -62,6 +62,43 @@ print("Test value: %.2f\n", testValue);
In order to add a console command, modify the `doCommand()` function in `cli.ino` file.
> [!IMPORTANT]
> Avoid using delays in in-flight commands, it will **crash** the drone! (The design is one-threaded.)
>
> For on-the-ground commands, use `pause()` function, instead of `delay()`. This function allows to pause in a way that MAVLink connection will continue working.
### Parameter subsystem
Parameters subsystem (`parameters.ino`) uses standard [Preferences.h](https://docs.espressif.com/projects/arduino-esp32/en/latest/tutorials/preferences.html) ESP32 library to store parameters in non-volatile memory. Each parameter is a regular global variable, which is registered in the `parameters` array.
To add a new parameter:
1. Define a global variable for the parameter, two types are supported: `float` and `int`.
2. Add an entry to the `parameters` array, with the parameter name, a pointer to the variable, and optionally a callback function to call when the parameter is changed.
3. Everything else will be handled automatically.
See examples of adding new parameters in commits: [c434107](https://github.com/okalachev/flix/commit/c434107), [a687303](https://github.com/okalachev/flix/commit/a687303).
> [!NOTE]
> Since all the parameters are internally stored and passed as floats, the safe range for `int` parameters is -16777216 to 16777215.
## Adding a subsystem
To add a new subsystem:
1. Create a new `*.ino` file for your subsystem.
2. Define setup and loop functions for the subsystem, for example `setupMySubsystem()` and `loopMySubsystem()`.
3. Use `Rate` class if you need to limit the loop frequency, for example:
```cpp
Rate mySubsystemRate(100); // 100 Hz
void loopMySubsystem() {
if (!mySubsystemRate) return;
// Do something...
}
4. Add setup and loop calls in to `setup()` and `loop()` functions in `flix.ino`.
## Building the firmware
See build instructions in [usage.md](usage.md).
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@@ -4,28 +4,33 @@
Do the following:
* **Check ESP32 core is installed**. Check if the version matches the one used in the [tutorial](usage.md#firmware).
* **Check libraries**. Install all the required libraries from the tutorial. Make sure there are no MPU9250 or other peripherals libraries that may conflict with the ones used in the tutorial.
* **Check ESP32 core is installed**. Check if the version matches the one used in the [tutorial](usage.md#building-the-firmware).
* **Check libraries**. Install all the required libraries from the tutorial. Make sure there are no MPU-9250 or other peripherals libraries that may conflict with the ones used in the tutorial.
* **Check the chosen board**. The correct board to choose in Arduino IDE for ESP32 Mini is *WEMOS D1 MINI ESP32*.
## The drone doesn't fly
Do the following:
* **Check the battery voltage**. Use a multimeter to measure the battery voltage. It should be in range of 3.7-4.2 V.
* **Check if there are some startup errors**. Connect the ESP32 to the computer and check the Serial Monitor output. Use the Reset button to make sure you see the whole ESP32 output.
* **Check the battery voltage**. Use a multimeter to measure the battery voltage. The fully charged battery should have about 4.2V.
* **Check the battery you use has enough discharge current**. The battery should be able to provide 15A of current. So the C-rating for a 1000 mAh battery should be at least 15C (higher is better).
* **Check if there are some startup errors**. Connect the ESP32 to the computer and check the Serial Monitor output. Use the Reset button or `reboot` command to see the whole startup output.
* **Check the baudrate is correct**. If you see garbage characters in the Serial Monitor, make sure the baudrate is set to 115200.
* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
* **Check if the CLI is working**. Perform `help` command in Serial Monitor. You should see the list of available commands. You can also access the CLI using QGroundControl (*Vehicle Setup* ⇒ *Analyze Tools**MAVLink Console*).
* **Check if the console is working**. Perform `help` command in Serial Monitor. You should see the list of available commands. You can also access the console using QGroundControl *(Vehicle Setup**Analyze Tools**MAVLink Console)*.
* **Configure QGroundControl correctly before connecting to the drone** if you use it to control the drone. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
* **If QGroundControl doesn't connect**, you might need to disable the firewall and/or VPN on your computer.
* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
* **Check the IMU is working**. Perform `imu` command and check its output:
* The `status` field should be `OK`.
* The `rate` field should be about 1000 (Hz).
* The `accel` and `gyro` fields should change as you move the drone.
* **Check the IMU orientation is set correctly**. If the attitude estimation is rotated, set the correct IMU orientation as described in the [tutorial](usage.md#define-imu-orientation).
* **Calibrate the accelerometer.** if is wasn't done before. Type `ca` command in Serial Monitor and follow the instructions.
* **Check the attitude estimation**. Connect to the drone using QGroundControl. Rotate the drone in different orientations and check if the attitude estimation shown in QGroundControl is correct.
* **Check the IMU orientation is set correctly**. If the attitude estimation is rotated, make sure `rotateIMU` function is defined correctly in `imu.ino` file.
* **Check the attitude estimation**. Connect to the drone using QGroundControl. Rotate the drone in different orientations and check if the attitude estimation is shown exactly as on the video below:
<a href="https://youtu.be/yVRN23-GISU"><img width=200 src="https://i3.ytimg.com/vi/yVRN23-GISU/maxresdefault.jpg"></a>
* **Check the IMU output**. Connect to the drone using QGroundControl on your computer. Go to the *Analyze* tab, *MAVLINK Inspector*. Plot the data from the `SCALED_IMU` message. The gyroscope and accelerometer data should change according to the drone movement.
* **Check the motors type**. Motors with exact 3.7V voltage are needed, not ranged working voltage (3.7V — 6V).
* **Check the motors**. Perform the following commands using Serial Monitor:
* `mfr` — should rotate front right motor (counter-clockwise).
@@ -33,7 +38,10 @@ Do the following:
* `mrl` — should rotate rear left motor (counter-clockwise).
* `mrr` — should rotate rear right motor (clockwise).
* **Check the propeller directions are correct**. Make sure your propeller types (A or B) are installed as on the picture:
<img src="img/user/peter_ukhov-2/1.jpg" width="200">
* **Check the remote control**. Using `rc` command, check the control values reflect your sticks movement. All the controls should change between -1 and 1, and throttle between 0 and 1.
* If using SBUS receiver, **calibrate the RC**. Type `cr` command in Serial Monitor and follow the instructions.
* **Check the IMU output using QGroundControl**. Connect to the drone using QGroundControl on your computer. Go to the *Analyze* tab, *MAVLINK Inspector*. Plot the data from the `SCALED_IMU` message. The gyroscope and accelerometer data should change according to the drone movement.
* **If using an SBUS receiver**:
* **Define the used GPIO pin** in `RC_RX_PIN` parameter.
* **Calibrate the RC** using `cr` command in the console.
* **Check the controls** using `rc` command. All the controls should change between -1 and 1, and the throttle between 0 and 1.
+173 -38
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@@ -20,13 +20,14 @@ You can build and upload the firmware using either **Arduino IDE** (easier for b
1. Install [Arduino IDE](https://www.arduino.cc/en/software) (version 2 is recommended).
2. *Windows users might need to install [USB to UART bridge driver from Silicon Labs](https://www.silabs.com/developers/usb-to-uart-bridge-vcp-drivers).*
3. Install ESP32 core, version 3.2.0. See the [official Espressif's instructions](https://docs.espressif.com/projects/arduino-esp32/en/latest/installing.html#installing-using-arduino-ide) on installing ESP32 Core in Arduino IDE.
3. Install ESP32 core, version 3.3.10. See the [official Espressif's instructions](https://docs.espressif.com/projects/arduino-esp32/en/latest/installing.html#installing-using-arduino-ide) on installing ESP32 Core in Arduino IDE.
4. Install the following libraries using [Library Manager](https://docs.arduino.cc/software/ide-v2/tutorials/ide-v2-installing-a-library):
* `FlixPeriph`, the latest version.
* `MAVLink`, version 2.0.16.
* `MAVLink`, version 2.0.25.
5. Open the `flix/flix.ino` sketch from downloaded firmware sources in Arduino IDE.
6. Connect your ESP32 board to the computer and choose correct board type in Arduino IDE (*WEMOS D1 MINI ESP32* for ESP32 Mini) and the port.
7. [Build and upload](https://docs.arduino.cc/software/ide-v2/tutorials/getting-started/ide-v2-uploading-a-sketch) the firmware using Arduino IDE.
6. Connect your ESP32 board to the computer and choose correct board type in Arduino IDE (*WEMOS D1 MINI ESP32* for ESP32 Mini, *ESP32S3 Dev Module* for ESP32-S3 Super Mini) and the port.
7. Set *Tools**Core Debug Level* to *Error* to see the errors in the serial console. Set *Tools**USB CDC on Boot* to *Enabled* for ESP32-S3/ESP32-C3 boards.
8. [Build and upload](https://docs.arduino.cc/software/ide-v2/tutorials/getting-started/ide-v2-uploading-a-sketch) the firmware using Arduino IDE.
### Command line (Windows, Linux, macOS)
@@ -57,6 +58,12 @@ You can build and upload the firmware using either **Arduino IDE** (easier for b
make upload monitor
```
For ESP32-S3/ESP32-C3 boards, set the appropriate [FQBN](https://docs.arduino.cc/arduino-cli/FAQ/#whats-the-fqbn-string) using `BOARD` parameter:
```bash
make BOARD=esp32:esp32:esp32s3:FlashSize=4M,CDCOnBoot=cdc upload
```
See other available Make commands in [Makefile](../Makefile).
> [!TIP]
@@ -69,8 +76,25 @@ See other available Make commands in [Makefile](../Makefile).
In case if using different IMU model than MPU9250, change `imu` variable declaration in the `imu.ino`:
```cpp
ICM20948 imu(SPI); // For ICM-20948
MPU6050 imu(Wire); // For MPU-6050
ICM20948 imu(SPI); // For ICM-20948 via SPI
// or
MPU6050 imu(Wire); // For MPU-6050 via I2C
```
If using non-default SPI pins, pass SCK, MISO, and MOSI pin numbers to `SPI.begin` call and SS pin to `imu` constructor like that:
```cpp
ICM20948(SPI, <SS>);
// ...
SPI.begin(<SCK>, <MISO>, <MOSI>);
imu.begin();
```
If using non-default I2C pins, pass SDA and SCL pin numbers to `Wire.setPins` call like that:
```cpp
Wire.begin(<SDA>, <SCL>);
imu.begin();
```
### Connect using QGroundControl
@@ -80,7 +104,10 @@ QGroundControl is a ground control station software that can be used to monitor
1. Install mobile or desktop version of [QGroundControl](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html).
2. Power up the drone.
3. Connect your computer or smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
4. Launch QGroundControl app. It should connect and begin showing the drone's telemetry automatically
4. Launch QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
> [!TIP]
> If QGroundControl doesn't connect, try to disable the firewall and/or VPN on your computer, as they may block the connection.
### Access console
@@ -95,7 +122,7 @@ To access the console using serial port:
To access the console using QGroundControl:
1. Connect to the drone using QGroundControl app.
2. Go to the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Analyze Tools* ⇒ *MAVLink Console*.
2. Go to the QGroundControl menu ⇒ *Analyze Tools* ⇒ *MAVLink Console*.
<img src="img/cli.png" width="400">
@@ -108,11 +135,13 @@ The drone is configured using parameters. To access and modify them, go to the Q
<img src="img/parameters.png" width="400">
You can also work with parameters using `p` command in the console. Parameter names are case-insensitive.
### Define IMU orientation
Use parameters, to define the IMU board axes orientation relative to the drone's axes: `IMU_ROT_ROLL`, `IMU_ROT_PITCH`, and `IMU_ROT_YAW`.
The IMU orientation (relative to the drone's axes) is defined using the parameters: `IMU_ROT_ROLL`, `IMU_ROT_PITCH`, and `IMU_ROT_YAW`.
The drone has *X* axis pointing forward, *Y* axis pointing left, and *Z* axis pointing up, and the supported IMU boards have *X* axis pointing to the pins side and *Z* axis pointing up from the side with the components:
The drone has *X* axis pointing forward, *Y* axis pointing left, and *Z* axis pointing up, and the supported IMU boards have *X* axis pointing to the mounting holes side and *Z* axis pointing up from the component side:
<img src="img/imu-axes.png" width="200">
@@ -120,10 +149,10 @@ Use the following table to set the parameters for common IMU orientations:
|Orientation|Parameters|Orientation|Parameters|
|:-:|-|-|-|
|<img src="img/imu-rot-1.png" width="200">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0 |<img src="img/imu-rot-5.png" width="200">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0|
|<img src="img/imu-rot-2.png" width="200">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|<img src="img/imu-rot-6.png" width="200">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|
|<img src="img/imu-rot-3.png" width="200">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|<img src="img/imu-rot-7.png" width="200">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|
|<img src="img/imu-rot-4.png" width="200"><br>☑️ **Default**|<br>`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|<img src="img/imu-rot-8.png" width="200">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|
|<img src="img/imu-rot-3.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0 |<img src="img/imu-rot-7.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0|
|<img src="img/imu-rot-2.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|<img src="img/imu-rot-6.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|
|<img src="img/imu-rot-1.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|<img src="img/imu-rot-5.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|
|<img src="img/imu-rot-4.png" width="180"><br>☑️ **Default**|<br>`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|<img src="img/imu-rot-8.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|
### Calibrate accelerometer
@@ -132,34 +161,75 @@ Before flight you need to calibrate the accelerometer:
1. Access the console using QGroundControl (recommended) or Serial Monitor.
2. Type `ca` command there and follow the instructions.
### Check everything works
### Setup motors
1. Check the IMU is working: perform `imu` command and check its output:
If using non-default motor pins, set the pin numbers using the parameters: `MOTOR_PIN_FL`, `MOTOR_PIN_FR`, `MOTOR_PIN_RL`, `MOTOR_PIN_RR` (front-left, front-right, rear-left, rear-right respectively).
Certain ESP32 models (such as ESP32-S3 and ESP32-C3) support a lower maximum PWM frequency; on these boards the parameter `MOT_PWM_FREQ` should be set to 38000 Hz.
If using brushless motors and ESCs:
1. Set the appropriate PWM using the parameters: `MOT_PWM_STOP`, `MOT_PWM_MIN`, and `MOT_PWM_MAX` (1000, 1000, and 2000 is typical).
2. Decrease the PWM frequency using the `MOT_PWM_FREQ` parameter (400 is typical).
> [!CAUTION]
> **Remove the props when configuring the motors!** If improperly configured, you may not be able to stop them.
### Battery voltage monitoring
ESP32 ADC can measure only up to 3.3 V, so you need to use a voltage divider to monitor the battery voltage. To enable voltage measurement, set the following parameters:
1. `PWR_VOLT_PIN` — GPIO pin number where the voltage divider is connected (*-1* to disable).
2. `PWR_VOLT_SCALE` — voltage divider coefficient (*2* for two equal resistors).
After this setup, you should see the battery voltage in QGroundControl top panel or using `pw` command in the console.
### Important: check everything works
1. Check the IMU is working: perform `imu` command in the console and check the output:
* The `status` field should be `OK`.
* The `rate` field should be about 1000 (Hz).
* The `accel` and `gyro` fields should change as you move the drone.
* The `accel bias` and `accel scale` fields should contain calibration parameters (not zeros and ones).
* The `gyro bias` field should contain estimated gyro bias (not zeros).
* The `landed` field should be `1` when the drone is still on the ground and `0` when you lift it up.
2. Check the attitude estimation: connect to the drone using QGroundControl, rotate the drone in different orientations and check if the attitude estimation shown in QGroundControl is correct. Attitude indicator in QGroundControl is shown below:
2. Check the attitude estimation: connect to the drone using QGroundControl, rotate the drone in different orientations and check if the attitude estimation shown in QGroundControl is correct. Compare your attitude indicator (in the *large vertical* mode) to the video:
<img src="img/qgc-attitude.png" height="200">
<a href="https://youtu.be/yVRN23-GISU"><img width=300 src="https://i3.ytimg.com/vi/yVRN23-GISU/maxresdefault.jpg"></a>
3. Perform motor tests in the console. Use the following commands **— remove the propellers before running the tests!**
3. Perform motor tests. Use the following commands **— remove the propellers before running the tests!**
* `mfr` — should rotate front right motor (counter-clockwise).
* `mfl` — should rotate front left motor (clockwise).
* `mrl` — should rotate rear left motor (counter-clockwise).
* `mrr` — should rotate rear right motor (clockwise).
* `mfr` — rotate front right motor (counter-clockwise).
* `mfl` — rotate front left motor (clockwise).
* `mrl` — rotate rear left motor (counter-clockwise).
* `mrr` — rotate rear right motor (clockwise).
Make sure rotation directions and propeller types match the following diagram:
<img src="img/motors.svg" width=200>
> [!WARNING]
> Never run the motors when powering the drone from USB, always use the battery for that.
## Setup remote control
There are several ways to control the drone's flight: using **smartphone** (Wi-Fi), using **SBUS remote control**, or using **USB remote control** (Wi-Fi).
There are several ways to control the drone's flight: using **smartphone** (Wi-Fi), using **SBUS remote control**, or using **USB remote control** (Wi-Fi/ESP-NOW).
### Control with smartphone
### Control with a smartphone
#### Using Mavlink Joystick app (Android)
<img src="https://github.com/goldarte/mavlink-joystick/blob/master/app_screen.png?raw=true" width="400">
1. Download and install [Mavlink Joystick app](https://github.com/goldarte/mavlink-joystick/releases/latest).
2. Power the drone using the battery.
3. Connect your smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
4. Open Mavlink Joystick app. It should connect and begin showing the drone's telemetry automatically.
5. Use the virtual joystick to fly the drone!
#### Using QGroundControl app
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone.
2. Power the drone using the battery.
@@ -171,15 +241,17 @@ There are several ways to control the drone's flight: using **smartphone** (Wi-F
> [!TIP]
> Decrease `CTL_TILT_MAX` parameter when flying using the smartphone to make the controls less sensitive.
### Control with remote control
### Control with a remote control
Before using remote SBUS-connected remote control, you need to calibrate it:
If using SBUS-connected remote control you need to enable SBUS and calibrate it:
1. Access the console using QGroundControl (recommended) or Serial Monitor.
2. Type `cr` command and follow the instructions.
3. Use the remote control to fly the drone!
1. Connect to the drone using QGroundControl.
2. In parameters, set the `RC_RX_PIN` parameter to the GPIO pin number where the SBUS signal is connected, for example: 4. Negative value disables SBUS.
3. Check if the receiver is working using `rc` command in the console.
4. Open the console, type `cr` command and follow the instructions to calibrate the remote control.
5. Use the remote control to fly the drone!
### Control with USB remote control
### Control with a USB remote control
If your drone doesn't have RC receiver installed, you can use USB remote control and QGroundControl app to fly it.
@@ -188,7 +260,7 @@ If your drone doesn't have RC receiver installed, you can use USB remote control
3. Power up the drone.
4. Connect your computer to the appeared `flix` Wi-Fi network (password: `flixwifi`).
5. Launch QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
6. Go the the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Joystick*. Calibrate you USB remote control there.
6. Go to the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Joystick*. Calibrate your USB remote control there.
7. Use the USB remote control to fly the drone!
## Flight
@@ -214,11 +286,11 @@ When finished flying, **disarm** the drone, moving the left stick to the bottom
### Flight modes
Flight mode is changed using mode switch on the remote control or using the command line.
Flight mode is changed using mode switch on the remote control (if configured) or using the console commands. The main flight mode is *STAB*. In order to change modes using SBUS remote control, set the parameters: `CTL_FLT_MODE_0`, `CTL_FLT_MODE_1`, and `CTL_FLT_MODE_2` to required mode numbers (0 for *RAW*, 1 for *ACRO*, 2 for *STAB*, 3 for *AUTO*).
#### STAB
The default mode is *STAB*. In this mode, the drone stabilizes its attitude (orientation). The left stick controls throttle and yaw rate, the right stick controls pitch and roll angles.
In this mode, the drone stabilizes its attitude (orientation). The left stick controls throttle and yaw rate, the right stick controls pitch and roll angles.
> [!IMPORTANT]
> The drone doesn't stabilize its position, so slight drift is possible. The pilot should compensate it manually.
@@ -233,15 +305,78 @@ In this mode, the pilot controls the angular rates. This control method is diffi
#### AUTO
In this mode, the pilot inputs are ignored (except the mode switch, if configured). The drone can be controlled using [pyflix](../tools/pyflix/) Python library, or by modifying the firmware to implement the needed autonomous behavior.
In this mode, the pilot inputs are ignored (except the mode switch). The drone can be controlled using [pyflix](../tools/pyflix/) Python library, or by modifying the firmware to implement the needed behavior.
If the pilot moves the control sticks, the drone will switch back to *STAB* mode.
If the pilot moves the control sticks and mode switch is not configured, the drone will switch back to *STAB* mode.
<img src="img/parameters.png" width="400">
## Wi-Fi configuration
You can configure the Wi-Fi using parameters and console commands.
The Wi-Fi mode is chosen using `WIFI_MODE` parameter in QGroundControl or in the console:
* `0` — Wi-Fi is disabled.
* `1` — Access Point mode *(AP)* — the drone creates a Wi-Fi network.
* `2` — Client mode *(STA)* — the drone connects to an existing Wi-Fi network (may cause additional delays, so generally not recommended).
* `3` — ESP-NOW mode — the drone uses ESP-NOW protocol for communication.
The SSID and password are configured using the `ap` and `sta` console commands:
```
ap <ssid> <password>
sta <ssid> <password>
```
Example of configuring the Access Point mode:
```
ap my-flix-ssid mypassword123
p WIFI_MODE 1
```
Disabling Wi-Fi:
```
p WIFI_MODE 0
```
### Using ESP-NOW
[ESP-NOW](https://docs.espressif.com/projects/esp-idf/en/stable/esp32/api-reference/network/esp_now.html) is a low level wireless communication protocol. It can provide lower latency, better reliability, and longer range than Wi-Fi. However, it requires a second ESP32 board to be used as a proxy for the computer.
<img src="img/espnow-connection.jpg" width="600">
To setup ESP-NOW communication:
1. Flash the second ESP32 board with ESP-NOW proxy sketch: [`tools/espnow-proxy/espnow-proxy.ino`](../tools/espnow-proxy/espnow-proxy.ino). Use Arduino IDE or command line: `make upload_proxy`.
2. Open Serial Monitor in Arduino IDE or use `make monitor` command. The ESP32 will print its MAC address and generated encryption key, for example:
```
espnow 7a:c8:e3:eb:bf:e9 &PiuSysxP9+$L&5E
```
Run this line as a console command on each drone you want to bind to this proxy board. [The maximum number](https://github.com/espressif/esp-idf/blob/e95cab4be8fd293e3f3323181e7a2280874da6f7/components/esp_wifi/include/esp_now.h#L32-L33) of simultaneously connected drones is 20 (unencrypted) or 6 (encrypted).
3. Set the `WIFI_MODE` parameter to `3` on the drone:
```
p WIFI_MODE 3
```
4. Go to the QGroundControl menu ⇒ *Application Settings* ⇒ *Comm Links*, add new link with the following settings:
* Name: ESP32.
* Type: Serial.
* Serial Port: choose the port of the proxy ESP32 board, e. g. `/dev/cu.usbserial-0001`.
* Baud Rate: 115200.
5. Click *Save*, click *Connect*. QGroundControl should connect to the drone using ESP-NOW and begin showing the telemetry.
> [!TIP]
> Make sure Arduino IDE is not running when using ESP-NOW proxy board, as it may block it.
## Flight log
After the flight, you can download the flight log for analysis wirelessly. Use the following for that:
After the flight, you can download the flight log wirelessly for analysis. Use the following command on your computer for that:
```bash
make log
+96 -2
View File
@@ -4,6 +4,89 @@ This page contains user-built drones based on the Flix project. Publish your pro
---
Author: Alican Erüst.<br>
Description: QX95 mm frame, 55 mm propellers, 3.7 V 25C 1050 mAh LiPo battery, MPU6050 IMU, Logitech F310 gamepad controller, with a total quadcopter weight of 66 g.
<img src="img/user/alicanerus/1.jpg" height=200> <img src="img/user/alicanerus/2.jpg" height=200> <img src="img/user/alicanerus/3.jpg" height=200>
[Flight video](https://drive.google.com/file/d/1k0WeWTKnCAfaugkX7LcmNxsUuq79RL8Z/view?usp=sharing).
---
Author: [Неруш Михаил](https://t.me/NerushMV).<br>
Description: custom frame made of 4 mm plywood, 8520 brushed motors, 75 mm propellers, MPU-6500. FlySky FS-i6X with ESP32-based adapter for ESP-NOW communication (using PPM output).<br>
Sources and materials: [link](https://drive.google.com/drive/folders/1uWiDcuorLrtVs_IIR7Y13omij-7Q1nx8).
<img src="img/user/nerush/1.jpg" height=200> <img src="img/user/nerush/2.jpg" height=200>
[Flight video](https://drive.google.com/file/d/1jRXeGx34lJpUfw0GKLQeIzkWZvooQJSE/view?usp=sharing).
---
Author: [Konstantinos Paraskevas](https://github.com/Frapais).<br>
Description: drone with a custom single-boarded airframe, extending the [Sprig-C3 module](https://github.com/Frapais/Sprig-C3).
ESP32-C3 microcontroller, ICM-20948 IMU, on-board fuel-gauge, status LED indicator.<br>
Repository with all the code and PCB sources: https://github.com/Frapais/Sprig-Drone.
<img src="img/user/kostas/1.jpg" height=150> <img src="img/user/kostas/2.jpg" height=150>
Detailed video about making the drone:
<a href="https://youtu.be/82Q-uBq6s48"><img width=400 src="https://i3.ytimg.com/vi/82Q-uBq6s48/maxresdefault.jpg"></a>
---
Author: [Awab Anas](http://t.me/AW_VENOM).<br>
Description: ESP32 D1 Mini, MPU-6050, 8520 3.7V brushed motors, 55 mm propellers, battery li-po 1200 mAh, controlling via [Mavlink Joystick app](https://github.com/goldarte/mavlink-joystick/releases/latest).<br>
[Flight validation](https://drive.google.com/file/d/12z0jfctZDBA6b5UKCG0Uje5rAxj6DhF-/view?usp=sharing).
<img src="img/user/aw_venom/1.jpg" height=200>
---
Author: [Ina Tix](https://t.me/ina_tix).<br>
Description: XR2981 based DC-DC converter, ELRS MINI 2.4GHz RX SX1280 receiver (SBUS interface), Radiomaster TX12 remote control.<br>
[Flight validation](https://drive.google.com/file/d/1yqkKNuz4R_yxGqUNQxVpixJbXqEEcUSj/view?usp=share_link).
<img src="img/user/ina_tix/1.jpg" height=200> <img src="img/user/ina_tix/2.jpg" height=200> <img src="img/user/ina_tix/3.jpg" height=200>
---
Author: Oleg Kalachev.<br>
Description: the first attempt on making an official PCB based Flix drone (Flix2 board). The IMU is not working on this version, so an external MPU-6050 board was used, therefore considered as **Flix version 1.5**.<br>
[Flight video](https://drive.google.com/file/d/1R7tuUsFmPY0CGcOCFfMFaCp9kR49K3bl/view?usp=sharing).
<img src="img/flix1.5.jpg" width=300>
---
Author: [FanBy0ru](https://https://github.com/FanBy0ru).<br>
Description: custom 3D-printed frame.<br>
Frame STLs and flight validation: https://cults3d.com/en/3d-model/gadget/armature-pour-flix-drone.
<img src="img/user/fanby0ru/1.jpg" height=200> <img src="img/user/fanby0ru/2.jpg" height=200>
---
Author: Ivan44 Phalko.<br>
Description: custom PCB, cusom test bench.<br>
[Flight validation](https://drive.google.com/file/d/17DNDJ1gPmCmDRAwjedCbJ9RXAyqMqqcX/view?usp=sharing).
<img src="img/user/phalko/1.jpg" height=200> <img src="img/user/phalko/2.jpg" height=200> <img src="img/user/phalko/3.jpg" height=200>
---
Author: **Arkadiy "Arky" Matsekh**, Foucault Dynamics, Gold Coast, Australia.<br>
The drone was built for the University of Queensland industry-led Master's capstone project.
**Flight video:**
<a href="https://drive.google.com/file/d/1NNYSVXBY-w0JjCo07D8-PgnVq3ca9plj/view?usp=sharing"><img height=300 src="img/user/arkymatsekh/video.jpg"></a>
<img src="img/user/arkymatsekh/1.jpg" height=150> <img src="img/user/arkymatsekh/2.jpg" height=150> <img src="img/user/arkymatsekh/3.jpg" height=150>
---
Author: [goldarte](https://t.me/goldarte).<br>
<img src="img/user/goldarte/1.jpg" height=150> <img src="img/user/goldarte/2.jpg" height=150>
@@ -14,9 +97,20 @@ Author: [goldarte](https://t.me/goldarte).<br>
---
Author: [malagis](https://oshwhub.com/malagis).<br>
A Chinese custom PCB version of Flix with a big community of users, lots of materials and modifications.
Main project's page: https://oshwhub.com/malagis/esp32-mini-plane.<br>
Video about the project: https://www.bilibili.com/video/BV14vyqBFEJn/.
<img src="img/user/malagis/1.jpg" height=200> <img src="img/user/malagis/2.jpg" height=200> <img src="img/user/malagis/3.jpg" height=200>
---
## School 548 course
Special quadcopter design and engineering course took place in october-november 2025 in School 548, Moscow. Course included UAV control theory, electronics, and practical drone assembly and setup using the Flix project.
Special course on quadcopter design and engineering took place in october-november 2025 in School 548, Moscow. The course included UAV control theory, electronics, drone assembly and setup practice, using the Flix project.
<img height=200 src="img/user/school548/1.jpg"> <img height=200 src="img/user/school548/2.jpg"> <img height=200 src="img/user/school548/3.jpg">
@@ -25,7 +119,7 @@ STL files and other materials: see [here](https://drive.google.com/drive/folders
### Selected works
Author: [KiraFlux](https://t.me/@kiraflux_0XC0000005).<br>
Description: **custom ESPNOW remote control** is implemented, firmware modified to support ESPNOW protocol.<br>
Description: **custom ESPNOW remote control** was implemented, modified firmware to support ESPNOW protocol.<br>
Telegram posts: [1](https://t.me/opensourcequadcopter/106), [2](https://t.me/opensourcequadcopter/114).<br>
Modified Flix firmware: https://github.com/KiraFlux/flix/tree/klyax.<br>
Remote control project: https://github.com/KiraFlux/ESP32-DJC.<br>
+73 -42
View File
@@ -6,58 +6,70 @@
#include "pid.h"
#include "vector.h"
#include "util.h"
#include "filter.h"
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern const int RAW, ACRO, STAB, AUTO;
extern const int RAW, ACRO, STAB, AUTO, POS;
extern const int W_AP, W_STA, W_ESPNOW;
extern float t, dt, loopRate;
extern uint16_t channels[16];
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
extern float controlTime;
extern int mode;
extern bool armed;
extern LowPassFilter<Vector> gyroBiasFilter;
extern float voltage;
const char* motd =
"\nWelcome to\n"
" _______ __ __ ___ ___\n"
"| ____|| | | | \\ \\ / /\n"
"| |__ | | | | \\ V /\n"
"| __| | | | | > <\n"
"| | | `----.| | / . \\\n"
"|__| |_______||__| /__/ \\__\\\n\n"
"(C) Oleg Kalachev\n"
"https://github.com/okalachev/flix\n\n"
"Commands:\n\n"
"help - show help\n"
"p - show all parameters\n"
"p <name> - show parameter\n"
"p <str> - show parameters starting with str\n"
"p <name> <value> - set parameter\n"
"preset - reset parameters\n"
"time - show time info\n"
"ps - show pitch/roll/yaw\n"
"psq - show attitude quaternion\n"
"imu - show IMU data\n"
"ca - calibrate accel\n"
"st - show state estimation\n"
"arm - arm the drone\n"
"disarm - disarm the drone\n"
"raw/stab/acro/auto - set mode\n"
"rc - show RC data\n"
"wifi - show Wi-Fi info\n"
"mot - show motor output\n"
"log [dump] - print log header [and data]\n"
"cr - calibrate RC\n"
"ca - calibrate accel\n"
"cl - calibrate level\n"
"mfr, mfl, mrr, mrl - test motor (remove props)\n"
"pw - show power info\n"
"wifi - show Wi-Fi info\n"
"wifi ap/sta/espnow/off - set Wi-Fi mode\n"
"ap <ssid> <password> - configure Wi-Fi access point\n"
"sta <ssid> <password> - configure Wi-Fi client mode\n"
"espnow <mac> [<key>] - configure ESP-NOW peer\n"
"mot - show motor output\n"
"mfr/mfl/mrr/mrl [<thrust>] - test motor (remove props)\n"
"log [dump] - print log header [and data]\n"
"log - show log info\n"
"log header - show log header\n"
"log reset - reset log\n"
"log <name> <rate> - setup log topic rate\n"
"l <str> - show log values starting with str\n"
"l expose <name> - expose log value to telemetry\n"
"sys - show system info\n"
"reset - reset drone's state\n"
"reboot - reboot the drone\n";
void print(const char* format, ...) {
char buf[1000];
char buf[3000];
va_list args;
va_start(args, format);
vsnprintf(buf, sizeof(buf), format, args);
va_end(args);
Serial.print(buf);
#if WIFI_ENABLED
mavlinkPrint(buf);
#endif
}
void pause(float duration) {
@@ -65,9 +77,7 @@ void pause(float duration) {
while (t - start < duration) {
step();
handleInput();
#if WIFI_ENABLED
processMavlink();
#endif
delay(50);
}
}
@@ -88,14 +98,12 @@ void doCommand(String str, bool echo = false) {
// execute command
if (command == "help" || command == "motd") {
print("%s\n", motd);
} else if (command == "p" && arg0 == "") {
printParameters();
} else if (command == "p" && arg0 != "" && arg1 == "") {
print("%s = %g\n", arg0.c_str(), getParameter(arg0.c_str()));
} else if (command == "p" && arg1 == "") {
printParameters(arg0.c_str());
} else if (command == "p") {
bool success = setParameter(arg0.c_str(), arg1.toFloat());
if (success) {
print("%s = %g\n", arg0.c_str(), arg1.toFloat());
print("%s = %g\n", arg0.c_str(), getParameter(arg0.c_str()));
} else {
print("Parameter not found: %s\n", arg0.c_str());
}
@@ -105,15 +113,15 @@ void doCommand(String str, bool echo = false) {
print("Time: %f\n", t);
print("Loop rate: %.0f\n", loopRate);
print("dt: %f\n", dt);
} else if (command == "ps") {
Vector a = attitude.toEuler();
print("roll: %f pitch: %f yaw: %f\n", degrees(a.x), degrees(a.y), degrees(a.z));
} else if (command == "psq") {
print("qw: %f qx: %f qy: %f qz: %f\n", attitude.w, attitude.x, attitude.y, attitude.z);
} else if (command == "imu") {
printIMUInfo();
printIMUCalibration();
print("landed: %d\n", landed);
} else if (command == "st") {
print("rates: %g %g %g\n", rates.x, rates.y, rates.z);
print("attitude: %g %g %g %g\n", attitude.w, attitude.x, attitude.y, attitude.z);
print("roll: %g° pitch: %g° yaw: %g°\n", degrees(attitude.getRoll()), degrees(attitude.getPitch()), degrees(attitude.getYaw()));
print("landed: %d\n", landed);
} else if (command == "arm") {
armed = true;
} else if (command == "disarm") {
@@ -126,6 +134,8 @@ void doCommand(String str, bool echo = false) {
mode = ACRO;
} else if (command == "auto") {
mode = AUTO;
} else if (command == "pos") {
mode = POS;
} else if (command == "rc") {
print("channels: ");
for (int i = 0; i < 16; i++) {
@@ -133,39 +143,59 @@ void doCommand(String str, bool echo = false) {
}
print("\nroll: %g pitch: %g yaw: %g throttle: %g mode: %g\n",
controlRoll, controlPitch, controlYaw, controlThrottle, controlMode);
print("time: %.1f\n", controlTime);
print("mode: %s\n", getModeName());
print("armed: %d\n", armed);
} else if (command == "wifi") {
#if WIFI_ENABLED
} else if (command == "pw") {
print("Voltage: %.1f V\n", voltage);
} else if (command == "wifi" && arg0 == "") {
printWiFiInfo();
#endif
} else if (command == "wifi") {
setWiFiMode(arg0);
} else if (command == "ap") {
configWiFi(W_AP, arg0.c_str(), arg1.c_str());
} else if (command == "sta") {
configWiFi(W_STA, arg0.c_str(), arg1.c_str());
} else if (command == "espnow") {
configWiFi(W_ESPNOW, arg0.c_str(), arg1.c_str());
} else if (command == "mot") {
print("front-right %g front-left %g rear-right %g rear-left %g\n",
motors[MOTOR_FRONT_RIGHT], motors[MOTOR_FRONT_LEFT], motors[MOTOR_REAR_RIGHT], motors[MOTOR_REAR_LEFT]);
} else if (command == "log") {
} else if (command == "log" && arg0 == "") {
printLogInfo();
} else if (command == "log" && arg1 != "") {
configLogThrottle(arg0.c_str(), arg1.toFloat());
} else if (command == "log" && arg0 == "header") {
printLogHeader();
if (arg0 == "dump") printLogData();
} else if (command == "log" && arg0 == "reset") {
resetLog();
} else if (command == "l" && arg0 == "expose" && arg1 != "") {
exposeLogValue(arg1.c_str());
} else if (command == "l") {
printLogValues(arg0.c_str());
} else if (command == "cr") {
calibrateRC();
} else if (command == "ca") {
calibrateAccel();
} else if (command == "cl") {
calibrateLevel();
} else if (command == "mfr") {
testMotor(MOTOR_FRONT_RIGHT);
testMotor(MOTOR_FRONT_RIGHT, arg0.isEmpty() ? 0.2 : arg0.toFloat());
} else if (command == "mfl") {
testMotor(MOTOR_FRONT_LEFT);
testMotor(MOTOR_FRONT_LEFT, arg0.isEmpty() ? 0.2 : arg0.toFloat());
} else if (command == "mrr") {
testMotor(MOTOR_REAR_RIGHT);
testMotor(MOTOR_REAR_RIGHT, arg0.isEmpty() ? 0.2 : arg0.toFloat());
} else if (command == "mrl") {
testMotor(MOTOR_REAR_LEFT);
testMotor(MOTOR_REAR_LEFT, arg0.isEmpty() ? 0.2 : arg0.toFloat());
} else if (command == "sys") {
#ifdef ESP32
print("Chip: %s\n", ESP.getChipModel());
print("Temperature: %.1f °C\n", temperatureRead());
print("Free heap: %d\n", ESP.getFreeHeap());
print("Total RAM: %d KB\n", ESP.getHeapSize() / 1024);
print("Free heap: %d KB\n", ESP.getFreeHeap() / 1024);
print("PSRAM: %d KB\n", ESP.getPsramSize() / 1024);
print("Free PSRAM: %d KB\n", ESP.getFreePsram() / 1024);
print("Firmware: " __DATE__ " " __TIME__ "\n");
// Print tasks table
print("Num Task Stack Prio Core CPU%%\n");
print("Num Task MinSt Prio Core CPU%%\n");
int taskCount = uxTaskGetNumberOfTasks();
TaskStatus_t *systemState = new TaskStatus_t[taskCount];
uint32_t totalRunTime;
@@ -174,12 +204,13 @@ void doCommand(String str, bool echo = false) {
String core = systemState[i].xCoreID == tskNO_AFFINITY ? "*" : String(systemState[i].xCoreID);
int cpuPercentage = systemState[i].ulRunTimeCounter / (totalRunTime / 100);
print("%-5d%-20s%-7d%-6d%-6s%d\n",systemState[i].xTaskNumber, systemState[i].pcTaskName,
systemState[i].usStackHighWaterMark, systemState[i].uxCurrentPriority, core, cpuPercentage);
systemState[i].usStackHighWaterMark, systemState[i].uxCurrentPriority, core.c_str(), cpuPercentage);
}
delete[] systemState;
#endif
} else if (command == "reset") {
attitude = Quaternion();
gyroBiasFilter.reset();
} else if (command == "reboot") {
ESP.restart();
} else {
@@ -198,7 +229,7 @@ void handleInput() {
while (Serial.available()) {
char c = Serial.read();
if (c == '\n') {
if (c == '\n' || c == '\r') {
doCommand(input);
input.clear();
} else {
+39 -12
View File
@@ -6,7 +6,7 @@
#include "vector.h"
#include "quaternion.h"
#include "pid.h"
#include "lpf.h"
#include "filter.h"
#include "util.h"
#define PITCHRATE_P 0.05
@@ -34,10 +34,16 @@
#define TILT_MAX radians(30)
#define RATES_D_LPF_ALPHA 0.2 // cutoff frequency ~ 40 Hz
const int RAW = 0, ACRO = 1, STAB = 2, AUTO = 3; // flight modes
const int RAW = 0, ACRO = 1, STAB = 2, AUTO = 3, POS = 4;
int mode = STAB;
bool armed = false;
Quaternion attitudeTarget;
Vector ratesTarget;
Vector ratesExtra; // feedforward rates
Vector torqueTarget;
float thrustTarget;
PID rollRatePID(ROLLRATE_P, ROLLRATE_I, ROLLRATE_D, ROLLRATE_I_LIM, RATES_D_LPF_ALPHA);
PID pitchRatePID(PITCHRATE_P, PITCHRATE_I, PITCHRATE_D, PITCHRATE_I_LIM, RATES_D_LPF_ALPHA);
PID yawRatePID(YAWRATE_P, YAWRATE_I, YAWRATE_D);
@@ -46,15 +52,11 @@ PID pitchPID(PITCH_P, PITCH_I, PITCH_D);
PID yawPID(YAW_P, 0, 0);
Vector maxRate(ROLLRATE_MAX, PITCHRATE_MAX, YAWRATE_MAX);
float tiltMax = TILT_MAX;
Quaternion attitudeTarget;
Vector ratesTarget;
Vector ratesExtra; // feedforward rates
Vector torqueTarget;
float thrustTarget;
int flightModes[] = {STAB, STAB, STAB}; // map for rc mode switch
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
extern Vector position, positionTarget;
void control() {
interpretControls();
@@ -65,9 +67,9 @@ void control() {
}
void interpretControls() {
if (controlMode < 0.25) mode = STAB;
if (controlMode < 0.75) mode = STAB;
if (controlMode > 0.75) mode = STAB;
if (controlMode < 0.25) mode = flightModes[0];
else if (controlMode <= 0.75) mode = flightModes[1];
else if (controlMode > 0.75) mode = flightModes[2];
if (mode == AUTO) return; // pilot is not effective in AUTO mode
@@ -78,7 +80,18 @@ void interpretControls() {
thrustTarget = controlThrottle;
if (mode == STAB) {
if (mode == POS) {
if (controlRoll != 0 || controlPitch != 0) {
positionTarget.x = NAN;
positionTarget.y = NAN;
} else if (invalid(positionTarget.x) || invalid(positionTarget.y)) {
// reset position target
positionTarget.x = position.x;
positionTarget.y = position.y;
}
}
if (mode == STAB || (mode == POS && invalid(positionTarget.x))) {
float yawTarget = attitudeTarget.getYaw();
if (!armed || invalid(yawTarget) || controlYaw != 0) yawTarget = attitude.getYaw(); // reset yaw target
attitudeTarget = Quaternion::fromEuler(Vector(controlRoll * tiltMax, controlPitch * tiltMax, yawTarget));
@@ -148,12 +161,26 @@ void controlTorque() {
motors[MOTOR_REAR_LEFT] = thrustTarget + torqueTarget.x + torqueTarget.y - torqueTarget.z;
motors[MOTOR_REAR_RIGHT] = thrustTarget - torqueTarget.x + torqueTarget.y + torqueTarget.z;
// Prioritize angle control over thrust control
desaturate(motors[MOTOR_FRONT_LEFT], motors[MOTOR_FRONT_RIGHT], motors[MOTOR_REAR_LEFT], motors[MOTOR_REAR_RIGHT]);
motors[0] = constrain(motors[0], 0, 1);
motors[1] = constrain(motors[1], 0, 1);
motors[2] = constrain(motors[2], 0, 1);
motors[3] = constrain(motors[3], 0, 1);
}
void desaturate(float& a, float& b, float& c, float& d) {
float maxThrust = max(max(a, b), max(c, d));
if (maxThrust > 1) {
float diff = maxThrust - 1;
a -= diff;
b -= diff;
c -= diff;
d -= diff;
}
}
const char* getModeName() {
switch (mode) {
case RAW: return "RAW";
+27 -4
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@@ -1,24 +1,38 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Attitude estimation from gyro and accelerometer
// Attitude estimation using gyro and accelerometer
#include "quaternion.h"
#include "vector.h"
#include "lpf.h"
#include "filter.h"
#include "util.h"
Vector rates; // estimated angular rates, rad/s
Quaternion attitude; // estimated attitude
bool landed;
float accWeight = 0.003;
float levelWeight = 0.0002;
LowPassFilter<Vector> ratesFilter(0.2); // cutoff frequency ~ 40 Hz
NotchFilter<Vector> ratesNotch(382, 0);
void setupEstimate() {
print("Setup estimation\n");
ratesNotch.reset();
}
void estimate() {
applyGyro();
applyAcc();
applyLevel();
estimatePosition();
}
void applyGyro() {
// filter gyro to get angular rates
rates = ratesFilter.update(gyro);
rates = ratesNotch.update(rates);
// apply rates to attitude
attitude = Quaternion::rotate(attitude, Quaternion::fromRotationVector(rates * dt));
@@ -26,8 +40,7 @@ void applyGyro() {
void applyAcc() {
// test should we apply accelerometer gravity correction
float accNorm = acc.norm();
landed = !motorsActive() && abs(accNorm - ONE_G) < ONE_G * 0.1f;
landed = !motorsActive() && abs(acc.norm() - ONE_G) < ONE_G * 0.1f;
if (!landed) return;
@@ -38,3 +51,13 @@ void applyAcc() {
// apply correction
attitude = Quaternion::rotate(attitude, Quaternion::fromRotationVector(correction));
}
void applyLevel() {
if (landed) return;
if (thrustTarget < 0.1) return; // skip at idle thrust
// assume the pilot keeps the drone more or less level in flight
Vector up = Quaternion::rotateVector(Vector(0, 0, 1), attitude);
Vector correction = Vector::rotationVectorBetween(Vector(0, 0, 1), up) * levelWeight;
attitude = Quaternion::rotate(attitude, Quaternion::fromRotationVector(correction));
}
+98
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@@ -0,0 +1,98 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Low pass and notch filters
#pragma once
template <typename T> // Using template to make the filter usable for scalar and vector values
class LowPassFilter {
public:
float alpha; // smoothing constant, 1 means filter disabled
T output;
LowPassFilter(float alpha): alpha(alpha) {};
T update(const T input) {
if (!init) {
init = true;
return output = input;
}
return output += alpha * (input - output);
}
void setCutOffFrequency(float cutOffFreq, float dt) {
alpha = 1 - exp(-2 * PI * cutOffFreq * dt);
}
void reset() {
init = false;
}
private:
bool init = false;
};
template <typename T>
class NotchFilter {
public:
float frequency;
float bandwidth;
T output;
NotchFilter(float frequency, float bandwidth): frequency(frequency), bandwidth(bandwidth) {
reset();
};
T update(const T input) {
if (frequency <= 0 || bandwidth <= 0) return input;
if (!init) {
init = true;
x1 = x2 = input;
y1 = y2 = input;
return output = input;
}
output = b0 * input + b1 * x1 + b2 * x2 - a1 * y1 - a2 * y2;
x2 = x1;
x1 = input;
y2 = y1;
y1 = output;
return output;
}
void reset() {
const float dt = 0.001f;
float f = frequency;
float bw = bandwidth;
if (f < 0) f = 0;
if (bw < 1e-6f) bw = 1e-6f;
float q = f / bw;
if (q < 1e-3f) q = 1e-3f;
const float w0 = 2.0f * PI * f * dt;
const float c = cos(w0);
const float s = sin(w0);
const float alpha = s / (2.0f * q);
const float a0 = 1.0f + alpha;
const float invA0 = 1.0f / a0;
b0 = 1.0f * invA0;
b1 = -2.0f * c * invA0;
b2 = 1.0f * invA0;
a1 = -2.0f * c * invA0;
a2 = (1.0f - alpha) * invA0;
init = false;
}
private:
float b0, b1, b2, a1, a2;
T x1, x2, y1, y2;
bool init = false;
};
+14 -20
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@@ -7,32 +7,27 @@
#include "quaternion.h"
#include "util.h"
#define WIFI_ENABLED 1
float t = NAN; // current step time, s
float dt; // time delta from previous step, s
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
float controlMode = NAN;
Vector gyro; // gyroscope data
Vector acc; // accelerometer data, m/s/s
Vector rates; // filtered angular rates, rad/s
Quaternion attitude; // estimated attitude
bool landed; // are we landed and stationary
float motors[4]; // normalized motors thrust in range [0..1]
extern float t, dt;
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
extern Vector gyro, acc;
extern Vector rates;
extern Quaternion attitude;
extern bool landed;
extern float motors[4];
void setup() {
Serial.begin(115200);
print("Initializing flix\n");
disableBrownOut();
print("Initializing Flix\n");
setupParameters();
setupPower();
setupLED();
setupMotors();
setLED(true);
#if WIFI_ENABLED
setupMotors();
setupWiFi();
#endif
setupIMU();
setupRC();
setupEstimate();
setupLog();
setLED(false);
print("Initializing complete\n");
}
@@ -45,9 +40,8 @@ void loop() {
control();
sendMotors();
handleInput();
#if WIFI_ENABLED
processMavlink();
#endif
logData();
readVoltage();
loopLog();
syncParameters();
}
+15 -15
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@@ -6,15 +6,20 @@
#include <SPI.h>
#include <FlixPeriph.h>
#include "vector.h"
#include "lpf.h"
#include "filter.h"
#include "util.h"
MPU9250 imu(SPI);
Vector imuRotation(0, 0, -PI / 2); // imu orientation as Euler angles
Vector imuRotation(0, 0, PI / 2); // imu orientation as Euler angles
Vector gyro; // gyroscope output, rad/s
Vector gyroBias;
Vector acc; // accelerometer output, m/s/s
Vector accBias;
Vector accScale(1, 1, 1);
Vector gyroBias;
LowPassFilter<Vector> gyroBiasFilter(0.001);
void setupIMU() {
print("Setup IMU\n");
@@ -35,10 +40,12 @@ void readIMU() {
imu.getGyro(gyro.x, gyro.y, gyro.z);
imu.getAccel(acc.x, acc.y, acc.z);
calibrateGyroOnce();
// apply scale and bias
// Apply scale and bias
acc = (acc - accBias) / accScale;
gyro = gyro - gyroBias;
// rotate to body frame
// Rotate to body frame
Quaternion rotation = Quaternion::fromEuler(imuRotation);
acc = Quaternion::rotateVector(acc, rotation.inversed());
gyro = Quaternion::rotateVector(gyro, rotation.inversed());
@@ -48,7 +55,6 @@ void calibrateGyroOnce() {
static Delay landedDelay(2);
if (!landedDelay.update(landed)) return; // calibrate only if definitely stationary
static LowPassFilter<Vector> gyroBiasFilter(0.001);
gyroBias = gyroBiasFilter.update(gyro);
}
@@ -102,19 +108,12 @@ void calibrateAccelOnce() {
if (acc.x < accMin.x) accMin.x = acc.x;
if (acc.y < accMin.y) accMin.y = acc.y;
if (acc.z < accMin.z) accMin.z = acc.z;
// Compute scale and bias
accScale = (accMax - accMin) / 2 / ONE_G;
accBias = (accMax + accMin) / 2;
}
void calibrateLevel() {
print("Place perfectly level [1 sec]\n");
pause(1);
Quaternion correction = Quaternion::fromBetweenVectors(Quaternion::rotateVector(Vector(0, 0, 1), attitude), Vector(0, 0, 1));
imuRotation = Quaternion::rotate(correction, Quaternion::fromEuler(imuRotation)).toEuler();
print("✓ Done: %.3f %.3f %.3f\n", degrees(imuRotation.x), degrees(imuRotation.y), degrees(imuRotation.z));
}
void printIMUCalibration() {
print("gyro bias: %f %f %f\n", gyroBias.x, gyroBias.y, gyroBias.z);
print("accel bias: %f %f %f\n", accBias.x, accBias.y, accBias.z);
@@ -126,7 +125,8 @@ void printIMUInfo() {
print("model: %s\n", imu.getModel());
print("who am I: 0x%02X\n", imu.whoAmI());
print("rate: %.0f\n", loopRate);
print("gyro: %f %f %f\n", rates.x, rates.y, rates.z);
print("temperature: %.1f °C\n", imu.getTemp());
print("gyro: %f %f %f\n", gyro.x, gyro.y, gyro.z);
print("acc: %f %f %f\n", acc.x, acc.y, acc.z);
imu.waitForData();
Vector rawGyro, rawAcc;
+252 -52
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@@ -1,77 +1,277 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// In-RAM logging
// Logging subsystem
#include "vector.h"
#include "util.h"
#define LOG_RATE 100
#define LOG_DURATION 10
#define LOG_SIZE LOG_DURATION * LOG_RATE
int logMemory = -1; // 0 - RAM, 1 - PSRAM, -1 - disabled
float logUsage = 0.5; // fraction of free memory to use for log
Vector attitudeEuler;
Vector attitudeTargetEuler;
struct LogEntry {
struct LogValue {
const char *name;
float *value;
Value value;
float lastValue = NAN;
bool logged = true; // if false, use only for triggering log update
LogValue() : name(nullptr), value() {}; // empty value constructor
template <typename T>
LogValue(const char *name, T value, bool logged = true) : name(name), value(value), logged(logged) {};
};
LogEntry logEntries[] = {
{"t", &t},
{"rates.x", &rates.x},
{"rates.y", &rates.y},
{"rates.z", &rates.z},
{"ratesTarget.x", &ratesTarget.x},
{"ratesTarget.y", &ratesTarget.y},
{"ratesTarget.z", &ratesTarget.z},
{"attitude.x", &attitudeEuler.x},
{"attitude.y", &attitudeEuler.y},
{"attitude.z", &attitudeEuler.z},
{"attitudeTarget.x", &attitudeTargetEuler.x},
{"attitudeTarget.y", &attitudeTargetEuler.y},
{"attitudeTarget.z", &attitudeTargetEuler.z},
{"thrustTarget", &thrustTarget}
struct LogTopic {
LogValue values[10];
int length = 0; // number of logged values
float throttle; // max update rate, Hz
float lastUpdate = -INFINITY;
LogTopic(float throttle, LogValue v0, LogValue v1 = {}, LogValue v2 = {}, LogValue v3 = {}, LogValue v4 = {}, LogValue v5 = {}, LogValue v6 = {}, LogValue v7 = {}, LogValue v8 = {}, LogValue v9 = {}) :
throttle(throttle), values{v0, v1, v2, v3, v4, v5, v6, v7, v8, v9} {
// Count logged values
for (auto& v : values) {
if (v.name == nullptr) break;
if (v.logged) length++;
}
};
LogTopic(LogValue v0, LogValue v1 = {}, LogValue v2 = {}, LogValue v3 = {}, LogValue v4 = {}, LogValue v5 = {}, LogValue v6 = {}, LogValue v7 = {}, LogValue v8 = {}, LogValue v9 = {}) :
LogTopic(INFINITY, v0, v1, v2, v3, v4, v5, v6, v7, v8, v9) {};
};
const int logColumns = sizeof(logEntries) / sizeof(logEntries[0]);
float logBuffer[LOG_SIZE][logColumns];
LogTopic logTopics[] = {
// time
LogTopic({"t", &t}), // must be the first topic
LogTopic(1, {"loopRate", &loopRate}),
void prepareLogData() {
attitudeEuler = attitude.toEuler();
attitudeTargetEuler = attitudeTarget.toEuler();
}
// imu
LogTopic(
{"gyro.x", &gyro.x},
{"gyro.y", &gyro.y},
{"gyro.z", &gyro.z}),
void logData() {
if (!armed) return;
static int logPointer = 0;
static Rate period(LOG_RATE);
if (!period) return;
LogTopic(50,
{"acc.x", &acc.x},
{"acc.y", &acc.y},
{"acc.z", &acc.z}),
prepareLogData();
LogTopic(10,
{"gyroBias.x", &gyroBias.x},
{"gyroBias.y", &gyroBias.y},
{"gyroBias.z", &gyroBias.z}),
for (int i = 0; i < logColumns; i++) {
logBuffer[logPointer][i] = *logEntries[i].value;
}
// estimation
LogTopic(50,
{"rates.x", &rates.x},
{"rates.y", &rates.y},
{"rates.z", &rates.z},
{"attitude.roll", []() { return attitude.getRoll(); }},
{"attitude.pitch", []() { return attitude.getPitch(); }},
{"attitude.yaw", []() { return attitude.getYaw(); }}),
logPointer++;
if (logPointer >= LOG_SIZE) {
logPointer = 0;
LogTopic(50,
{"position.x", &position.x},
{"position.y", &position.y},
{"position.z", &position.z}),
// rc
LogTopic(10,
{"controlTime", &controlTime, false}, // trigger value
{"controlRoll", &controlRoll},
{"controlPitch", &controlPitch},
{"controlYaw", &controlYaw},
{"controlThrottle", &controlThrottle}),
// control
LogTopic({"armed", &armed}),
LogTopic({"mode", &mode}),
LogTopic(10,
{"ratesTarget.x", &ratesTarget.x},
{"ratesTarget.y", &ratesTarget.y},
{"ratesTarget.z", &ratesTarget.z},
{"attitudeTarget.roll", []() { return attitudeTarget.getRoll(); }},
{"attitudeTarget.pitch", []() { return attitudeTarget.getPitch(); }},
{"attitudeTarget.yaw", []() { return attitudeTarget.getYaw(); }},
{"thrustTarget", &thrustTarget}),
// motors
LogTopic(
{"motors[0]", &motors[0]},
{"motors[1]", &motors[1]},
{"motors[2]", &motors[2]},
{"motors[3]", &motors[3]}),
// misc
LogTopic(5,
{"voltage", &voltage},
{"temp", &temperatureRead},
{"imuTemp", []() { return imu.getTemp(); }}),
};
void *logBuffer; // buffer for log data
size_t logCapacity;
size_t logCursor = 0;
size_t logLength = 0;
LogValue *logExposed = nullptr; // log values exposed to telemetry
void setupLog() {
print("Setup log\n");
free(logBuffer); // when reconfiguring
logBuffer = nullptr;
logCursor = 0;
logLength = 0;
if (logMemory == 0) {
logCapacity = ESP.getFreeHeap() * logUsage;
logBuffer = (uint8_t *)calloc(logCapacity, 1);
} else if (logMemory == 1) {
logCapacity = ESP.getFreePsram() * logUsage;
logBuffer = (uint8_t *)heap_caps_calloc(logCapacity, 1, MALLOC_CAP_SPIRAM | MALLOC_CAP_8BIT);
}
}
void printLogHeader() {
for (int i = 0; i < logColumns; i++) {
print("%s%s", logEntries[i].name, i < logColumns - 1 ? "," : "\n");
}
}
void loopLog() {
if (logBuffer == nullptr || !armed) return;
void printLogData() {
for (int i = 0; i < LOG_SIZE; i++) {
if (logBuffer[i][0] == 0) continue; // skip empty records
for (int j = 0; j < logColumns; j++) {
print("%g%s", logBuffer[i][j], j < logColumns - 1 ? "," : "\n");
if (!logLength) resetLog(); // reset state on first log write
static Rate sync(2);
if (sync) {
const uint8_t marker[] = {0x1A, 0x91, 0x4F, 0xF6, 0x7F};
writeLog(&marker, sizeof(marker)); // write sync marker
}
for (uint8_t i = 0; i < sizeof(logTopics) / sizeof(logTopics[0]); i++) {
LogTopic& topic = logTopics[i];
if (t - topic.lastUpdate < 1 / topic.throttle) continue; // throttle topic
if (!isTopicUpdated(i)) continue; // skip if topic was't updated
topic.lastUpdate = t;
writeLog(&i, sizeof(i)); // write topic index
for (auto& value : topic.values) {
if (value.name == nullptr) break;
if (!value.logged) continue;
value.lastValue = value.value.get();
writeLog(&value.lastValue, sizeof(float)); // write value
}
}
}
void resetLog() {
for (auto& topic : logTopics) {
topic.lastUpdate = -INFINITY;
for (auto& value : topic.values) {
value.lastValue = NAN;
}
}
logCursor = 0;
logLength = 0;
}
void writeLog(const void *data, size_t size) {
size_t first = min(size, logCapacity - logCursor);
size_t second = size - first;
memcpy(logBuffer + logCursor, data, first);
logCursor = (logCursor + first) % logCapacity;
if (second > 0) {
memcpy(logBuffer + logCursor, data + first, second);
logCursor = (logCursor + second) % logCapacity;
}
logLength = min(logLength + size, logCapacity);
}
void readLog(void *data, size_t position, size_t size) {
if (logLength == logCapacity) {
position = (logCursor + position) % logCapacity;
}
size_t first = min(size, logCapacity - position);
size_t second = size - first;
memcpy(data, logBuffer + position, first);
if (second > 0) {
memcpy(data + first, logBuffer, second);
}
}
bool isTopicUpdated(const uint8_t topic) {
LogTopic& logTopic = logTopics[topic];
bool updated = false;
for (auto& value : logTopic.values) {
if (value.name == nullptr) break;
float v = value.value.get();
if (!floatEquals(value.lastValue, v)) {
value.lastValue = v;
updated = true;
}
}
return updated;
}
void printLogInfo() {
if (logMemory == -1) return print("Log: disabled\n");
print("Memory: %s\n", logMemory == 0 ? "RAM" : "PSRAM");
print("Usage: %.f%%\n", logUsage * 100);
print("Capacity: %u bytes\n", (unsigned)logCapacity);
print("Used: %u bytes\n", (unsigned)logLength);
print("Estimated duration: %d seconds\n", estimateLogDuration());
}
int estimateLogDuration() {
float bandwidth = 0;
for (LogTopic& topic : logTopics) {
float rate = isinf(topic.throttle) ? loopRate : topic.throttle;
bandwidth += rate * topic.length * sizeof(float);
}
return logCapacity / bandwidth;
}
void printLogHeader() {
int i = 0;
for (auto& topic : logTopics) {
print("Topic #%d (%g Hz):\n", i++, topic.throttle);
for (auto& value : topic.values) {
if (value.name == nullptr) break;
print(" %s%s\n", value.name, value.logged ?"" : " (not logged)");
}
}
}
void printLogValues(const char *filter) {
for (LogTopic& topic : logTopics) {
for (LogValue& value : topic.values) {
if (value.name == nullptr) break;
if (strncasecmp(value.name, filter, strlen(filter))) continue;
print("%s = %g\n", value.name, value.value.get());
}
}
}
void configLogThrottle(const char *name, float throttle) {
for (LogTopic& topic : logTopics) {
for (LogValue& value : topic.values) {
if (value.name == nullptr) break;
if (strcasecmp(value.name, name) != 0) continue;
topic.throttle = throttle;
print("Log throttle for %s set to %.1f Hz\n", name, throttle);
return;
}
}
print("Log value not found: %s\n", name);
}
void exposeLogValue(const char *name) {
for (int i = 0; i < sizeof(logTopics) / sizeof(logTopics[0]); i++) {
LogTopic& topic = logTopics[i];
for (LogValue& value : topic.values) {
if (value.name == nullptr) break;
if (strcasecmp(value.name, name) != 0) continue;
logExposed = &value;
print("Log value %s exposed\n", name);
return;
}
}
print("Log value not found: %s\n", name);
}
-39
View File
@@ -1,39 +0,0 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Low pass filter implementation
#pragma once
template <typename T> // Using template to make the filter usable for scalar and vector values
class LowPassFilter {
public:
float alpha; // smoothing constant, 1 means filter disabled
T output;
LowPassFilter(float alpha): alpha(alpha) {};
T update(const T input) {
if (alpha == 1) { // filter disabled
return input;
}
if (!initialized) {
output = input;
initialized = true;
}
return output += alpha * (input - output);
}
void setCutOffFrequency(float cutOffFreq, float dt) {
alpha = 1 - exp(-2 * PI * cutOffFreq * dt);
}
void reset() {
initialized = false;
}
private:
bool initialized = false;
};
+130 -63
View File
@@ -3,21 +3,24 @@
// MAVLink communication
#if WIFI_ENABLED
#include <MAVLink.h>
#include "util.h"
#define SYSTEM_ID 1
#define MAVLINK_RATE_SLOW 1
#define MAVLINK_RATE_FAST 10
extern float controlTime;
extern float voltage;
int mavlinkSysId = 1;
Rate telemetrySlow(2);
Rate telemetryAttitude(20);
Rate telemetryRC(10);
Rate telemetryMotors(10);
Rate telemetryIMU(15);
Rate telemetryTopic(10);
bool mavlinkConnected = false;
String mavlinkPrintBuffer;
extern float controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
void processMavlink() {
sendMavlink();
receiveMavlink();
@@ -29,44 +32,65 @@ void sendMavlink() {
mavlink_message_t msg;
uint32_t time = t * 1000;
static Rate slow(MAVLINK_RATE_SLOW), fast(MAVLINK_RATE_FAST);
if (slow) {
mavlink_msg_heartbeat_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, MAV_TYPE_QUADROTOR, MAV_AUTOPILOT_GENERIC,
if (telemetrySlow) {
mavlink_msg_heartbeat_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, MAV_TYPE_QUADROTOR, MAV_AUTOPILOT_GENERIC,
(armed ? MAV_MODE_FLAG_SAFETY_ARMED : 0) |
((mode == STAB) ? MAV_MODE_FLAG_STABILIZE_ENABLED : 0) |
((mode == AUTO) ? MAV_MODE_FLAG_AUTO_ENABLED : MAV_MODE_FLAG_MANUAL_INPUT_ENABLED),
mode, MAV_STATE_STANDBY);
sendMessage(&msg);
}
if (!mavlinkConnected) return; // send only heartbeat until connected
if (!mavlinkConnected) return; // send only heartbeat until connected
mavlink_msg_extended_sys_state_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
if (telemetrySlow) {
mavlink_msg_extended_sys_state_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
MAV_VTOL_STATE_UNDEFINED, landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR);
sendMessage(&msg);
}
if (fast && mavlinkConnected) {
const float zeroQuat[] = {0, 0, 0, 0};
mavlink_msg_attitude_quaternion_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
time, attitude.w, attitude.x, -attitude.y, -attitude.z, rates.x, -rates.y, -rates.z, zeroQuat); // convert to frd
if (telemetrySlow && valid(voltage)) {
uint16_t voltages[] = {(uint16_t)(voltage * 1000), UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX};
uint16_t voltagesExt[] = {0, 0, 0, 0};
float remaining = constrain(mapf(voltage, 3.4, 4.2, 0, 1), 0, 1);
mavlink_msg_battery_status_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, 0, MAV_BATTERY_FUNCTION_ALL,
MAV_BATTERY_TYPE_LIPO, INT16_MAX, voltages, -1, -1, -1, remaining * 100, 0, MAV_BATTERY_CHARGE_STATE_OK, voltagesExt, 0, 0);
sendMessage(&msg);
}
mavlink_msg_rc_channels_raw_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, controlTime * 1000, 0,
if (telemetryAttitude) {
const float offset[] = {0, 0, 0, 0};
mavlink_msg_attitude_quaternion_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
time, attitude.w, attitude.x, -attitude.y, -attitude.z, rates.x, -rates.y, -rates.z, offset); // convert to frd
sendMessage(&msg);
}
if (telemetryRC && channels[0]) { // 0 means no RC input
mavlink_msg_rc_channels_raw_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, controlTime * 1000, 0,
channels[0], channels[1], channels[2], channels[3], channels[4], channels[5], channels[6], channels[7], UINT8_MAX);
if (channels[0] != 0) sendMessage(&msg); // 0 means no RC input
sendMessage(&msg);
}
if (telemetryMotors) {
float controls[8];
memcpy(controls, motors, sizeof(motors));
mavlink_msg_actuator_control_target_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time, 0, controls);
mavlink_msg_actuator_control_target_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, time, 0, controls);
sendMessage(&msg);
}
mavlink_msg_scaled_imu_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time,
acc.x * 1000, -acc.y * 1000, -acc.z * 1000, // convert to frd
if (telemetryIMU) {
mavlink_msg_scaled_imu_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, time,
acc.x / ONE_G * 1000, -acc.y / ONE_G * 1000, -acc.z / ONE_G * 1000, // convert to frd
gyro.x * 1000, -gyro.y * 1000, -gyro.z * 1000,
0, 0, 0, 0);
sendMessage(&msg);
}
if (telemetryTopic && logExposed != nullptr) {
mavlink_msg_named_value_float_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
time, logExposed->name, logExposed->value.get());
sendMessage(&msg);
}
}
void sendMessage(const void *msg) {
@@ -75,16 +99,36 @@ void sendMessage(const void *msg) {
sendWiFi(buf, len);
}
static uint8_t mavlinkBatch[ESP_NOW_MAX_DATA_LEN_V2];
static int mavlinkBatchSize = 0;
void batchMessage(const void *msg) {
uint8_t buf[MAVLINK_MAX_PACKET_LEN];
int len = mavlink_msg_to_send_buffer(buf, (mavlink_message_t *)msg);
if (mavlinkBatchSize + len > sizeof(mavlinkBatch)) {
sendWiFi(mavlinkBatch, mavlinkBatchSize);
mavlinkBatchSize = 0;
}
memcpy(mavlinkBatch + mavlinkBatchSize, buf, len);
mavlinkBatchSize += len;
}
void flushBatchMessages() {
sendWiFi(mavlinkBatch, mavlinkBatchSize);
mavlinkBatchSize = 0;
}
void receiveMavlink() {
uint8_t buf[MAVLINK_MAX_PACKET_LEN];
int len = receiveWiFi(buf, MAVLINK_MAX_PACKET_LEN);
if (len) mavlinkConnected = true;
// New packet, parse it
mavlink_message_t msg;
mavlink_status_t status;
for (int i = 0; i < len; i++) {
if (mavlink_parse_char(MAVLINK_COMM_0, buf[i], &msg, &status)) {
mavlinkConnected = true;
handleMavlink(&msg);
}
}
@@ -96,7 +140,7 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_MANUAL_CONTROL) {
mavlink_manual_control_t m;
mavlink_msg_manual_control_decode(&msg, &m);
if (m.target && m.target != SYSTEM_ID) return; // 0 is broadcast
if (m.target && m.target != mavlinkSysId) return; // 0 is broadcast
controlThrottle = m.z / 1000.0f;
controlPitch = m.x / 1000.0f;
@@ -109,11 +153,11 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_PARAM_REQUEST_LIST) {
mavlink_param_request_list_t m;
mavlink_msg_param_request_list_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
if (m.target_system && m.target_system != mavlinkSysId) return;
mavlink_message_t msg;
for (int i = 0; i < parametersCount(); i++) {
mavlink_msg_param_value_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
mavlink_msg_param_value_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
getParameterName(i), getParameter(i), MAV_PARAM_TYPE_REAL32, parametersCount(), i);
sendMessage(&msg);
}
@@ -122,7 +166,7 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_PARAM_REQUEST_READ) {
mavlink_param_request_read_t m;
mavlink_msg_param_request_read_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
if (m.target_system && m.target_system != mavlinkSysId) return;
char name[MAVLINK_MSG_PARAM_REQUEST_READ_FIELD_PARAM_ID_LEN + 1];
strlcpy(name, m.param_id, sizeof(name)); // param_id might be not null-terminated
@@ -131,7 +175,7 @@ void handleMavlink(const void *_msg) {
memcpy(name, getParameterName(m.param_index), 16);
}
mavlink_message_t msg;
mavlink_msg_param_value_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
mavlink_msg_param_value_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
name, value, MAV_PARAM_TYPE_REAL32, parametersCount(), m.param_index);
sendMessage(&msg);
}
@@ -139,32 +183,40 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_PARAM_SET) {
mavlink_param_set_t m;
mavlink_msg_param_set_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
if (m.target_system && m.target_system != mavlinkSysId) return;
char name[MAVLINK_MSG_PARAM_SET_FIELD_PARAM_ID_LEN + 1];
strlcpy(name, m.param_id, sizeof(name)); // param_id might be not null-terminated
setParameter(name, m.param_value);
bool success = setParameter(name, m.param_value);
if (!success) return;
// send ack
mavlink_message_t msg;
mavlink_msg_param_value_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
m.param_id, m.param_value, MAV_PARAM_TYPE_REAL32, parametersCount(), 0); // index is unknown
mavlink_msg_param_value_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
m.param_id, getParameter(name), MAV_PARAM_TYPE_REAL32, parametersCount(), 0); // index is unknown
sendMessage(&msg);
}
if (msg.msgid == MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE) {
mavlink_vision_position_estimate_t m;
mavlink_msg_vision_position_estimate_decode(&msg, &m);
Vector pos(m.x, m.y, m.z);
correctPosition(pos);
}
if (msg.msgid == MAVLINK_MSG_ID_MISSION_REQUEST_LIST) { // handle to make qgc happy
mavlink_mission_request_list_t m;
mavlink_msg_mission_request_list_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
if (m.target_system && m.target_system != mavlinkSysId) return;
mavlink_message_t msg;
mavlink_msg_mission_count_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, 0, 0, 0, MAV_MISSION_TYPE_MISSION, 0);
mavlink_msg_mission_count_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, 0, 0, 0, MAV_MISSION_TYPE_MISSION, 0);
sendMessage(&msg);
}
if (msg.msgid == MAVLINK_MSG_ID_SERIAL_CONTROL) {
mavlink_serial_control_t m;
mavlink_msg_serial_control_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
if (m.target_system && m.target_system != mavlinkSysId) return;
char data[MAVLINK_MSG_SERIAL_CONTROL_FIELD_DATA_LEN + 1];
strlcpy(data, (const char *)m.data, m.count); // data might be not null-terminated
@@ -176,20 +228,26 @@ void handleMavlink(const void *_msg) {
mavlink_set_attitude_target_t m;
mavlink_msg_set_attitude_target_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
if (m.target_system && m.target_system != mavlinkSysId) return;
// copy attitude, rates and thrust targets
ratesTarget.x = m.body_roll_rate;
ratesTarget.y = -m.body_pitch_rate; // convert to flu
ratesTarget.z = -m.body_yaw_rate;
attitudeTarget.w = m.q[0];
attitudeTarget.x = m.q[1];
attitudeTarget.y = -m.q[2];
attitudeTarget.z = -m.q[3];
thrustTarget = m.thrust;
ratesExtra = Vector(0, 0, 0);
if (!(m.type_mask & ATTITUDE_TARGET_TYPEMASK_ATTITUDE_IGNORE)) {
// Attitude control
attitudeTarget.w = m.q[0];
attitudeTarget.x = m.q[1];
attitudeTarget.y = -m.q[2];
attitudeTarget.z = -m.q[3];
ratesExtra.x = m.type_mask & ATTITUDE_TARGET_TYPEMASK_BODY_ROLL_RATE_IGNORE ? 0 : m.body_roll_rate;
ratesExtra.y = m.type_mask & ATTITUDE_TARGET_TYPEMASK_BODY_PITCH_RATE_IGNORE ? 0 : -m.body_pitch_rate; // convert to flu
ratesExtra.z = m.type_mask & ATTITUDE_TARGET_TYPEMASK_BODY_YAW_RATE_IGNORE ? 0 : -m.body_yaw_rate;
} else {
// Rates control
attitudeTarget.invalidate();
ratesTarget.x = m.type_mask & ATTITUDE_TARGET_TYPEMASK_BODY_ROLL_RATE_IGNORE ? ratesTarget.x : m.body_roll_rate;
ratesTarget.y = m.type_mask & ATTITUDE_TARGET_TYPEMASK_BODY_PITCH_RATE_IGNORE ? ratesTarget.y : -m.body_pitch_rate;
ratesTarget.z = m.type_mask & ATTITUDE_TARGET_TYPEMASK_BODY_YAW_RATE_IGNORE ? ratesTarget.z : -m.body_yaw_rate;
}
if (m.type_mask & ATTITUDE_TARGET_TYPEMASK_ATTITUDE_IGNORE) attitudeTarget.invalidate();
thrustTarget = valid(m.thrust) ? m.thrust : thrustTarget;
armed = m.thrust > 0;
}
@@ -198,7 +256,7 @@ void handleMavlink(const void *_msg) {
mavlink_set_actuator_control_target_t m;
mavlink_msg_set_actuator_control_target_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
if (m.target_system && m.target_system != mavlinkSysId) return;
attitudeTarget.invalidate();
ratesTarget.invalidate();
@@ -207,37 +265,48 @@ void handleMavlink(const void *_msg) {
armed = motors[0] > 0 || motors[1] > 0 || motors[2] > 0 || motors[3] > 0;
}
if (msg.msgid == MAVLINK_MSG_ID_LOG_REQUEST_LIST) {
const uint32_t qgcEpoch = 1262304000; // qgc accepts only timestamps after 2010-01-01
mavlink_message_t response;
mavlink_msg_log_entry_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &response,
0, 1, 0, qgcEpoch + t * 60, logLength); // put fake unique date to make qgc happy with saving logs
sendMessage(&response);
}
if (msg.msgid == MAVLINK_MSG_ID_LOG_REQUEST_DATA) {
mavlink_log_request_data_t m;
mavlink_msg_log_request_data_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
if (m.target_system && m.target_system != mavlinkSysId) return;
// Send all log records
for (int i = 0; i < sizeof(logBuffer) / sizeof(logBuffer[0]); i++) {
mavlink_message_t msg;
mavlink_msg_log_data_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, 0, i,
sizeof(logBuffer[0]), (uint8_t *)logBuffer[i]);
sendMessage(&msg);
for (int i = 0; i < m.count; i += MAVLINK_MSG_LOG_DATA_FIELD_DATA_LEN) {
int chunkSize = min(MAVLINK_MSG_LOG_DATA_FIELD_DATA_LEN, (int)(m.count - i));
mavlink_message_t response;
uint8_t data[MAVLINK_MSG_LOG_DATA_FIELD_DATA_LEN];
readLog(data, m.ofs + i, chunkSize);
mavlink_msg_log_data_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &response,
m.id, m.ofs + i, chunkSize, data);
batchMessage(&response);
}
flushBatchMessages();
}
// Handle commands
if (msg.msgid == MAVLINK_MSG_ID_COMMAND_LONG) {
mavlink_command_long_t m;
mavlink_msg_command_long_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
if (m.target_system && m.target_system != mavlinkSysId) return;
mavlink_message_t response;
bool accepted = false;
if (m.command == MAV_CMD_REQUEST_MESSAGE && m.param1 == MAVLINK_MSG_ID_AUTOPILOT_VERSION) {
accepted = true;
mavlink_msg_autopilot_version_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &response,
mavlink_msg_autopilot_version_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &response,
MAV_PROTOCOL_CAPABILITY_PARAM_FLOAT | MAV_PROTOCOL_CAPABILITY_MAVLINK2, 1, 0, 1, 1, 0, 0, 0, 0, 0, 0, 0);
sendMessage(&response);
}
if (m.command == MAV_CMD_COMPONENT_ARM_DISARM) {
if (m.param1 && controlThrottle > 0.05) return; // don't arm if throttle is not low
if (m.param1 == 1 && controlThrottle > 0.05) return; // don't arm if throttle is not low
accepted = true;
armed = m.param1 == 1;
}
@@ -250,7 +319,7 @@ void handleMavlink(const void *_msg) {
// send command ack
mavlink_message_t ack;
mavlink_msg_command_ack_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &ack, m.command, accepted ? MAV_RESULT_ACCEPTED : MAV_RESULT_UNSUPPORTED, UINT8_MAX, 0, msg.sysid, msg.compid);
mavlink_msg_command_ack_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &ack, m.command, accepted ? MAV_RESULT_ACCEPTED : MAV_RESULT_UNSUPPORTED, UINT8_MAX, 0, msg.sysid, msg.compid);
sendMessage(&ack);
}
}
@@ -267,7 +336,7 @@ void sendMavlinkPrint() {
char data[MAVLINK_MSG_SERIAL_CONTROL_FIELD_DATA_LEN + 1];
strlcpy(data, str + i, sizeof(data));
mavlink_message_t msg;
mavlink_msg_serial_control_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
mavlink_msg_serial_control_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
SERIAL_CONTROL_DEV_SHELL,
i + MAVLINK_MSG_SERIAL_CONTROL_FIELD_DATA_LEN < strlen(str) ? SERIAL_CONTROL_FLAG_MULTI : 0, // more chunks to go
0, 0, strlen(data), (uint8_t *)data, 0, 0);
@@ -275,5 +344,3 @@ void sendMavlinkPrint() {
}
mavlinkPrintBuffer.clear();
}
#endif
+33 -37
View File
@@ -1,63 +1,59 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Motors output control using MOSFETs
// In case of using ESCs, change PWM_STOP, PWM_MIN and PWM_MAX to appropriate values in μs, decrease PWM_FREQUENCY (to 400)
// PWM control for motors
#include "util.h"
#define MOTOR_0_PIN 12 // rear left
#define MOTOR_1_PIN 13 // rear right
#define MOTOR_2_PIN 14 // front right
#define MOTOR_3_PIN 15 // front left
float motors[4]; // normalized motor thrusts in range [0..1]
#define PWM_FREQUENCY 78000
#define PWM_RESOLUTION 10
#define PWM_STOP 0
#define PWM_MIN 0
#define PWM_MAX 1000000 / PWM_FREQUENCY
int motorPins[4] = {-1, -1, -1, -1}; // default pin numbers
int pwmFrequency = 78000;
int pwmResolution = 10;
int pwmStop = 0;
int pwmMin = 0;
int pwmMax = -1; // -1 means duty cycle mode
// Motors array indexes:
const int MOTOR_REAR_LEFT = 0;
const int MOTOR_REAR_RIGHT = 1;
const int MOTOR_FRONT_RIGHT = 2;
const int MOTOR_FRONT_LEFT = 3;
const int MOTOR_REAR_LEFT = 0, MOTOR_REAR_RIGHT = 1, MOTOR_FRONT_RIGHT = 2, MOTOR_FRONT_LEFT = 3;
void setupMotors() {
print("Setup Motors\n");
// configure pins
ledcAttach(MOTOR_0_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
ledcAttach(MOTOR_1_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
ledcAttach(MOTOR_2_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
ledcAttach(MOTOR_3_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
print("Setup motors\n");
// Configure pins
for (int i = 0; i < 4; i++) {
if (motorPins[i] < 0) continue; // skip unassigned motors
ledcAttach(motorPins[i], pwmFrequency, pwmResolution);
pwmFrequency = ledcChangeFrequency(motorPins[i], pwmFrequency, pwmResolution); // when reconfiguring
}
sendMotors();
print("Motors initialized\n");
}
void sendMotors() {
for (int i = 0; i < 4; i++) {
if (motorPins[i] < 0) continue; // skip unassigned motors
ledcWrite(motorPins[i], getDutyCycle(motors[i]));
}
}
int getDutyCycle(float value) {
value = constrain(value, 0, 1);
float pwm = mapf(value, 0, 1, PWM_MIN, PWM_MAX);
if (value == 0) pwm = PWM_STOP;
float duty = mapf(pwm, 0, 1000000 / PWM_FREQUENCY, 0, (1 << PWM_RESOLUTION) - 1);
return round(duty);
}
void sendMotors() {
ledcWrite(MOTOR_0_PIN, getDutyCycle(motors[0]));
ledcWrite(MOTOR_1_PIN, getDutyCycle(motors[1]));
ledcWrite(MOTOR_2_PIN, getDutyCycle(motors[2]));
ledcWrite(MOTOR_3_PIN, getDutyCycle(motors[3]));
if (pwmMax >= 0) { // pwm mode
float pwm = mapf(value, 0, 1, pwmMin, pwmMax);
if (value == 0) pwm = pwmStop;
float duty = mapf(pwm, 0, 1000000 / pwmFrequency, 0, (1 << pwmResolution) - 1);
return round(duty);
} else { // duty cycle mode
return round(value * ((1 << pwmResolution) - 1));
}
}
bool motorsActive() {
return motors[0] != 0 || motors[1] != 0 || motors[2] != 0 || motors[3] != 0;
}
void testMotor(int n) {
void testMotor(int n, float thrust) {
print("Testing motor %d\n", n);
motors[n] = 1;
motors[n] = thrust;
delay(50); // ESP32 may need to wait until the end of the current cycle to change duty https://github.com/espressif/arduino-esp32/issues/5306
sendMotors();
pause(3);
+110 -22
View File
@@ -5,17 +5,30 @@
#include <Preferences.h>
#include "util.h"
#include "pid.h"
extern float channelZero[16];
extern float channelMax[16];
extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
extern int channelZero[16], channelMax[16];
extern int rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
extern int rcRxPin, voltagePin;
extern int wifiMode, wifiLongRange, udpLocalPort, udpRemotePort, espnowChannel;
extern float rcLossTimeout, descendTime, disarmTilt;
extern float voltageScale;
extern LowPassFilter<float> voltageFilter;
extern PID posX_PID, posY_PID;
Preferences storage;
struct Parameter {
const char *name; // max length is 15 (Preferences key limit)
float *variable;
float value; // cache
const char *name; // max length is 15
bool integer;
union { float *f; int *i; }; // pointer to the variable
float inital; // default value
float cache; // what's stored in flash
void (*callback)(); // called after parameter change
Parameter(const char *name, float *variable, void (*callback)() = nullptr) : name(name), integer(false), f(variable), callback(callback) {};
Parameter(const char *name, int *variable, void (*callback)() = nullptr) : name(name), integer(true), i(variable), callback(callback) {};
float getValue() const { return integer ? *i : *f; };
void setValue(const float value) { if (integer) *i = value; else *f = value; };
};
Parameter parameters[] = {
@@ -24,13 +37,16 @@ Parameter parameters[] = {
{"CTL_R_RATE_I", &rollRatePID.i},
{"CTL_R_RATE_D", &rollRatePID.d},
{"CTL_R_RATE_WU", &rollRatePID.windup},
{"CTL_R_RATE_D_A", &rollRatePID.lpf.alpha},
{"CTL_P_RATE_P", &pitchRatePID.p},
{"CTL_P_RATE_I", &pitchRatePID.i},
{"CTL_P_RATE_D", &pitchRatePID.d},
{"CTL_P_RATE_WU", &pitchRatePID.windup},
{"CTL_P_RATE_D_A", &pitchRatePID.lpf.alpha},
{"CTL_Y_RATE_P", &yawRatePID.p},
{"CTL_Y_RATE_I", &yawRatePID.i},
{"CTL_Y_RATE_D", &yawRatePID.d},
{"CTL_Y_RATE_D_A", &yawRatePID.lpf.alpha},
{"CTL_R_P", &rollPID.p},
{"CTL_R_I", &rollPID.i},
{"CTL_R_D", &rollPID.d},
@@ -42,6 +58,15 @@ Parameter parameters[] = {
{"CTL_R_RATE_MAX", &maxRate.x},
{"CTL_Y_RATE_MAX", &maxRate.z},
{"CTL_TILT_MAX", &tiltMax},
{"CTL_FLT_MODE_0", &flightModes[0]},
{"CTL_FLT_MODE_1", &flightModes[1]},
{"CTL_FLT_MODE_2", &flightModes[2]},
// position
{"POS_XY_P", &posX_PID.p, setupPosition},
{"POS_XY_I", &posX_PID.i, setupPosition},
{"POS_XY_D", &posX_PID.d, setupPosition},
{"POS_XY_WU", &posX_PID.windup, setupPosition},
{"POS_XY_D_A", &posX_PID.lpf.alpha, setupPosition},
// imu
{"IMU_ROT_ROLL", &imuRotation.x},
{"IMU_ROT_PITCH", &imuRotation.y},
@@ -52,10 +77,25 @@ Parameter parameters[] = {
{"IMU_ACC_SCALE_X", &accScale.x},
{"IMU_ACC_SCALE_Y", &accScale.y},
{"IMU_ACC_SCALE_Z", &accScale.z},
{"IMU_GYRO_BIAS_A", &gyroBiasFilter.alpha},
// estimate
{"EST_ACC_WEIGHT", &accWeight},
{"EST_LVL_WEIGHT", &levelWeight},
{"EST_RATES_LPF_A", &ratesFilter.alpha},
{"EST_RATES_NF_F", &ratesNotch.frequency, setupEstimate},
{"EST_RATES_NF_BW", &ratesNotch.bandwidth, setupEstimate},
// motors
{"MOT_PIN_FL", &motorPins[MOTOR_FRONT_LEFT], setupMotors},
{"MOT_PIN_FR", &motorPins[MOTOR_FRONT_RIGHT], setupMotors},
{"MOT_PIN_RL", &motorPins[MOTOR_REAR_LEFT], setupMotors},
{"MOT_PIN_RR", &motorPins[MOTOR_REAR_RIGHT], setupMotors},
{"MOT_PWM_FREQ", &pwmFrequency, setupMotors},
{"MOT_PWM_RES", &pwmResolution, setupMotors},
{"MOT_PWM_STOP", &pwmStop},
{"MOT_PWM_MIN", &pwmMin},
{"MOT_PWM_MAX", &pwmMax},
// rc
{"RC_RX_PIN", &rcRxPin, setupRC},
{"RC_ZERO_0", &channelZero[0]},
{"RC_ZERO_1", &channelZero[1]},
{"RC_ZERO_2", &channelZero[2]},
@@ -77,17 +117,56 @@ Parameter parameters[] = {
{"RC_THROTTLE", &throttleChannel},
{"RC_YAW", &yawChannel},
{"RC_MODE", &modeChannel},
// wifi
{"WIFI_MODE", &wifiMode},
{"WIFI_PORT_LOC", &udpLocalPort},
{"WIFI_PORT_REM", &udpRemotePort},
{"WIFI_LONG_RANGE", &wifiLongRange},
// espnow
{"ESPNOW_CHANNEL", &espnowChannel},
// mavlink
{"MAV_SYS_ID", &mavlinkSysId},
{"MAV_RATE_SLOW", &telemetrySlow.rate},
{"MAV_RATE_ATT", &telemetryAttitude.rate},
{"MAV_RATE_RC", &telemetryRC.rate},
{"MAV_RATE_MOT", &telemetryMotors.rate},
{"MAV_RATE_IMU", &telemetryIMU.rate},
{"MAV_RATE_TOPIC", &telemetryTopic.rate},
// log
{"LOG_MEMORY", &logMemory, setupLog},
{"LOG_USAGE", &logUsage, setupLog},
{"LOG_RATE_000", &logTopics[0].throttle},
{"LOG_RATE_001", &logTopics[1].throttle},
{"LOG_RATE_002", &logTopics[2].throttle},
{"LOG_RATE_003", &logTopics[3].throttle},
{"LOG_RATE_004", &logTopics[4].throttle},
{"LOG_RATE_005", &logTopics[5].throttle},
{"LOG_RATE_006", &logTopics[6].throttle},
{"LOG_RATE_007", &logTopics[7].throttle},
{"LOG_RATE_008", &logTopics[8].throttle},
{"LOG_RATE_009", &logTopics[9].throttle},
{"LOG_RATE_010", &logTopics[10].throttle},
{"LOG_RATE_011", &logTopics[11].throttle},
// power
{"PWR_VOLT_PIN", &voltagePin, setupPower},
{"PWR_VOLT_SCALE", &voltageScale},
{"PWR_VOLT_LPF_A", &voltageFilter.alpha},
// safety
{"SF_RC_LOSS_TIME", &rcLossTimeout},
{"SF_DESCEND_TIME", &descendTime},
{"SF_DISARM_TILT", &disarmTilt}
};
void setupParameters() {
storage.begin("flix", false);
print("Setup parameters\n");
storage.begin("flix");
// Read parameters from storage
for (auto &parameter : parameters) {
if (!storage.isKey(parameter.name)) {
storage.putFloat(parameter.name, *parameter.variable);
parameter.inital = parameter.getValue();
if (storage.isKey(parameter.name)) {
parameter.setValue(storage.getFloat(parameter.name));
}
*parameter.variable = storage.getFloat(parameter.name, *parameter.variable);
parameter.value = *parameter.variable;
parameter.cache = parameter.getValue();
}
}
@@ -102,13 +181,13 @@ const char *getParameterName(int index) {
float getParameter(int index) {
if (index < 0 || index >= parametersCount()) return NAN;
return *parameters[index].variable;
return parameters[index].getValue();
}
float getParameter(const char *name) {
for (auto &parameter : parameters) {
if (strcmp(parameter.name, name) == 0) {
return *parameter.variable;
if (strcasecmp(parameter.name, name) == 0) {
return parameter.getValue();
}
}
return NAN;
@@ -116,8 +195,10 @@ float getParameter(const char *name) {
bool setParameter(const char *name, const float value) {
for (auto &parameter : parameters) {
if (strcmp(parameter.name, name) == 0) {
*parameter.variable = value;
if (strcasecmp(parameter.name, name) == 0) {
if (parameter.integer && !isfinite(value)) return false; // can't set integer to NaN or Inf
parameter.setValue(value);
if (parameter.callback) parameter.callback();
return true;
}
}
@@ -130,16 +211,23 @@ void syncParameters() {
if (motorsActive()) return; // don't use flash while flying, it may cause a delay
for (auto &parameter : parameters) {
if (parameter.value == *parameter.variable) continue;
if (isnan(parameter.value) && isnan(*parameter.variable)) continue; // handle NAN != NAN
storage.putFloat(parameter.name, *parameter.variable);
parameter.value = *parameter.variable;
if (floatEquals(parameter.getValue(), parameter.cache)) continue; // no change
storage.putFloat(parameter.name, parameter.getValue());
parameter.cache = parameter.getValue(); // update cache
}
}
void printParameters() {
void printParameters(const char *filter) {
print("Name Value [Default]\n");
for (auto &parameter : parameters) {
print("%s = %g\n", parameter.name, *parameter.variable);
if (strncasecmp(parameter.name, filter, strlen(filter))) continue;
if (floatEquals(parameter.getValue(), parameter.inital)) { // parameter changed
print("%-15s %-13g\n", parameter.name, parameter.getValue());
} else {
print("%-15s %-13g [%g]\n", parameter.name, parameter.getValue(), parameter.inital);
}
}
}
+1 -1
View File
@@ -5,7 +5,7 @@
#pragma once
#include "lpf.h"
#include "filter.h"
class PID {
public:
+95
View File
@@ -0,0 +1,95 @@
#include "vector.h"
#include "quaternion.h"
#include "pid.h"
#include "util.h"
float mass = 0.065;
float motorThrust = 0.031 * ONE_G;
float positionWeight = 0.9;
float velocityWeight = 0.9;
PID velX_PID(1.0, 0.0, 0.02);
PID velY_PID(1.0, 0.0, 0.02);
PID velZ_PID(1.0, 0.0, 0.02);
// PID posX_PID(1.0, 0.0, 0.0);
// PID posY_PID(1.0, 0.0, 0.0);
// PID posZ_PID(1.0, 0.0, 0.0);
PID posX_PID(0.1, 0.0, 0.0);
PID posY_PID(0.1, 0.0, 0.0);
PID posZ_PID(0.1, 0.0, 0.0);
Vector acceleration;
Vector velocity;
Vector position;
Vector velocityTarget(NAN, NAN, NAN);
Vector positionTarget(NAN, NAN, NAN);
extern Quaternion attitudeTarget;
extern float thrustTarget;
void setupPosition() {
// TODO: posY_PID = posX_PID;
// posX_PID.copy(posY_PID);
posY_PID.p = posX_PID.p;
posY_PID.i = posX_PID.i;
posY_PID.d = posX_PID.d;
}
void estimatePosition() {
acceleration = Quaternion::rotateVector(acceleration, attitude) + Vector(0, 0, -ONE_G);
velocity += acceleration * dt;
position += velocity * dt;
}
void correctPosition(Vector& pos) {
// position += (pos - position) * positionWeight;
position = pos;
// positionUpdated = true;
if (invalid(positionTarget.x) || invalid(positionTarget.y)) return;
attitudeTarget.setPitch(posX_PID.update(positionTarget.x - position.x));
attitudeTarget.setRoll(posY_PID.update(positionTarget.y - position.y));
}
void correctVelocity(Vector& vel) {
velocity += (vel - velocity) * velocityWeight;
}
void controlVelocity() {
Vector accelerationTarget(
velX_PID.update(velocityTarget.x - velocity.x),
velY_PID.update(velocityTarget.y - velocity.y),
velZ_PID.update(velocityTarget.z - velocity.z)
);
Vector thrustVector = (accelerationTarget + Vector(0, 0, ONE_G)) * mass;
const Vector up(0, 0, 1);
attitudeTarget = Quaternion::fromBetweenVectors(up, thrustVector);
float maxThrust = motorThrust * 4; // 4 motors
thrustTarget = thrustVector.norm() / maxThrust;
}
void controlPosition() {
if (positionTarget.invalid()) return;
velocityTarget = Vector(
posX_PID.update(positionTarget.x - position.x),
posY_PID.update(positionTarget.y - position.y),
posZ_PID.update(positionTarget.z - position.z)
);
controlVelocity();
}
void controlPositionSimple() {
if (positionTarget.invalid()) return;
// straight attitude target control
attitudeTarget.setPitch(posX_PID.update(positionTarget.x - position.x));
attitudeTarget.setRoll(posY_PID.update(positionTarget.y - position.y));
}
+29
View File
@@ -0,0 +1,29 @@
// Copyright (c) 2026 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Power management
#include <soc/soc.h>
#include <soc/rtc_cntl_reg.h>
#include "filter.h"
#include "util.h"
float voltage = NAN;
LowPassFilter<float> voltageFilter(1);
int voltagePin = -1;
float voltageScale = 2;
void setupPower() {
REG_CLR_BIT(RTC_CNTL_BROWN_OUT_REG, RTC_CNTL_BROWN_OUT_ENA); // disable reset on low voltage
if (digitalPinToAnalogChannel(voltagePin) == -1) voltagePin = -1; // test ADC pin
}
void readVoltage() {
if (voltagePin < 0) return;
static Rate rate(10);
if (!rate) return;
float v = analogReadMilliVolts(voltagePin) * voltageScale / 1000.0f;
voltage = voltageFilter.update(v);
}
+45 -37
View File
@@ -6,30 +6,33 @@
#include <SBUS.h>
#include "util.h"
SBUS rc(Serial2); // NOTE: Use RC(Serial2, 16, 17) if you use the old UART2 pins
SBUS rc(Serial1);
int rcRxPin = -1; // -1 means disabled
uint16_t channels[16]; // raw rc channels
float controlTime; // time of the last controls update
float channelZero[16]; // calibration zero values
float channelMax[16]; // calibration max values
int channelZero[16]; // calibration zero values
int channelMax[16]; // calibration max values
// Channels mapping (using float to store in parameters):
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
float controlMode = NAN;
float controlTime = NAN; // time of the last controls update
int rollChannel = -1, pitchChannel = -1, throttleChannel = -1, yawChannel = -1, modeChannel = -1; // channel mapping
void setupRC() {
if (rcRxPin < 0) return;
print("Setup RC\n");
rc.begin();
rc.begin(rcRxPin);
}
bool readRC() {
if (rc.read()) {
SBUSData data = rc.data();
for (int i = 0; i < 16; i++) channels[i] = data.ch[i]; // copy channels data
normalizeRC();
controlTime = t;
return true;
}
return false;
if (rcRxPin < 0) return false;
if (!rc.read()) return false;
rc.getChannels(channels);
normalizeRC();
controlTime = t;
return true;
}
void normalizeRC() {
@@ -38,30 +41,35 @@ void normalizeRC() {
controls[i] = mapf(channels[i], channelZero[i], channelMax[i], 0, 1);
}
// Update control values
controlRoll = rollChannel >= 0 ? controls[(int)rollChannel] : NAN;
controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : NAN;
controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : NAN;
controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : NAN;
controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN;
controlRoll = rollChannel < 0 ? 0 : controls[rollChannel];
controlPitch = pitchChannel < 0 ? 0 : controls[pitchChannel];
controlYaw = yawChannel < 0 ? 0 : controls[yawChannel];
controlThrottle = throttleChannel < 0 ? 0 : controls[throttleChannel];
controlMode = modeChannel < 0 ? NAN : controls[modeChannel]; // mode control is ineffective if not mapped
}
void calibrateRC() {
uint16_t zero[16];
uint16_t center[16];
uint16_t max[16];
if (rcRxPin < 0) {
print("RC_RX_PIN = %d, set the RC pin!\n", rcRxPin);
return;
}
uint16_t zero[16]; // for zero positions
uint16_t center[16]; // for center positions
uint16_t _[16]; // for unused data
print("1/8 Calibrating RC: put all switches to default positions [3 sec]\n");
pause(3);
calibrateRCChannel(NULL, zero, zero, "2/8 Move sticks [3 sec]\n... ...\n... .o.\n.o. ...\n");
calibrateRCChannel(NULL, center, center, "3/8 Move sticks [3 sec]\n... ...\n.o. .o.\n... ...\n");
calibrateRCChannel(&throttleChannel, zero, max, "4/8 Move sticks [3 sec]\n.o. ...\n... .o.\n... ...\n");
calibrateRCChannel(&yawChannel, center, max, "5/8 Move sticks [3 sec]\n... ...\n..o .o.\n... ...\n");
calibrateRCChannel(&pitchChannel, zero, max, "6/8 Move sticks [3 sec]\n... .o.\n... ...\n.o. ...\n");
calibrateRCChannel(&rollChannel, zero, max, "7/8 Move sticks [3 sec]\n... ...\n... ..o\n.o. ...\n");
calibrateRCChannel(&modeChannel, zero, max, "8/8 Put mode switch to max [3 sec]\n");
calibrateRCChannel(NULL, _, zero, "2/8 Move sticks [3 sec]\n... ...\n... .o.\n.o. ...\n");
calibrateRCChannel(&throttleChannel, zero, _, "3/8 Move sticks [3 sec]\n.o. ...\n... .o.\n... ...\n");
calibrateRCChannel(NULL, _, center, "4/8 Move sticks [3 sec]\n... ...\n.o. .o.\n... ...\n");
calibrateRCChannel(&yawChannel, center, _, "5/8 Move sticks [3 sec]\n... ...\n..o .o.\n... ...\n");
calibrateRCChannel(&pitchChannel, zero, _, "6/8 Move sticks [3 sec]\n... .o.\n... ...\n.o. ...\n");
calibrateRCChannel(&rollChannel, zero, _, "7/8 Move sticks [3 sec]\n... ...\n... ..o\n.o. ...\n");
calibrateRCChannel(&modeChannel, zero, _, "8/8 Put mode switch to max [3 sec]\n");
printRCCalibration();
}
void calibrateRCChannel(float *channel, uint16_t in[16], uint16_t out[16], const char *str) {
void calibrateRCChannel(int *channel, uint16_t in[16], uint16_t out[16], const char *str) {
print("%s", str);
pause(3);
for (int i = 0; i < 30; i++) readRC(); // try update 30 times max
@@ -82,15 +90,15 @@ void calibrateRCChannel(float *channel, uint16_t in[16], uint16_t out[16], const
channelZero[ch] = in[ch];
channelMax[ch] = out[ch];
} else {
*channel = NAN;
*channel = -1;
}
}
void printRCCalibration() {
print("Control Ch Zero Max\n");
print("Roll %-7g%-7g%-7g\n", rollChannel, rollChannel >= 0 ? channelZero[(int)rollChannel] : NAN, rollChannel >= 0 ? channelMax[(int)rollChannel] : NAN);
print("Pitch %-7g%-7g%-7g\n", pitchChannel, pitchChannel >= 0 ? channelZero[(int)pitchChannel] : NAN, pitchChannel >= 0 ? channelMax[(int)pitchChannel] : NAN);
print("Yaw %-7g%-7g%-7g\n", yawChannel, yawChannel >= 0 ? channelZero[(int)yawChannel] : NAN, yawChannel >= 0 ? channelMax[(int)yawChannel] : NAN);
print("Throttle %-7g%-7g%-7g\n", throttleChannel, throttleChannel >= 0 ? channelZero[(int)throttleChannel] : NAN, throttleChannel >= 0 ? channelMax[(int)throttleChannel] : NAN);
print("Mode %-7g%-7g%-7g\n", modeChannel, modeChannel >= 0 ? channelZero[(int)modeChannel] : NAN, modeChannel >= 0 ? channelMax[(int)modeChannel] : NAN);
print("Roll %-7d%-7d%-7d\n", rollChannel, rollChannel < 0 ? 0 : channelZero[rollChannel], rollChannel < 0 ? 0 : channelMax[rollChannel]);
print("Pitch %-7d%-7d%-7d\n", pitchChannel, pitchChannel < 0 ? 0 : channelZero[pitchChannel], pitchChannel < 0 ? 0 : channelMax[pitchChannel]);
print("Yaw %-7d%-7d%-7d\n", yawChannel, yawChannel < 0 ? 0 : channelZero[yawChannel], yawChannel < 0 ? 0 : channelMax[yawChannel]);
print("Throttle %-7d%-7d%-7d\n", throttleChannel, throttleChannel < 0 ? 0 : channelZero[throttleChannel], throttleChannel < 0 ? 0 : channelMax[throttleChannel]);
print("Mode %-7d%-7d%-7d\n", modeChannel, modeChannel < 0 ? 0 : channelZero[modeChannel], modeChannel < 0 ? 0 : channelMax[modeChannel]);
}
+22 -9
View File
@@ -3,22 +3,23 @@
// Fail-safe functions
#define RC_LOSS_TIMEOUT 1
#define DESCEND_TIME 10
extern float controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw;
float rcLossTimeout = 1;
float descendTime = 10;
float disarmTilt = radians(120);
void failsafe() {
rcLossFailsafe();
autoFailsafe();
tiltFailsafe();
}
// RC loss failsafe
void rcLossFailsafe() {
if (controlTime == 0) return; // no RC at all
if (!armed) return;
if (t - controlTime > RC_LOSS_TIMEOUT) {
if (t - controlTime > rcLossTimeout) {
descend();
}
}
@@ -27,7 +28,7 @@ void rcLossFailsafe() {
void descend() {
mode = AUTO;
attitudeTarget = Quaternion();
thrustTarget -= dt / DESCEND_TIME;
thrustTarget -= dt / descendTime;
if (thrustTarget < 0) {
thrustTarget = 0;
armed = false;
@@ -37,12 +38,24 @@ void descend() {
// Allow pilot to interrupt automatic flight
void autoFailsafe() {
static float roll, pitch, yaw, throttle;
if (roll != controlRoll || pitch != controlPitch || yaw != controlYaw || abs(throttle - controlThrottle) > 0.05) {
// controls changed
if (mode == AUTO) mode = STAB; // regain control by the pilot
if (abs(roll - controlRoll) > 0.05 || abs(pitch - controlPitch) > 0.05 || abs(yaw - controlYaw) > 0.05 || abs(throttle - controlThrottle) > 0.05) {
// controls changed and mode switch is not configured
if (mode == AUTO && invalid(controlMode)) mode = STAB; // regain control by the pilot
}
roll = controlRoll;
pitch = controlPitch;
yaw = controlYaw;
throttle = controlThrottle;
}
// Disarm if tilted too much
void tiltFailsafe() {
if (!armed) return;
if (mode != STAB) return;
Vector up = Quaternion::rotateVector(Vector(0, 0, 1), attitude);
float tilt = acos(up.z);
if (disarmTilt && tilt > disarmTilt) {
armed = false;
}
}
+2
View File
@@ -3,6 +3,8 @@
// Time related functions
float t = NAN; // current time, s
float dt; // time delta with the previous step, s
float loopRate; // Hz
void step() {
+68 -8
View File
@@ -6,8 +6,7 @@
#pragma once
#include <math.h>
#include <soc/soc.h>
#include <soc/rtc_cntl_reg.h>
#include <ESP32_NOW_Serial.h>
const float ONE_G = 9.80665;
extern float t;
@@ -24,6 +23,12 @@ bool valid(float x) {
return isfinite(x);
}
bool floatEquals(float a, float b, float epsilon = 0) {
if (isnan(a) && isnan(b)) return true;
if (a == b) return true;
return fabsf(a - b) <= epsilon;
}
// Wrap angle to [-PI, PI)
float wrapAngle(float angle) {
angle = fmodf(angle, 2 * PI);
@@ -35,21 +40,73 @@ float wrapAngle(float angle) {
return angle;
}
// Disable reset on low voltage
void disableBrownOut() {
REG_CLR_BIT(RTC_CNTL_BROWN_OUT_REG, RTC_CNTL_BROWN_OUT_ENA);
}
// Trim and split string by spaces
void splitString(String& str, String& token0, String& token1, String& token2) {
str.trim();
if (str.isEmpty()) return;
char chars[str.length() + 1];
str.toCharArray(chars, str.length() + 1);
token0 = strtok(chars, " ");
token1 = strtok(NULL, " "); // String(NULL) creates empty string
token1 = strtok(NULL, " ");
token2 = strtok(NULL, "");
if (token1.c_str() == NULL) token1 = "";
if (token2.c_str() == NULL) token2 = "";
}
// Simplified ESP-NOW Serial without resends
class ESPNOWSerial : public ESP_NOW_Serial_Class {
public:
int lost = 0;
using ESP_NOW_Serial_Class::ESP_NOW_Serial_Class;
void onSent(bool success) override {
if (!success) lost++;
ESP_NOW_Serial_Class::onSent(true); // always report success to avoid resends
}
};
// Simple variant type for logging and parameters
struct Value {
enum { EMPTY, FLOAT, INT, BOOL, FLOAT_FN, INT_FN, BOOL_FN } type;
union {
void *pointer;
float *_float;
int *_int;
bool *_bool;
float (*floatFn)();
int (*intFn)();
bool (*boolFn)();
};
Value() : type(EMPTY), pointer(nullptr) {};
Value(float *pt) : type(FLOAT), _float(pt) {};
Value(int *pt) : type(INT), _int(pt) {};
Value(bool *pt) : type(BOOL), _bool(pt) {};
Value(float (*fn)()) : type(FLOAT_FN), floatFn(fn) {};
Value(int (*fn)()) : type(INT_FN), intFn(fn) {};
Value(bool (*fn)()) : type(BOOL_FN), boolFn(fn) {};
float get() const {
switch (type) {
case FLOAT: return *_float;
case INT: return *_int;
case BOOL: return *_bool ? 1 : 0;
case FLOAT_FN: return floatFn();
case INT_FN: return intFn();
case BOOL_FN: return boolFn() ? 1 : 0;
default: return NAN;
}
};
void set(float value) const {
switch (type) {
case FLOAT: *_float = value; break;
case INT: *_int = value; break;
case BOOL: *_bool = (value != 0); break;
default: break;
}
};
};
// Rate limiter
class Rate {
public:
@@ -58,6 +115,9 @@ public:
Rate(float rate) : rate(rate) {}
operator bool() {
if (t == last) {
return true; // the same step
}
if (t - last >= 1 / rate) {
last = t;
return true;
+16 -4
View File
@@ -35,7 +35,6 @@ public:
z = NAN;
}
float norm() const {
return sqrt(x * x + y * y + z * z);
}
@@ -106,10 +105,23 @@ public:
}
static Vector rotationVectorBetween(const Vector& a, const Vector& b) {
float an = a.norm();
float bn = b.norm();
if (an < 1e-6 || bn < 1e-6) {
return Vector(0, 0, 0);
}
Vector direction = cross(a, b);
if (direction.zero()) {
// vectors are opposite, return any perpendicular vector
return cross(a, Vector(1, 0, 0));
if (direction.norm() < 1e-6) { // vectors are parallel
if (dot(a, b) > 0) { // same direction
return Vector(0, 0, 0);
}
// opposite direction
Vector perp = cross(a, Vector(1, 0, 0));
if (perp.norm() < 1e-6) {
perp = cross(a, Vector(0, 1, 0));
}
perp.normalize();
return perp * PI;
}
direction.normalize();
float angle = angleBetween(a, b);
+123 -20
View File
@@ -1,49 +1,152 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Wi-Fi support
#if WIFI_ENABLED
// Wi-Fi and ESP-NOW communication
#include <WiFi.h>
#include <WiFiAP.h>
#include <WiFiUdp.h>
#include <MacAddress.h>
#include <ESP32_NOW_Serial.h>
#include <Preferences.h>
#include "util.h"
#define WIFI_SSID "flix"
#define WIFI_PASSWORD "flixwifi"
#define WIFI_UDP_PORT 14550
#define WIFI_UDP_REMOTE_PORT 14550
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
extern Preferences storage; // use the main preferences storage
const int W_DISABLED = 0, W_AP = 1, W_STA = 2, W_ESPNOW = 3;
int wifiMode = W_AP;
int wifiLongRange = 0;
int udpLocalPort = 14550;
int udpRemotePort = 14550;
IPAddress udpRemoteIP = "255.255.255.255";
WiFiUDP udp;
ESPNOWSerial espnow(NULL, 0, WIFI_IF_AP);
ESPNOWSerial espnowBroadcast(ESP_NOW.BROADCAST_ADDR, 0, WIFI_IF_AP);
int espnowChannel = 6;
void setupWiFi() {
print("Setup Wi-Fi\n");
WiFi.softAP(WIFI_SSID, WIFI_PASSWORD);
udp.begin(WIFI_UDP_PORT);
WiFi.enableLongRange(wifiLongRange);
if (wifiMode == W_AP) {
WiFi.softAP(storage.getString("WIFI_AP_SSID", "flix").c_str(), storage.getString("WIFI_AP_PASS", "flixwifi").c_str());
udp.begin(udpLocalPort);
}
if (wifiMode == W_STA) {
WiFi.begin(storage.getString("WIFI_STA_SSID", "").c_str(), storage.getString("WIFI_STA_PASS", "").c_str());
udp.begin(udpLocalPort);
}
if (wifiMode == W_ESPNOW) {
WiFi.mode(WIFI_AP);
WiFi.setChannel(espnowChannel);
espnow.addr(MacAddress(storage.getString("ESPNOW_PEER_MAC", "FF:FF:FF:FF:FF:FF").c_str()));
String key = storage.getString("ESPNOW_PEER_KEY", "");
espnow.setKey(key.isEmpty() ? nullptr : (const uint8_t *)key.c_str());
espnow.begin();
espnowBroadcast.begin();
}
WiFi.setSleep(false); // disable power save
}
void sendWiFi(const uint8_t *buf, int len) {
if (WiFi.softAPIP() == IPAddress(0, 0, 0, 0) && WiFi.status() != WL_CONNECTED) return;
udp.beginPacket(udp.remoteIP() ? udp.remoteIP() : WIFI_UDP_REMOTE_ADDR, WIFI_UDP_REMOTE_PORT);
if (espnow) {
espnow.write(buf, len);
static Rate discovery(2);
if (espnow.isEncrypted() && discovery) espnowBroadcast.write((const uint8_t *)"flix", 4); // broadcast message to help finding this device
return;
}
if (WiFi.softAPgetStationNum() == 0 && !WiFi.isConnected()) return;
udp.beginPacket(udpRemoteIP, udpRemotePort);
udp.write(buf, len);
udp.endPacket();
}
int receiveWiFi(uint8_t *buf, int len) {
if (espnow) {
return espnow.read(buf, len);
}
if (WiFi.softAPgetStationNum() == 0 && !WiFi.isConnected()) return 0;
udp.parsePacket();
if (udp.remoteIP()) udpRemoteIP = udp.remoteIP();
return udp.read(buf, len);
}
void printWiFiInfo() {
print("MAC: %s\n", WiFi.softAPmacAddress().c_str());
print("SSID: %s\n", WiFi.softAPSSID().c_str());
print("Password: %s\n", WIFI_PASSWORD);
print("Clients: %d\n", WiFi.softAPgetStationNum());
print("Status: %d\n", WiFi.status());
print("IP: %s\n", WiFi.softAPIP().toString().c_str());
print("Remote IP: %s\n", udp.remoteIP().toString().c_str());
if (espnow) {
print("Mode: ESP-NOW\n");
print("ESP-NOW version: %d\n", ESP_NOW.getVersion());
print("Max packet size: %d\n", ESP_NOW.getMaxDataLen());
print("MAC: %s\n", WiFi.softAPmacAddress().c_str());
print("Peer MAC: %s\n", MacAddress(espnow.addr()).toString().c_str());
print("Encrypted: %d\n", espnow.isEncrypted());
print("Channel: %d\n", WiFi.channel());
print("Lost packets: %d\n", espnow.lost);
} else if (WiFi.getMode() == WIFI_MODE_AP) {
print("Mode: Access Point (AP)\n");
print("MAC: %s\n", WiFi.softAPmacAddress().c_str());
print("SSID: %s\n", WiFi.softAPSSID().c_str());
print("Password: ***\n");
print("Channel: %d\n", WiFi.channel());
print("Clients: %d\n", WiFi.softAPgetStationNum());
print("IP: %s\n", WiFi.softAPIP().toString().c_str());
print("Remote IP: %s\n", udpRemoteIP.toString().c_str());
} else if (WiFi.getMode() == WIFI_MODE_STA) {
print("Mode: Client (STA)\n");
print("Connected: %d\n", WiFi.isConnected());
print("MAC: %s\n", WiFi.macAddress().c_str());
print("SSID: %s\n", WiFi.SSID().c_str());
print("Password: ***\n");
print("Channel: %d\n", WiFi.channel());
print("RSSI: %d dBm\n", WiFi.RSSI());
print("IP: %s\n", WiFi.localIP().toString().c_str());
print("Remote IP: %s\n", udpRemoteIP.toString().c_str());
} else {
print("Mode: Disabled\n");
}
print("MAVLink connected: %d\n", mavlinkConnected);
}
#endif
void configWiFi(int mode, const char *first, const char *second) {
MacAddress mac;
if (mode == W_AP && strlen(first) > 0 && strlen(second) >= 8) {
storage.putString("WIFI_AP_SSID", first);
storage.putString("WIFI_AP_PASS", second);
} else if (mode == W_STA && strlen(first) > 0 && strlen(second) >= 8) {
storage.putString("WIFI_STA_SSID", first);
storage.putString("WIFI_STA_PASS", second);
} else if (mode == W_ESPNOW && mac.fromString(first)) {
storage.putString("ESPNOW_PEER_MAC", first);
storage.putString("ESPNOW_PEER_KEY", strlen(second) == ESP_NOW_KEY_LEN ? second : "");
} else {
print("Invalid configuration\n");
return;
}
print("✓ Reboot to apply new settings\n");
}
void setWiFiMode(const String& mode) {
if (mode == "ap") {
wifiMode = W_AP;
} else if (mode == "sta") {
wifiMode = W_STA;
} else if (mode == "espnow") {
wifiMode = W_ESPNOW;
} else if (mode == "off") {
wifiMode = W_DISABLED;
} else {
print("Invalid Wi-Fi mode\n");
return;
}
static const char *modes[] = {"Disabled", "Access Point (AP)", "Client (STA)", "ESP-NOW"};
print("✓ Wi-Fi mode set to %s, reboot to apply\n", modes[wifiMode]);
}
+17 -1
View File
@@ -20,7 +20,13 @@
#define radians(deg) ((deg)*DEG_TO_RAD)
#define degrees(rad) ((rad)*RAD_TO_DEG)
#define MALLOC_CAP_SPIRAM (1<<10)
#define MALLOC_CAP_8BIT (1<<2)
#define ESP_NOW_MAX_DATA_LEN_V2 1470
#define constrain(amt,low,high) ((amt)<(low)?(low):((amt)>(high)?(high):(amt)))
template<typename T> T max(T a, T b) { return a > b ? a : b; }
template<typename T> T min(T a, T b) { return a < b ? a : b; }
long map(long x, long in_min, long in_max, long out_min, long out_max) {
const long run = in_max - in_min;
@@ -149,11 +155,13 @@ public:
void setRxInvert(bool invert) {};
};
HardwareSerial Serial, Serial2;
HardwareSerial Serial, Serial1, Serial2;
class EspClass {
public:
void restart() { Serial.println("Ignore reboot in simulation"); }
uint32_t getFreeHeap() { return 300 * 1024; } // assume 300 KB free heap
uint32_t getFreePsram() { return 8 * 1024 * 1024; } // assume 8 MB free PSRAM
} ESP;
unsigned long __delayTime = 0;
@@ -163,8 +171,16 @@ void delay(uint32_t ms) {
__delayTime += ms * 1000;
}
void *heap_caps_calloc(size_t n, size_t size, uint32_t caps) {
return calloc(n, size);
}
bool ledcAttach(uint8_t pin, uint32_t freq, uint8_t resolution) { return true; }
bool ledcWrite(uint8_t pin, uint32_t duty) { return true; }
uint32_t ledcChangeFrequency(uint8_t pin, uint32_t freq, uint8_t resolution) { return freq; }
int8_t digitalPinToAnalogChannel(uint8_t pin) { return -1; }
uint32_t analogReadMilliVolts(uint8_t pin) { return 0; }
float temperatureRead() { return 0; }
unsigned long __micros;
unsigned long __resetTime = 0;
+12
View File
@@ -0,0 +1,12 @@
// Dummy file for the simulator
class ESP_NOW_Peer {
protected:
size_t send(const uint8_t *data, int len) { return 0; }
};
class ESP_NOW_Serial_Class : public ESP_NOW_Peer {
public:
virtual void onSent(bool success) {};
virtual size_t write(const uint8_t *data, size_t len) { return 0; };
};
+5 -6
View File
@@ -13,14 +13,13 @@ class SBUS {
public:
SBUS(HardwareSerial& bus, const bool inv = true) {};
SBUS(HardwareSerial& bus, const int8_t rxpin, const int8_t txpin, const bool inv = true) {};
void begin() {};
void begin(int rxpin = -1, int txpin = -1, bool inv = true, bool fast = false) {};
bool read() { return joystickInit(); };
SBUSData data() {
SBUSData data;
joystickGet(data.ch);
void getChannels(uint16_t (&channels)[16]) const {
int16_t ch[16];
joystickGet(ch);
for (int i = 0; i < 16; i++) {
data.ch[i] = map(data.ch[i], -32768, 32767, 1000, 2000); // convert to pulse width style
channels[i] = map(ch[i], -32768, 32767, 1000, 2000); // convert to pulse width style
}
return data;
};
};
+36 -19
View File
@@ -9,45 +9,56 @@
#include "quaternion.h"
#include "Arduino.h"
#include "wifi.h"
#include "filter.h"
#define WIFI_ENABLED 1
extern float t, dt;
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
extern Vector rates;
extern Quaternion attitude;
extern bool landed;
extern float motors[4];
float t = NAN;
float dt;
float motors[4];
float controlRoll, controlPitch, controlYaw, controlThrottle = NAN;
float controlMode = NAN;
Vector acc;
Vector gyro;
Vector rates;
Quaternion attitude;
bool landed;
Vector imuRotation;
Vector gyro, acc, imuRotation;
Vector accBias, gyroBias, accScale(1, 1, 1);
LowPassFilter<Vector> gyroBiasFilter(0);
// declarations
void step();
void computeLoopRate();
void applyGyro();
void applyAcc();
void applyLevel();
void control();
void interpretControls();
void controlAttitude();
void controlRates();
void controlTorque();
void desaturate(float& a, float& b, float& c, float& d);
const char* getModeName();
void sendMotors();
int getDutyCycle(float value);
bool motorsActive();
void testMotor(int n);
void testMotor(int, float);
void print(const char* format, ...);
void pause(float duration);
void doCommand(String str, bool echo);
void handleInput();
void setupRC();
void normalizeRC();
void calibrateRC();
void calibrateRCChannel(float *channel, uint16_t zero[16], uint16_t max[16], const char *str);
void calibrateRCChannel(int*, uint16_t[16], uint16_t[16], const char*);
void printRCCalibration();
void loopLog();
void resetLog();
void writeLog(const void *data, size_t size);
void readLog(void *data, size_t position, size_t size);
bool isTopicUpdated(const uint8_t topic);
void printLogInfo();
int estimateLogDuration();
void printLogHeader();
void printLogData();
void printLogValues(const char *filter);
void configLogThrottle(const char *name, float throttle);
void exposeLogValue(const char *name);
void processMavlink();
void sendMavlink();
void sendMessage(const void *msg);
@@ -56,24 +67,30 @@ void handleMavlink(const void *_msg);
void mavlinkPrint(const char* str);
void sendMavlinkPrint();
inline Quaternion fluToFrd(const Quaternion &q);
void setupPower();
void failsafe();
void rcLossFailsafe();
void descend();
void autoFailsafe();
void tiltFailsafe();
int parametersCount();
const char *getParameterName(int index);
float getParameter(int index);
float getParameter(const char *name);
bool setParameter(const char *name, const float value);
void printParameters();
void printParameters(const char *filter);
void resetParameters();
// mocks
void setLED(bool on) {};
void calibrateGyro() { print("Skip gyro calibrating\n"); };
void calibrateAccel() { print("Skip accel calibrating\n"); };
void calibrateLevel() { print("Skip level calibrating\n"); };
void printIMUCalibration() { print("cal: N/A\n"); };
void printIMUInfo() {};
void printWiFiInfo() {};
Vector accBias, gyroBias, accScale(1, 1, 1);
void configWiFi(bool, const char*, const char*) { print("Skip WiFi config\n"); };
void setWiFiMode(const String& mode) { print("Skip WiFi mode set\n"); };
class IMU {
public:
float getTemp() { return 0; }
} imu;
+7 -2
View File
@@ -23,10 +23,11 @@
#include "estimate.ino"
#include "safety.ino"
#include "log.ino"
#include "lpf.h"
#include "filter.h"
#include "mavlink.ino"
#include "motors.ino"
#include "parameters.ino"
#include "power.ino"
#include "rc.ino"
#include "time.ino"
@@ -54,6 +55,8 @@ public:
initNode();
Serial.begin(0);
setupParameters();
setupLog();
rcRxPin = 1; // set rc pin to enable rc reading
gzmsg << "Flix plugin loaded" << endl;
}
@@ -72,6 +75,8 @@ public:
gyro = Vector(imu->AngularVelocity().X(), imu->AngularVelocity().Y(), imu->AngularVelocity().Z());
acc = this->accFilter.update(Vector(imu->LinearAcceleration().X(), imu->LinearAcceleration().Y(), imu->LinearAcceleration().Z()));
voltage = 4.2f; // dummy voltage value
readRC();
estimate();
@@ -84,7 +89,7 @@ public:
applyMotorForces();
publishTopics();
logData();
loopLog();
syncParameters();
}
-1
View File
@@ -1,4 +1,3 @@
// Dummy file to make it possible to compile simulator with Flix' util.h
#define WRITE_PERI_REG(addr, val) {}
#define REG_CLR_BIT(_r, _b) {}
+14 -8
View File
@@ -11,9 +11,15 @@
#include <sys/poll.h>
#include <gazebo/gazebo.hh>
#define WIFI_UDP_PORT 14580
#define WIFI_UDP_REMOTE_PORT 14550
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
// Mocks
int wifiMode = 1;
int wifiLongRange = 0;
int espnowChannel = 6;
const int W_DISABLED = 0, W_AP = 1, W_STA = 2, W_ESPNOW = 3;
int udpLocalPort = 14580;
int udpRemotePort = 14550;
const char *udpRemoteIP = "255.255.255.255";
int wifiSocket;
@@ -22,22 +28,22 @@ void setupWiFi() {
sockaddr_in addr; // local address
addr.sin_family = AF_INET;
addr.sin_addr.s_addr = INADDR_ANY;
addr.sin_port = htons(WIFI_UDP_PORT);
addr.sin_port = htons(udpLocalPort);
if (bind(wifiSocket, (sockaddr *)&addr, sizeof(addr))) {
gzerr << "Failed to bind WiFi UDP socket on port " << WIFI_UDP_PORT << std::endl;
gzerr << "Failed to bind WiFi UDP socket on port " << udpLocalPort << std::endl;
return;
}
int broadcast = 1;
setsockopt(wifiSocket, SOL_SOCKET, SO_BROADCAST, &broadcast, sizeof(broadcast)); // enable broadcast
gzmsg << "WiFi UDP socket initialized on port " << WIFI_UDP_PORT << " (remote port " << WIFI_UDP_REMOTE_PORT << ")" << std::endl;
gzmsg << "WiFi UDP socket initialized on port " << udpLocalPort << " (remote port " << udpRemotePort << ")" << std::endl;
}
void sendWiFi(const uint8_t *buf, int len) {
if (wifiSocket == 0) setupWiFi();
sockaddr_in addr; // remote address
addr.sin_family = AF_INET;
addr.sin_addr.s_addr = inet_addr(WIFI_UDP_REMOTE_ADDR);
addr.sin_port = htons(WIFI_UDP_REMOTE_PORT);
addr.sin_addr.s_addr = inet_addr(udpRemoteIP);
addr.sin_port = htons(udpRemotePort);
sendto(wifiSocket, buf, len, 0, (sockaddr *)&addr, sizeof(addr));
}
+10 -1
View File
@@ -9,6 +9,7 @@ Usage:
import csv
import json
import docopt
import math
from mcap.writer import Writer
args = docopt.docopt(__doc__)
@@ -39,7 +40,15 @@ channel_id = writer.register_channel(
)
for row in csv_reader:
data = {key: float(value) for key, value in zip(header, row)}
if row[0] == '': continue
data = {}
for key, value in zip(header, row):
if value == '' or math.isnan(float(value)):
data[key] = None
else:
data[key] = float(value)
data = {key: float(value) if value != '' else None for key, value in zip(header, row)}
timestamp = round(float(row[0]) * 1e9)
writer.add_message(channel_id=channel_id, log_time=timestamp, data=json.dumps(data).encode(), publish_time=timestamp,)
+3
View File
@@ -0,0 +1,3 @@
# ESPNOW-proxy
Proxy sketch for using ESP-NOW connection with Flix drone.
+108
View File
@@ -0,0 +1,108 @@
// Copyright (c) 2026 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Proxy for ESP-NOW connection
#include <vector>
#include <WiFi.h>
#include <ESP32_NOW_Serial.h>
#include <MacAddress.h>
#include <MAVLink.h>
#include <Preferences.h>
#include "../../flix/util.h"
const bool DISABLE_SWARM = true;
const int CHANNEL = -1; // -1 means auto search
char key[ESP_NOW_KEY_LEN + 1] = {0}; // with trailing null
Preferences storage;
std::vector<ESPNOWSerial *> peers;
bool stop = false;
void onNewPeer(const esp_now_recv_info_t *info, const uint8_t *data, int len, void *arg) {
if (len != 4 || memcmp(data, "flix", 4) != 0) return; // check if discovery message
if (stop) return;
Serial.printf("New peer: " MACSTR "\n", MAC2STR(info->src_addr));
ESPNOWSerial *link = new ESPNOWSerial(info->src_addr, WiFi.channel(), WIFI_IF_STA);
link->begin();
link->setKey((const uint8_t *)key);
peers.push_back(link);
}
void setup() {
Serial.begin(115200);
WiFi.mode(WIFI_STA);
WiFi.setSleep(false);
ESP_NOW.onNewPeer(onNewPeer, NULL);
ESP_NOW.begin();
storage.begin("espnow-proxy");
if (!storage.isKey("key")) {
generateRandomKey();
storage.putString("key", key);
}
strcpy(key, storage.getString("key").c_str());
}
void generateRandomKey() {
const char chars[] = "ABCDEFGHIJKLMNOPQRSTUVWXYZabcdefghijklmnopqrstuvwxyz0123456789!@#$%^&*-_+=";
for (int i = 0; i < ESP_NOW_KEY_LEN; i++) {
key[i] = chars[random(0, strlen(chars))];
}
}
void loop() {
uint8_t buf[5000];
static int channelIndex = 0;
static const int channels[] = {6, 11, 1, 2, 6, 11, 3, 4, 5, 6, 1, 11, 8, 6, 9, 10, 11, 6, 1, 12, 13}; // 6, 1 and 11 are most common
static unsigned long last = 0;
if (!stop && millis() - last > 500) {
// Change search channel
last = millis();
channelIndex = (channelIndex + 1) % (sizeof(channels) / sizeof(channels[0]));
int channel = CHANNEL < 0 ? channels[channelIndex] : CHANNEL;
Serial.printf("Run on Flix: espnow %s %s\n", WiFi.STA.macAddress().c_str(), key);
Serial.printf("Searching channel %d\n", channel);
WiFi.setChannel(channel);
}
// Send from Serial to ESP-NOW
while (Serial.available() > 0) {
int b = Serial.read();
if (b < 0) {
break;
}
mavlink_message_t msg;
mavlink_status_t status;
if (mavlink_parse_char(MAVLINK_COMM_0, (uint8_t)b, &msg, &status)) {
int len = mavlink_msg_to_send_buffer(buf, &msg);
for (ESPNOWSerial *link : peers) {
link->write(buf, len);
}
}
}
// Send from ESP-NOW to Serial
for (ESPNOWSerial *link : peers) {
int len = link->read(buf, sizeof(buf));
if (!stop) {
for (int i = 0; i < len; i++) {
if (buf[i] == MAVLINK_STX) {
// Got MAVLink message, stop discovery
Serial.printf("Received MAVLink from " MACSTR "\n", MAC2STR(link->addr()));
if (DISABLE_SWARM) stop = true;
}
}
}
if (len > 0) {
Serial.write(buf, len);
}
}
}
+4 -3
View File
@@ -10,6 +10,7 @@ print('Connected:', flix.connected)
print('Mode:', flix.mode)
print('Armed:', flix.armed)
print('Landed:', flix.landed)
print('Voltage:', flix.voltage, 'V')
print('Rates:', *[f'{math.degrees(r):.0f}°/s' for r in flix.rates])
print('Attitude:', *[f'{math.degrees(a):.0f}°' for a in flix.attitude_euler])
print('Motors:', flix.motors)
@@ -23,11 +24,11 @@ print('> imu')
print(flix.cli('imu'))
print('=== Get parameter...')
pitch_p = flix.get_param('PITCH_P')
print('PITCH_P = ', pitch_p)
pitch_p = flix.get_param('CTL_P_P')
print('CTL_P_P = ', pitch_p)
print('=== Set parameter...')
flix.set_param('PITCH_P', pitch_p)
flix.set_param('CTL_P_P', pitch_p)
print('=== Wait for gyro update...')
print('Gyro: ', flix.wait('gyro'))
+1 -1
View File
@@ -13,7 +13,7 @@ lines = []
print('Downloading log...')
count = 0
dev.write('log\n'.encode())
dev.write('log dump\n'.encode())
while True:
line = dev.readline()
if not line:
+1
View File
@@ -43,6 +43,7 @@ records = [record for record in records if record[0] != 0]
print(f'Received records: {len(records)}')
os.makedirs(f'{DIR}/log', exist_ok=True)
log = open(f'{DIR}/log/{datetime.datetime.now().isoformat()}.csv', 'wb')
log.write(header.encode() + b'\n')
for record in records:
+76
View File
@@ -0,0 +1,76 @@
#!/usr/bin/env python3
"""Convert flight from Flix format to CSV
Usage:
log_to_csv.py <input_file>
"""
import os
from pyflix import Flix
import docopt
import struct
import csv
DIR = os.path.dirname(os.path.realpath(__file__))
HEADER_FILE = os.path.join(DIR, 'log/log_header.txt')
# Read log header
try:
# read from file
header = open(HEADER_FILE, 'r').read()
except FileNotFoundError:
flix = Flix()
header = flix.cli('log header') # receive the log schema
open(HEADER_FILE, 'w').write(header) # save to file
# Parse log header
topics = []
for line in header.splitlines():
if not line.startswith(' '):
topics.append([])
elif 'not logged' not in line:
topics[-1].append(line.strip())
# Read log file
args = docopt.docopt(__doc__)
input_file = args['<input_file>']
outfile_file = input_file + '.csv'
data = open(input_file, 'rb').read()
# Search for sync marker
SYNC_MARKER = bytes.fromhex('1A 91 4F F6 7F')
sync_offset = data.find(SYNC_MARKER)
if sync_offset == -1:
raise ValueError('Sync marker not found in log file')
data = data[sync_offset + len(SYNC_MARKER):]
data = data.replace(SYNC_MARKER, b'') # remove all other sync markers
header_row = [f'{value}' for topic in topics for value in topic]
rows = []
offset = 0
while offset < len(data):
try:
topic = struct.unpack_from('B', data, offset)[0]
offset += 1
if topic >= len(topics):
raise ValueError(f'Invalid topic {topic} at offset {offset}')
if topic == 0 or not rows:
rows.append({})
for name in topics[topic]:
value = struct.unpack_from('<f', data, offset)[0]
offset += 4
rows[-1][name] = value
except struct.error as e:
break
# Write CSV file
with open(outfile_file, 'w', newline='') as f:
writer = csv.DictWriter(f, fieldnames=header_row, extrasaction='ignore')
writer.writeheader()
rows = filter(lambda row: float(row.get('t', 0)), rows)
writer.writerows(rows)
+27 -20
View File
@@ -24,19 +24,22 @@ pip install pyflix
The API is accessed through the `Flix` class:
```python
from flix import Flix
from pyflix import Flix
flix = Flix() # create a Flix object and wait for connection
```
If using ESP-NOW connection, specify the proxy device name in `FLIX_DEVICE` environment variable or pass it to the constructor: `Flix(device='/dev/cu.usbserial-0001')`.
### Telemetry
Basic telemetry is available through object properties. The property names generally match the corresponding variables in the firmware itself:
Basic telemetry is available through object properties. The property names generally match the corresponding variables in the firmware code:
```python
print(flix.connected) # True if connected to the drone
print(flix.mode) # current flight mode (str)
print(flix.armed) # True if the drone is armed
print(flix.landed) # True if the drone is landed
print(flix.voltage) # battery voltage (NaN - unknown, ~0 - USB powered)
print(flix.attitude) # attitude quaternion [w, x, y, z]
print(flix.attitude_euler) # attitude as Euler angles [roll, pitch, yaw]
print(flix.rates) # angular rates [roll_rate, pitch_rate, yaw_rate]
@@ -92,17 +95,18 @@ Full list of events:
|-----|-----------|----------------|
|`connected`|Connected to the drone||
|`disconnected`|Connection is lost||
|`armed`|Armed state update|Armed state (*bool*)|
|`mode`|Flight mode update|Flight mode (*str*)|
|`landed`|Landed state update|Landed state (*bool*)|
|`print`|The drone sends text to the console|Text|
|`attitude`|Attitude update|Attitude quaternion (*list*)|
|`attitude_euler`|Attitude update|Euler angles (*list*)|
|`rates`|Angular rates update|Angular rates (*list*)|
|`channels`|Raw RC channels update|Raw RC channels (*list*)|
|`motors`|Motor outputs update|Motor outputs (*list*)|
|`acc`|Accelerometer update|Accelerometer output (*list*)|
|`gyro`|Gyroscope update|Gyroscope output (*list*)|
|`armed`|Armed state update|Armed state *(bool)*|
|`mode`|Flight mode update|Flight mode *(str)*|
|`landed`|Landed state update|Landed state *(bool)*|
|`voltage`|Battery voltage update|Voltage *(float)*|
|`print`|The drone prints text to the console|Text|
|`attitude`|Attitude update|Attitude quaternion *(list)*|
|`attitude_euler`|Attitude update|Euler angles *(list)*|
|`rates`|Angular rates update|Angular rates *(list)*|
|`channels`|Raw RC channels update|Raw RC channels *(list)*|
|`motors`|Motor outputs update|Motor outputs *(list)*|
|`acc`|Accelerometer update|Accelerometer output *(list)*|
|`gyro`|Gyroscope update|Gyroscope output *(list)*|
|`mavlink`|Received MAVLink message|Message object|
|`mavlink.<message_name>`|Received specific MAVLink message|Message object|
|`mavlink.<message_id>`|Received specific MAVLink message|Message object|
@@ -112,13 +116,13 @@ Full list of events:
> [!NOTE]
> Update events trigger on every new piece of data from the drone, and do not mean the value has changed.
### Common methods
### Basic methods
Get and set firmware parameters using `get_param` and `set_param` methods:
```python
pitch_p = flix.get_param('PITCH_P') # get parameter value
flix.set_param('PITCH_P', 5) # set parameter value
pitch_p = flix.get_param('CTL_P_P') # get parameter value
flix.set_param('CTL_P_P', 5) # set parameter value
```
Execute console commands using `cli` method. This method returns the command response:
@@ -218,6 +222,13 @@ The following scripts demonstrate how to use the library:
* [`log.py`](../log.py) — download flight logs from the drone.
* [`example.py`](../example.py) — a simple example, prints telemetry data and waits for events.
> [!TIP]
> Set `FLIX_DEVICE` environment variable to use these tools with ESP-NOW connection, for example:
>
> ```bash
> FLIX_DEVICE=/dev/cu.usbserial-0001 tools/cli.py
> ```
## Advanced usage
### MAVLink
@@ -277,7 +288,3 @@ logger = logging.getLogger('flix')
logger.setLevel(logging.DEBUG) # be more verbose
logger.setLevel(logging.WARNING) # be less verbose
```
## Stability
The library is in development stage. The API is not stable.
+26 -14
View File
@@ -5,6 +5,7 @@
import os
import time
import math
from queue import Queue, Empty
from typing import Optional, Callable, List, Dict, Any, Union, Sequence
import logging
@@ -26,6 +27,7 @@ class Flix:
mode: str = ''
armed: bool = False
landed: bool = False
voltage: float = math.nan
attitude: List[float]
attitude_euler: List[float] # roll, pitch, yaw
rates: List[float]
@@ -42,22 +44,27 @@ class Flix:
_print_buffer: str = ''
_modes = ['RAW', 'ACRO', 'STAB', 'AUTO']
def __init__(self, system_id: int=1, wait_connection: bool=True):
def __init__(self, system_id: int=1, wait_connection: bool=True, device=os.getenv('FLIX_DEVICE')):
if not (0 <= system_id < 256):
raise ValueError('system_id must be in range [0, 255]')
self._setup_mavlink()
self.system_id = system_id
self._init_state()
try:
# Direct connection
logger.debug('Listening on port 14550')
self.connection: mavutil.mavfile = mavutil.mavlink_connection('udpin:0.0.0.0:14550', source_system=255) # type: ignore
except OSError as e:
if e.errno != errno.EADDRINUSE:
raise
# Port busy - using proxy
logger.debug('Listening on port 14555 (proxy)')
self.connection: mavutil.mavfile = mavutil.mavlink_connection('udpin:0.0.0.0:14555', source_system=254) # type: ignore
if device is not None:
# User defined connection
logger.debug(f'Connecting to {device}')
self.connection: mavutil.mavfile = mavutil.mavlink_connection(device, source_system=255) # type: ignore
else:
try:
# Direct connection
logger.debug('Listening on port 14550')
self.connection: mavutil.mavfile = mavutil.mavlink_connection('udpin:0.0.0.0:14550', source_system=255) # type: ignore
except OSError as e:
if e.errno != errno.EADDRINUSE:
raise
# Port busy - using proxy
logger.debug('Listening on port 14555 (proxy)')
self.connection: mavutil.mavfile = mavutil.mavlink_connection('udpin:0.0.0.0:14555', source_system=254) # type: ignore
self.connection.target_system = system_id
self.mavlink: mavlink.MAVLink = self.connection.mav
self._event_listeners: Dict[str, List[Callable[..., Any]]] = {}
@@ -68,7 +75,7 @@ class Flix:
self._heartbeat_thread.start()
if wait_connection:
self.wait('mavlink.HEARTBEAT')
time.sleep(0.2) # give some time to receive initial state
time.sleep(0.6) # give some time to receive initial state
def _init_state(self):
self.attitude = [1, 0, 0, 0]
@@ -138,7 +145,7 @@ class Flix:
while True:
try:
msg: Optional[mavlink.MAVLink_message] = self.connection.recv_match(blocking=True)
if msg is None:
if msg is None or msg.get_srcSystem() != self.system_id:
continue
self._connected()
msg_dict = msg.to_dict()
@@ -185,11 +192,16 @@ class Flix:
self._trigger('motors', self.motors)
if isinstance(msg, mavlink.MAVLink_scaled_imu_message):
self.acc = self._mavlink_to_flu([msg.xacc / 1000, msg.yacc / 1000, msg.zacc / 1000])
ONE_G = 9.80665
self.acc = self._mavlink_to_flu([msg.xacc * ONE_G / 1000, msg.yacc * ONE_G / 1000, msg.zacc * ONE_G / 1000])
self.gyro = self._mavlink_to_flu([msg.xgyro / 1000, msg.ygyro / 1000, msg.zgyro / 1000])
self._trigger('acc', self.acc)
self._trigger('gyro', self.gyro)
if isinstance(msg, mavlink.MAVLink_battery_status_message):
self.voltage = msg.voltages[0] / 1000
self._trigger('voltage', self.voltage)
if isinstance(msg, mavlink.MAVLink_serial_control_message):
# new chunk of data
text = bytes(msg.data)[:msg.count].decode('utf-8', errors='ignore')
+1 -1
View File
@@ -1,6 +1,6 @@
[project]
name = "pyflix"
version = "0.11"
version = "0.16"
description = "Python API for Flix drone"
authors = [{ name="Oleg Kalachev", email="okalachev@gmail.com" }]
license = "MIT"