74 Commits

Author SHA1 Message Date
Oleg Kalachev
0908674a60 Add level calibration 2025-12-26 11:29:12 +03:00
Oleg Kalachev
13a7e67b92 Add parameters for IMU orientation definition 2025-12-26 06:29:19 +03:00
Oleg Kalachev
0547ea548b Add parameters for acc weight and rates lpf alpha 2025-12-24 05:43:55 +03:00
Oleg Kalachev
c02dba6812 Rename gyroCalibrationFilter to gyroBiasFilter
Which seems a better name
2025-12-24 05:36:43 +03:00
Oleg Kalachev
f1dc4a0400 Updates to user builds article 2025-12-17 02:21:51 +03:00
Oleg Kalachev
158827ac55 Add new user builds, add school 548 course overview
+ minor doc fixes.
2025-12-13 21:09:33 +03:00
Oleg Kalachev
36ca30c3e4 Minor docs fix 2025-11-27 18:34:32 +03:00
Oleg Kalachev
48711b55e1 Add tip about CNT_TILT_MAX parameter to the simulator article 2025-11-26 17:34:08 +03:00
Oleg Kalachev
4d583185a9 Rename manual mode to raw mode
Make it callable from the console.
Increase the coefficient.
Corresponding change in pyflix.
pyflix@0.11.
2025-11-25 04:44:16 +03:00
Oleg Kalachev
d757ffa853 Move yaw dead zone handling from mavlink to control subsystem
So yaw dead zone works the same for rc and mavlink.
2025-11-22 05:11:46 +03:00
Oleg Kalachev
5352386486 Minor updates to pyflix library, pyflix@0.10
Fixes to documentation.
Improve logger format.
2025-11-22 05:07:46 +03:00
Oleg Kalachev
9b5872740f Add wifi cli command
To show wi-fi info.
2025-11-22 04:46:54 +03:00
Oleg Kalachev
31dbdaf241 Group control parameters
Also add IMU group to accelerometer calibration parameters.
2025-11-19 01:50:46 +03:00
Oleg Kalachev
f4b56262b1 Remove unneeded SERIAL_BAUDRATE define 2025-11-14 20:23:15 +03:00
Oleg Kalachev
49039f752d Refactor Wi-Fi log download
Use MAVLink LOG_REQUEST_DATA and LOG_DATA for download log instead of console.
Make Wi-Fi download default way of downloading the log.
Make `log` command only print the header and `log dump` dump the log.
2025-11-14 20:21:05 +03:00
Oleg Kalachev
348721acc9 Updates in documentation
Fixes, updates, new illustrations.
2025-11-10 20:16:14 +03:00
Oleg Kalachev
774144c430 Many updates to documentation
Updates to main readme.
Add much more info to usage article.
Move simulator building to simulation's readme.
Improve assembly article.
Many fixes.
Updates in diagrams.
2025-11-06 13:55:52 +03:00
Oleg Kalachev
0e6651ab82 Add Rate class for running the code at fixed rate 2025-11-06 13:41:33 +03:00
Oleg Kalachev
1a017ccb97 Keep only one floating point version of map function
Two variants are redundant
2025-11-02 00:02:28 +03:00
Oleg Kalachev
7170b20d1d Simplify command for command handling 2025-10-21 19:41:10 +03:00
Oleg Kalachev
dc9aed113b Minor code fixes 2025-10-21 19:41:05 +03:00
Oleg Kalachev
08b6123eb7 Fixes to troubleshooting 2025-10-21 19:40:54 +03:00
Oleg Kalachev
1a8b63ee04 Send only mavlink heartbeats until connected 2025-10-21 19:39:17 +03:00
Oleg Kalachev
8c49a40516 Skip attitude/rate control if thrustTarget is ineffective
To prevent i term windup.
2025-10-20 23:01:17 +03:00
Oleg Kalachev
ca595edce5 Refactor PID control to simplify the code and modifications
Each PID uses its internal dt, so may be various contexts with different rate.
PID has max dt, so no need to reset explicitly.
2025-10-20 22:54:18 +03:00
KiraFlux
d06eb2a1aa Quaternion::fromBetweenVectors: pass u and v as const references (#21) 2025-10-19 20:46:46 +03:00
Oleg Kalachev
e50a9d5fea Revert t variable type to float instead of double
For the sake of simplicity and consistency.
2025-10-19 20:46:38 +03:00
Oleg Kalachev
ebac78dc0f Minor change 2025-10-19 20:46:26 +03:00
Oleg Kalachev
186cf88d84 Add generic Delay filter 2025-10-19 20:46:11 +03:00
Oleg Kalachev
253aae2220 Lowercase imu and rc variables
To make it more obvious these are variables, not classes.
2025-10-19 20:45:56 +03:00
Oleg Kalachev
6f0964fac4 Rename failsafe.ino to safety.ino
To aggregate all the safety related functionality.
2025-10-19 20:44:54 +03:00
Oleg Kalachev
1d034f268d Add ESP32-S3 build to Actions 2025-10-19 20:44:46 +03:00
Oleg Kalachev
1ca7d32862 Update VSCode settings
Disable error squiggles as they often work incorrectly.
Decrease number of include libraries to index.
2025-10-14 11:43:55 +03:00
Oleg Kalachev
ab941e34fa Fix Gazebo installation
Installation script is deprecated, install using package on Ubuntu 20.04
2025-10-13 18:56:14 +03:00
Oleg Kalachev
7bee3d1751 Improve rc failsafe logic
Don't trigger failsafe if there's no RC at all
Use AUTO mode for descending, instead of STAB
Increase RC loss timeout and descend time
2025-10-12 21:27:08 +03:00
Oleg Kalachev
06ec5f3160 Disarm the drone on simulator plugin reset
In order to reset yaw target.
2025-10-07 15:45:48 +03:00
Oleg Kalachev
c4533e3ac8 Reset yaw target when drone disarmed
Prevent unexpected behavior when the drone tries to restore its old yaw on takeoff.
2025-10-07 15:43:28 +03:00
Oleg Kalachev
e673b50f52 Include FlixPeriph header instead of MPU9250
This simplifies choosing IMU model
2025-10-07 08:43:12 +03:00
Oleg Kalachev
5151bb9133 Ensure showing correct raw data in imu command
Some IMUs will reset acc and gyro buffer on whoAmI() call
2025-10-07 08:43:06 +03:00
Oleg Kalachev
c08c8ad91c pyflix@0.9 2025-10-03 06:49:44 +03:00
Oleg Kalachev
e44f32fca7 pyflix: don't quit on any sendto error 2025-10-03 06:47:56 +03:00
Oleg Kalachev
ca03bdb260 pyflix: partially fix wireless downloading logs 2025-10-03 06:46:56 +03:00
Oleg Kalachev
b3dffe99fb pyflix: add passing event name to off method 2025-10-03 06:46:29 +03:00
Oleg Kalachev
6e6a71fa69 Remove unneeded advice from troubleshooting 2025-10-03 06:45:16 +03:00
Oleg Kalachev
838fe11f6b Simplify mode index check in set_mode 2025-09-26 05:03:36 +03:00
Oleg Kalachev
8b36509932 pyflix@0.8 2025-09-25 16:55:06 +03:00
Oleg Kalachev
0268c8ebcf Some fixes and updates in pyflix
Fix set_controls
Add set_armed method
2025-09-25 16:53:49 +03:00
Oleg Kalachev
09bf09e520 Update schematics diagram 2025-09-25 06:16:02 +03:00
Oleg Kalachev
4c89b10767 Fix fields order in psq command 2025-09-20 22:35:36 +03:00
Oleg Kalachev
a79df52959 Don't trigger rc failsafe in AUTO mode or if disamed 2025-09-20 20:36:36 +03:00
Oleg Kalachev
e88888baeb Fix rc calibration steps enumeration again 2025-09-11 11:47:28 +03:00
Oleg Kalachev
de69b228ff Fix rc calibration steps enumeration 2025-09-02 11:03:44 +03:00
Oleg Kalachev
f9739dcd7e Don't arm by mavlink command if throttle is not low 2025-08-29 03:47:51 +03:00
Oleg Kalachev
708c8f04dc Minor docs fix 2025-08-28 05:17:46 +03:00
Oleg Kalachev
2128201440 Fix simulation build 2025-08-28 01:13:38 +03:00
Oleg Kalachev
8e3c86f5ee pyflix@0.7 2025-08-28 00:52:27 +03:00
Oleg Kalachev
40fc4b96b5 Implement AUTO mode for automatic flights
Support SET_ATTITUDE_TARGET, SET_ACTUATOR_CONTROL_TARGET in mavlink.
ACTUATOR_OUTPUT_STATUS is changed ACTUATOR_CONTROL_TARGET to match used message for setting motor outputs.
Add support for changing mode from mavlink.
Support automatic flights in pyflix.
2025-08-28 00:49:24 +03:00
Oleg Kalachev
10fafbc4a0 Send udp packets in unicast after connection is established
This makes qgc connection faster.
Add WIFI_UDP_REMOTE_ADDR macro for default remote address for both the firmware and simulation.
2025-08-27 05:01:07 +03:00
Oleg Kalachev
d47d7b8bd4 Support arm/disarm mavlink commands
Refactor commands handling to remove repeating ack message packing.
2025-08-27 04:45:25 +03:00
Oleg Kalachev
a7fdc2a88f Minor change in cli help message 2025-08-27 04:43:24 +03:00
Oleg Kalachev
c1788e2c75 Refactor arming logic
Arm and disarm with gestures only: left stick right/down for arming, left/down for disarming.
Remove arming switch as it complicates arming gestures logic.
Remove MAV_CTRL_SCALE parameter as it complicates arming gestures logic, advise to decrease TILT_MAX when controlling with a smartphone.
Put some minimal thrust to motors to indicate armed state.
Rename build article to usage article, add flight instructions.
2025-08-27 03:19:26 +03:00
Oleg Kalachev
beb655fdcb Add illustration for qgc proxy for pyflix 2025-08-27 03:13:28 +03:00
Oleg Kalachev
bf0cdac111 Major update of the articles
Reflect control subsystem refactoring.
Update dataflow diagram.
Add control subsystem diagram.
Minor updates.
2025-08-27 00:09:42 +03:00
Oleg Kalachev
b21e81a68b Add cli commands for switching mode
Make mode variable int instead of enum, which is more convinient.
2025-08-26 21:55:27 +03:00
Oleg Kalachev
8418723ccc Refactor control subsystem
Add interpretControls function to convert pilot commands and mode into control targets and make control functions independent from the mode.
Add ratesExtra target for rates feed-forward; remove yawMode.
Rename controlRate to controlRates to reflect rates variable name.
Remove USER mode.
2025-08-26 01:00:56 +03:00
Oleg Kalachev
a1539157b8 Show raw values in imu command 2025-08-22 17:20:33 +03:00
Oleg Kalachev
80922dc68a Some updates to readme and build article
Add info on using USB gamepad
Replace KINGKONG transmitter with BetaFPV LiteRadio
Add RoboCamp video
2025-08-20 22:06:17 +03:00
Oleg Kalachev
fcd2738763 Add link to stls from robocamp 2025-08-19 15:20:24 +03:00
Oleg Kalachev
fa07ed3a4e Minor docs change 2025-08-15 00:51:08 +03:00
Oleg Kalachev
dee4d97ab3 Add getRoll, getPitch, setRoll, setPitch methods
Add methods to Quaternion for consistency with getYaw and setYaw
2025-08-09 18:10:11 +03:00
Oleg Kalachev
ea35db37da Minor code simplification 2025-08-09 17:53:06 +03:00
Oleg Kalachev
cd953f24ad Add RoboCamp to built drones article 2025-08-07 14:29:39 +03:00
Oleg Kalachev
3f80712641 Some updates to articles 2025-08-06 23:52:35 +03:00
Oleg Kalachev
18bacb64f3 Make rc loss timeout longer 2025-07-31 12:35:28 +03:00
85 changed files with 1806 additions and 1278 deletions

View File

@@ -23,7 +23,9 @@ jobs:
with: with:
name: firmware-binary name: firmware-binary
path: flix/build path: flix/build
- name: Build firmware without Wi-Fi - 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$/#define WIFI_ENABLED 0/' flix/flix.ino && make run: sed -i 's/^#define WIFI_ENABLED 1$/#define WIFI_ENABLED 0/' flix/flix.ino && make
- name: Check c_cpp_properties.json - name: Check c_cpp_properties.json
run: tools/check_c_cpp_properties.py run: tools/check_c_cpp_properties.py
@@ -53,15 +55,25 @@ jobs:
run: python3 tools/check_c_cpp_properties.py run: python3 tools/check_c_cpp_properties.py
build_simulator: build_simulator:
runs-on: ubuntu-22.04 runs-on: ubuntu-latest
container:
image: ubuntu:20.04
steps: steps:
- name: Install dependencies
run: |
apt-get update
DEBIAN_FRONTEND=noninteractive apt-get install -y curl wget build-essential cmake g++ pkg-config gnupg2 lsb-release sudo
- name: Install Arduino CLI - name: Install Arduino CLI
uses: arduino/setup-arduino-cli@v1.1.1 uses: arduino/setup-arduino-cli@v1.1.1
- uses: actions/checkout@v4 - uses: actions/checkout@v4
- name: Install Gazebo - name: Install Gazebo
run: curl -sSL http://get.gazebosim.org | sh run: |
sudo sh -c 'echo "deb http://packages.osrfoundation.org/gazebo/ubuntu-stable `lsb_release -cs` main" > /etc/apt/sources.list.d/gazebo-stable.list'
wget https://packages.osrfoundation.org/gazebo.key -O - | sudo apt-key add -
sudo apt-get update
sudo apt-get install -y gazebo11 libgazebo11-dev
- name: Install SDL2 - name: Install SDL2
run: sudo apt-get install libsdl2-dev run: sudo apt-get install -y libsdl2-dev
- name: Build simulator - name: Build simulator
run: make build_simulator run: make build_simulator
- uses: actions/upload-artifact@v4 - uses: actions/upload-artifact@v4

View File

@@ -7,6 +7,7 @@
"MD024": false, "MD024": false,
"MD033": false, "MD033": false,
"MD034": false, "MD034": false,
"MD059": false,
"MD044": { "MD044": {
"html_elements": false, "html_elements": false,
"code_blocks": false, "code_blocks": false,
@@ -64,5 +65,6 @@
"PX4" "PX4"
] ]
}, },
"MD045": false "MD045": false,
"MD060": false
} }

View File

@@ -5,13 +5,15 @@
"includePath": [ "includePath": [
"${workspaceFolder}/flix", "${workspaceFolder}/flix",
"${workspaceFolder}/gazebo", "${workspaceFolder}/gazebo",
"${workspaceFolder}/tools/**",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32", "~/.arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**", "~/.arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32", "~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/**", "~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/**",
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include", "~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
"~/Arduino/libraries/**", "~/Arduino/libraries/**",
"/usr/include/**" "/usr/include/gazebo-11/",
"/usr/include/ignition/math6/"
], ],
"forcedInclude": [ "forcedInclude": [
"${workspaceFolder}/.vscode/intellisense.h", "${workspaceFolder}/.vscode/intellisense.h",
@@ -51,14 +53,14 @@
"name": "Mac", "name": "Mac",
"includePath": [ "includePath": [
"${workspaceFolder}/flix", "${workspaceFolder}/flix",
// "${workspaceFolder}/gazebo",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32", "~/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/libraries/**",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32", "~/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/include/**",
"~/Library/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include", "~/Library/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
"~/Documents/Arduino/libraries/**", "~/Documents/Arduino/libraries/**",
"/opt/homebrew/include/**" "/opt/homebrew/include/gazebo-11/",
"/opt/homebrew/include/ignition/math6/"
], ],
"forcedInclude": [ "forcedInclude": [
"${workspaceFolder}/.vscode/intellisense.h", "${workspaceFolder}/.vscode/intellisense.h",
@@ -100,6 +102,7 @@
"includePath": [ "includePath": [
"${workspaceFolder}/flix", "${workspaceFolder}/flix",
"${workspaceFolder}/gazebo", "${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/cores/esp32",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**", "~/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/hardware/esp32/3.2.0/variants/d1_mini32",

View File

@@ -1,5 +1,6 @@
{ {
"C_Cpp.intelliSenseEngineFallback": "enabled", "C_Cpp.intelliSenseEngineFallback": "enabled",
"C_Cpp.errorSquiggles": "disabled",
"files.associations": { "files.associations": {
"*.sdf": "xml", "*.sdf": "xml",
"*.ino": "cpp", "*.ino": "cpp",

View File

@@ -32,7 +32,7 @@ simulator: build_simulator
gazebo --verbose ${CURDIR}/gazebo/flix.world gazebo --verbose ${CURDIR}/gazebo/flix.world
log: log:
PORT=$(PORT) tools/grab_log.py tools/log.py
plot: plot:
plotjuggler -d $(shell ls -t tools/log/*.csv | head -n1) plotjuggler -d $(shell ls -t tools/log/*.csv | head -n1)

109
README.md
View File

@@ -1,6 +1,6 @@
# Flix # Flix
**Flix** (*flight + X*) — making an open source ESP32-based quadcopter from scratch. **Flix** (*flight + X*) — open source ESP32-based quadcopter made from scratch.
<table> <table>
<tr> <tr>
@@ -17,11 +17,11 @@
* Dedicated for education and research. * Dedicated for education and research.
* Made from general-purpose components. * Made from general-purpose components.
* Simple and clean source code in Arduino. * Simple and clean source code in Arduino (<2k lines firmware).
* Control using remote control or smartphone. * Control using USB gamepad, remote control or smartphone.
* Precise simulation with Gazebo.
* Wi-Fi and MAVLink support. * Wi-Fi and MAVLink support.
* Wireless command line interface and analyzing. * Wireless command line interface and analyzing.
* Precise simulation with Gazebo.
* Python library. * Python library.
* Textbook on flight control theory and practice ([in development](https://quadcopter.dev)). * Textbook on flight control theory and practice ([in development](https://quadcopter.dev)).
* *Position control (using external camera) and autonomous flights¹*. * *Position control (using external camera) and autonomous flights¹*.
@@ -38,7 +38,11 @@ Version 0 demo video: https://youtu.be/8GzzIQ3C6DQ.
<a href="https://youtu.be/8GzzIQ3C6DQ"><img width=500 src="https://i3.ytimg.com/vi/8GzzIQ3C6DQ/maxresdefault.jpg"></a> <a href="https://youtu.be/8GzzIQ3C6DQ"><img width=500 src="https://i3.ytimg.com/vi/8GzzIQ3C6DQ/maxresdefault.jpg"></a>
See the [user builds gallery](docs/user.md). Usage in education (RoboCamp): https://youtu.be/Wd3yaorjTx0.
<a href="https://youtu.be/Wd3yaorjTx0"><img width=500 src="https://i3.ytimg.com/vi/Wd3yaorjTx0/sddefault.jpg"></a>
See the [user builds gallery](docs/user.md):
<a href="docs/user.md"><img src="docs/img/user/user.jpg" width=500></a> <a href="docs/user.md"><img src="docs/img/user/user.jpg" width=500></a>
@@ -48,25 +52,29 @@ The simulator is implemented using Gazebo and runs the original Arduino code:
<img src="docs/img/simulator1.png" width=500 alt="Flix simulator"> <img src="docs/img/simulator1.png" width=500 alt="Flix simulator">
## Articles ## Documentation
1. [Assembly instructions](docs/assembly.md).
2. [Usage: build, setup and flight](docs/usage.md).
3. [Simulation](gazebo/README.md).
4. [Python library](tools/pyflix/README.md).
Additional articles:
* [Assembly instructions](docs/assembly.md).
* [Building and running the code](docs/build.md).
* [Troubleshooting](docs/troubleshooting.md).
* [Firmware architecture overview](docs/firmware.md).
* [Python library tutorial](tools/pyflix/README.md).
* [Log analysis](docs/log.md).
* [User builds gallery](docs/user.md). * [User builds gallery](docs/user.md).
* [Firmware architectural overview](docs/firmware.md).
* [Troubleshooting](docs/troubleshooting.md).
* [Log analysis](docs/log.md).
## Components ## Components
|Type|Part|Image|Quantity| |Type|Part|Image|Quantity|
|-|-|:-:|:-:| |-|-|:-:|:-:|
|Microcontroller board|ESP32 Mini|<img src="docs/img/esp32.jpg" width=100>|1| |Microcontroller board|ESP32 Mini|<img src="docs/img/esp32.jpg" width=100>|1|
|IMU (and barometer²) board|GY91, MPU-9265 (or other MPU9250/MPU6500 board)<br>ICM20948³<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| |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|
|<span style="background:yellow">(Recommended) Buck-boost converter</span>|To be determined, output 5V or 3.3V, see [user-contributed schematics](https://miro.com/app/board/uXjVN-dTjoo=/?moveToWidget=3458764612179508274&cot=14)|<img src="docs/img/buck-boost.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 (shaft 0.8mm).<br>Motor with exact 3.7V voltage is needed, not ranged working voltage (3.7V — 6V).|<img src="docs/img/motor.jpeg" width=100>|4| |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|Hubsan 55 mm|<img src="docs/img/prop.jpg" 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| |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| |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| |3.7V Li-Po battery|LW 952540 (or any compatible by the size)|<img src="docs/img/battery.jpg" width=100>|1|
@@ -74,19 +82,17 @@ The simulator is implemented using Gazebo and runs the original Arduino code:
|Li-Po Battery charger|Any|<img src="docs/img/charger.jpg" 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| |Screws for IMU board mounting|M3x5|<img src="docs/img/screw-m3.jpg" width=100>|2|
|Screws for frame assembly|M1.4x5|<img src="docs/img/screw-m1.4.jpg" height=30 align=center>|4| |Screws for frame assembly|M1.4x5|<img src="docs/img/screw-m1.4.jpg" height=30 align=center>|4|
|Frame main part|3D printed⁴:<br>[`flix-frame-1.1.stl`](docs/assets/flix-frame-1.1.stl) [`flix-frame-1.1.step`](docs/assets/flix-frame-1.1.step)<br>Recommended settings: layer 0.2 mm, line 0.4 mm, infill 100%.|<img src="docs/img/frame1.jpg" width=100>|1| |Frame main part|3D printed²: [`stl`](docs/assets/flix-frame-1.1.stl) [`step`](docs/assets/flix-frame-1.1.step)<br>Recommended settings: layer 0.2 mm, line 0.4 mm, infill 100%.|<img src="docs/img/frame1.jpg" width=100>|1|
|Frame top part|3D printed:<br>[`esp32-holder.stl`](docs/assets/esp32-holder.stl) [`esp32-holder.step`](docs/assets/esp32-holder.step)|<img src="docs/img/esp32-holder.jpg" width=100>|1| |Frame top part|3D printed: [`stl`](docs/assets/esp32-holder.stl) [`step`](docs/assets/esp32-holder.step)|<img src="docs/img/esp32-holder.jpg" width=100>|1|
|Washer for IMU board mounting|3D printed:<br>[`washer-m3.stl`](docs/assets/washer-m3.stl) [`washer-m3.step`](docs/assets/washer-m3.step)|<img src="docs/img/washer-m3.jpg" width=100>|2| |Washer for IMU board mounting|3D printed: [`stl`](docs/assets/washer-m3.stl) [`step`](docs/assets/washer-m3.step)|<img src="docs/img/washer-m3.jpg" width=100>|2|
|*RC transmitter (optional)*|*KINGKONG TINY X8 (warning: lacks USB support) or other⁵*|<img src="docs/img/tx.jpg" width=100>|1| |Controller (recommended)|CC2500 transmitter, like BetaFPV LiteRadio CC2500 (RC receiver/Wi-Fi).<br>Two-sticks gamepad (Wi-Fi only) — see [recommended gamepads](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/setup_view/joystick.html#supported-joysticks).<br>Other⁵|<img src="docs/img/betafpv.jpg" width=100><img src="docs/img/logitech.jpg" width=80>|1|
|*RC receiver (optional)*|*DF500 or other*|<img src="docs/img/rx.jpg" width=100>|1| |*RC receiver (optional)*|*DF500 or other³*|<img src="docs/img/rx.jpg" width=100>|1|
|Wires|28 AWG recommended|<img src="docs/img/wire-28awg.jpg" width=100>|| |Wires|28 AWG recommended|<img src="docs/img/wire-28awg.jpg" width=100>||
|Tape, double-sided tape|||| |Tape, double-sided tape||||
*² barometer is not used for now.*<br> *¹ barometer is not used for now.*<br>
*³ — change `MPU9250` to `ICM20948` in `imu.ino` file if using ICM-20948 board.*<br> *² — this frame is optimized for GY-91 board, if using other, the board mount holes positions should be modified.*<br>
*³⁻¹ — MPU-6050 supports I²C interface only (not recommended). To use it change IMU declaration to `MPU6050 IMU(Wire)`.*<br> *³ — you also may use any transmitter-receiver pair with SBUS interface.*
*⁴ — this frame is optimized for GY-91 board, if using other, the board mount holes positions should be modified.*<br>
*⁵ — you may use any transmitter-receiver pair with SBUS interface.*
Tools required for assembly: Tools required for assembly:
@@ -96,13 +102,15 @@ Tools required for assembly:
* Screwdrivers. * Screwdrivers.
* Multimeter. * Multimeter.
Feel free to modify the design and or code, and create your own improved versions of Flix! Send your results to the [official Telegram chat](https://t.me/opensourcequadcopterchat), or directly to the author ([E-mail](mailto:okalachev@gmail.com), [Telegram](https://t.me/okalachev)). Feel free to modify the design and or code, and create your own improved versions. Send your results to the [official Telegram chat](https://t.me/opensourcequadcopterchat), or directly to the author ([E-mail](mailto:okalachev@gmail.com), [Telegram](https://t.me/okalachev)).
## Schematics ## Schematics
### Simplified connection diagram ### Simplified connection diagram
<img src="docs/img/schematics1.svg" width=800 alt="Flix version 1 schematics"> <img src="docs/img/schematics1.svg" width=700 alt="Flix version 1 schematics">
*(Dashed elements are optional).*
Motor connection scheme: Motor connection scheme:
@@ -110,8 +118,6 @@ Motor connection scheme:
You can see a user-contributed [variant of complete circuit diagram](https://miro.com/app/board/uXjVN-dTjoo=/?moveToWidget=3458764612338222067&cot=14) of the drone. You can see a user-contributed [variant of complete circuit diagram](https://miro.com/app/board/uXjVN-dTjoo=/?moveToWidget=3458764612338222067&cot=14) of the drone.
See [assembly guide](docs/assembly.md) for instructions on assembling the drone.
### Notes ### Notes
* Power ESP32 Mini with Li-Po battery using VCC (+) and GND (-) pins. * Power ESP32 Mini with Li-Po battery using VCC (+) and GND (-) pins.
@@ -129,14 +135,15 @@ See [assembly guide](docs/assembly.md) for instructions on assembling the drone.
* Solder pull-down resistors to the MOSFETs. * Solder pull-down resistors to the MOSFETs.
* Connect the motors to the ESP32 Mini using MOSFETs, by following scheme: * Connect the motors to the ESP32 Mini using MOSFETs, by following scheme:
|Motor|Position|Direction|Wires|GPIO| |Motor|Position|Direction|Prop type|Motor wires|GPIO|
|-|-|-|-|-| |-|-|-|-|-|-|
|Motor 0|Rear left|Counter-clockwise|Black & White|GPIO12 (*TDI*)| |Motor 0|Rear left|Counter-clockwise|B|Black & White|GPIO12 (*TDI*)|
|Motor 1|Rear right|Clockwise|Blue & Red|GPIO13 (*TCK*)| |Motor 1|Rear right|Clockwise|A|Blue & Red|GPIO13 (*TCK*)|
|Motor 2|Front right|Counter-clockwise|Black & White|GPIO14 (*TMS*)| |Motor 2|Front right|Counter-clockwise|B|Black & White|GPIO14 (*TMS*)|
|Motor 3|Front left|Clockwise|Blue & Red|GPIO15 (*TD0*)| |Motor 3|Front left|Clockwise|A|Blue & Red|GPIO15 (*TD0*)|
Counter-clockwise motors have black and white wires and clockwise motors have blue and red wires. 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.
* Optionally connect the RC receiver to the ESP32's UART2: * Optionally connect the RC receiver to the ESP32's UART2:
@@ -144,32 +151,18 @@ See [assembly guide](docs/assembly.md) for instructions on assembling the drone.
|-|-| |-|-|
|GND|GND| |GND|GND|
|VIN|VCC (or 3.3V depending on the receiver)| |VIN|VCC (or 3.3V depending on the receiver)|
|Signal (TX)|GPIO4| |Signal (TX)|GPIO4¹|
* — 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.* *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.*
### IMU placement ## Resources
Default IMU orientation in the code is **LFD** (Left-Forward-Down): * Telegram channel on developing the drone and the flight controller (in Russian): https://t.me/opensourcequadcopter.
* Official Telegram chat: https://t.me/opensourcequadcopterchat.
<img src="docs/img/gy91-lfd.svg" width=400 alt="GY-91 axes"> * Detailed article on Habr.com about the development of the drone (in Russian): https://habr.com/ru/articles/814127/.
In case of using other IMU orientation, modify the `rotateIMU` function in the `imu.ino` file.
See [FlixPeriph documentation](https://github.com/okalachev/flixperiph?tab=readme-ov-file#imu-axes-orientation) to learn axis orientation of other IMU boards.
## Materials
Subscribe to the Telegram channel on developing the drone and the flight controller (in Russian): https://t.me/opensourcequadcopter.
Join the official Telegram chat: https://t.me/opensourcequadcopterchat.
Detailed article on Habr.com about the development of the drone (in Russian): https://habr.com/ru/articles/814127/.
See the information on the obsolete version 0 in the [corresponding article](docs/version0.md).
## Disclaimer ## Disclaimer
This is a fun DIY project, and I hope you find it interesting and useful. However, it's not easy to assemble and set up, and it's provided "as is" without any warranties. Theres no guarantee that it will work perfectly or even work at all. This is a DIY project, and I hope you find it interesting and useful. However, it's not easy to assemble and set up, and it's provided "as is" without any warranties. There's no guarantee that it will work perfectly, or even work at all.
⚠️ The author is not responsible for any damage, injury, or loss resulting from the use of this project. Use at your own risk! ⚠️ The author is not responsible for any damage, injury, or loss resulting from the use of this project. Use at your own risk!

View File

@@ -27,3 +27,27 @@ Soldered components ([schematics variant](https://miro.com/app/board/uXjVN-dTjoo
<br>Assembled drone: <br>Assembled drone:
<img src="img/assembly/7.jpg" width=600> <img src="img/assembly/7.jpg" width=600>
## Motor directions
> [!WARNING]
> The drone above is an early build, and it has **inversed** motor directions scheme. The photos only illustrate the assembly process in general.
Use standard motor directions scheme:
<img src="img/motors.svg" width=200>
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*)|
## Motors tightening
Motors should be installed very tightly — any vibration may lead to bad attitude estimation and unstable flight. If motors are loose, use tiny tape pieces to fix them tightly as shown below:
<img src="img/motor-tape.jpg" width=600>

View File

@@ -1,8 +1,10 @@
# Архитектура прошивки # Архитектура прошивки
<img src="img/dataflow.svg" width=800 alt="Firmware dataflow diagram"> Прошивка Flix это обычный скетч Arduino, реализованный в однопоточном стиле. Код инициализации находится в функции `setup()`, а главный цикл — в функции `loop()`. Скетч состоит из нескольких файлов, каждый из которых отвечает за определенную подсистему.
Главный цикл работает на частоте 1000 Гц. Передача данных между подсистемами происходит через глобальные переменные: <img src="img/dataflow.svg" width=600 alt="Firmware dataflow diagram">
Главный цикл `loop()` работает на частоте 1000 Гц. Передача данных между подсистемами происходит через глобальные переменные:
* `t` *(float)* — текущее время шага, *с*. * `t` *(float)* — текущее время шага, *с*.
* `dt` *(float)* — дельта времени между текущим и предыдущим шагами, *с*. * `dt` *(float)* — дельта времени между текущим и предыдущим шагами, *с*.
@@ -10,23 +12,39 @@
* `acc` *(Vector)* — данные с акселерометра, *м/с<sup>2</sup>*. * `acc` *(Vector)* — данные с акселерометра, *м/с<sup>2</sup>*.
* `rates` *(Vector)* — отфильтрованные угловые скорости, *рад/с*. * `rates` *(Vector)* — отфильтрованные угловые скорости, *рад/с*.
* `attitude` *(Quaternion)* — оценка ориентации (положения) дрона. * `attitude` *(Quaternion)* — оценка ориентации (положения) дрона.
* `controlRoll`, `controlPitch`, ... *(float[])* — команды управления от пилота, в диапазоне [-1, 1]. * `controlRoll`, `controlPitch`, `controlYaw`, `controlThrottle`, `controlMode` *(float)* — команды управления от пилота, в диапазоне [-1, 1].
* `motors` *(float[])* — выходные сигналы на моторы, в диапазоне [0, 1]. * `motors` *(float[4])* — выходные сигналы на моторы, в диапазоне [0, 1].
## Исходные файлы ## Исходные файлы
Исходные файлы прошивки находятся в директории `flix`. Ключевые файлы: Исходные файлы прошивки находятся в директории `flix`. Основные файлы:
* [`flix.ino`](https://github.com/okalachev/flix/blob/canonical/flix/flix.ino) — основной входной файл, скетч Arduino. Включает определение глобальных переменных и главный цикл. * [`flix.ino`](https://github.com/okalachev/flix/blob/master/flix/flix.ino) — основной файл Arduino-скетча. Определяет некоторые глобальные переменные и главный цикл.
* [`imu.ino`](https://github.com/okalachev/flix/blob/canonical/flix/imu.ino) — чтение данных с датчика IMU (гироскоп и акселерометр), калибровка IMU. * [`imu.ino`](https://github.com/okalachev/flix/blob/master/flix/imu.ino) — чтение данных с датчика IMU (гироскоп и акселерометр), калибровка IMU.
* [`rc.ino`](https://github.com/okalachev/flix/blob/canonical/flix/rc.ino) — чтение данных с RC-приемника, калибровка RC. * [`rc.ino`](https://github.com/okalachev/flix/blob/master/flix/rc.ino) — чтение данных с RC-приемника, калибровка RC.
* [`mavlink.ino`](https://github.com/okalachev/flix/blob/canonical/flix/mavlink.ino) — взаимодействие с QGroundControl через MAVLink. * [`estimate.ino`](https://github.com/okalachev/flix/blob/master/flix/estimate.ino) — оценка ориентации дрона, комплементарный фильтр.
* [`estimate.ino`](https://github.com/okalachev/flix/blob/canonical/flix/estimate.ino) — оценка ориентации дрона, комплементарный фильтр. * [`control.ino`](https://github.com/okalachev/flix/blob/master/flix/control.ino) — подсистема управления, трехмерный двухуровневый каскадный ПИД-регулятор.
* [`control.ino`](https://github.com/okalachev/flix/blob/canonical/flix/control.ino) — управление ориентацией и угловыми скоростями дрона, трехмерный двухуровневый каскадный PID-регулятор. * [`motors.ino`](https://github.com/okalachev/flix/blob/master/flix/motors.ino) — выход PWM на моторы.
* [`motors.ino`](https://github.com/okalachev/flix/blob/canonical/flix/motors.ino) — управление выходными сигналами на моторы через ШИМ. * [`mavlink.ino`](https://github.com/okalachev/flix/blob/master/flix/mavlink.ino) — взаимодействие с QGroundControl или [pyflix](https://github.com/okalachev/flix/tree/master/tools/pyflix) через протокол MAVLink.
Вспомогательные файлы включают: Вспомогательные файлы:
* [`vector.h`](https://github.com/okalachev/flix/blob/canonical/flix/vector.h), [`quaternion.h`](https://github.com/okalachev/flix/blob/canonical/flix/quaternion.h) — реализация библиотек векторов и кватернионов проекта. * [`vector.h`](https://github.com/okalachev/flix/blob/master/flix/vector.h), [`quaternion.h`](https://github.com/okalachev/flix/blob/master/flix/quaternion.h) — библиотеки векторов и кватернионов.
* [`pid.h`](https://github.com/okalachev/flix/blob/canonical/flix/pid.h) — реализация общего ПИД-регулятора. * [`pid.h`](https://github.com/okalachev/flix/blob/master/flix/pid.h) — ПИД-регулятор.
* [`lpf.h`](https://github.com/okalachev/flix/blob/canonical/flix/lpf.h) — реализация общего фильтра нижних частот. * [`lpf.h`](https://github.com/okalachev/flix/blob/master/flix/lpf.h) — фильтр нижних частот.
### Подсистема управления
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*.
* `ratesExtra` *(Vector)* — дополнительные (feed-forward) угловые скорости, для управления рысканием в режиме STAB, *рад/с*.
* `torqueTarget` *(Vector)* — целевой крутящий момент, диапазон [-1, 1].
* `thrustTarget` *(float)* — целевая общая тяга, диапазон [0, 1].
Команда управления обрабатывается в функциях `controlAttitude()`, `controlRates()`, `controlTorque()`. Если значение одной из переменных установлено в `NAN`, то соответствующая функция пропускается.
<img src="img/control.svg" width=300 alt="Control subsystem diagram">
Состояние *armed* хранится в переменной `armed`, а текущий режим — в переменной `mode`.

View File

@@ -1,205 +1,2 @@
# Building and running <!-- markdownlint-disable MD041 -->
Build instructions are moved to [usage article](usage.md).
To build the firmware or the simulator, you need to clone the repository using git:
```bash
git clone https://github.com/okalachev/flix.git
cd flix
```
## Simulation
### Ubuntu
The latest version of Ubuntu supported by Gazebo 11 simulator is 22.04. If you have a newer version, consider using a virtual machine.
1. Install Arduino CLI:
```bash
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
```
2. Install Gazebo 11:
```bash
curl -sSL http://get.gazebosim.org | sh
```
Set up your Gazebo environment variables:
```bash
echo "source /usr/share/gazebo/setup.sh" >> ~/.bashrc
source ~/.bashrc
```
3. Install SDL2 and other dependencies:
```bash
sudo apt-get update && sudo apt-get install build-essential libsdl2-dev
```
4. Add your user to the `input` group to enable joystick support (you need to re-login after this command):
```bash
sudo usermod -a -G input $USER
```
5. Run the simulation:
```bash
make simulator
```
### macOS
1. Install Homebrew package manager, if you don't have it installed:
```bash
/bin/bash -c "$(curl -fsSL https://raw.githubusercontent.com/Homebrew/install/HEAD/install.sh)"
```
2. Install Arduino CLI, Gazebo 11 and SDL2:
```bash
brew tap osrf/simulation
brew install arduino-cli
brew install gazebo11
brew install sdl2
```
Set up your Gazebo environment variables:
```bash
echo "source /opt/homebrew/share/gazebo/setup.sh" >> ~/.zshrc
source ~/.zshrc
```
3. Run the simulation:
```bash
make simulator
```
### Setup and flight
#### Control with smartphone
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone. For **iOS**, use [QGroundControl build from TAJISOFT](https://apps.apple.com/ru/app/qgc-from-tajisoft/id1618653051).
2. Connect your smartphone to the same Wi-Fi network as the machine running the simulator.
3. If you're using a virtual machine, make sure that its network is set to the **bridged** mode with Wi-Fi adapter selected.
4. Run the simulation.
5. Open QGroundControl app. It should connect and begin showing the virtual drone's telemetry automatically.
6. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
7. Use the virtual joystick to fly the drone!
#### Control with USB remote control
1. Connect your USB remote control to the machine running the simulator.
2. Run the simulation.
3. Calibrate the RC using `cr` command in the command line interface.
4. Run the simulation again.
5. Use the USB remote control to fly the drone!
## Firmware
### Arduino IDE (Windows, Linux, macOS)
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.
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.
5. Clone the project using git or [download the source code as a ZIP archive](https://codeload.github.com/okalachev/flix/zip/refs/heads/master).
6. Open the downloaded Arduino sketch `flix/flix.ino` in Arduino IDE.
7. 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.
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)
1. [Install Arduino CLI](https://arduino.github.io/arduino-cli/installation/).
On Linux, use:
```bash
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
```
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. Compile the firmware using `make`. Arduino dependencies will be installed automatically:
```bash
make
```
You can flash the firmware to the board using command:
```bash
make upload
```
You can also compile the firmware, upload it and start serial port monitoring using command:
```bash
make upload monitor
```
See other available Make commands in the [Makefile](../Makefile).
> [!TIP]
> You can test the firmware on a bare ESP32 board without connecting IMU and other peripherals. The Wi-Fi network `flix` should appear and all the basic functionality including CLI and QGroundControl connection should work.
### Setup and flight
Before flight you need to calibrate the accelerometer:
1. Open Serial Monitor in Arduino IDE (or use `make monitor` command in the command line).
2. Type `ca` command there and follow the instructions.
#### Control with smartphone
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.
3. Connect your smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
4. Open QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
5. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
6. Use the virtual joystick to fly the drone!
#### Control with remote control
Before flight using remote control, you need to calibrate it:
1. Open Serial Monitor in Arduino IDE (or use `make monitor` command in the command line).
2. Type `cr` command there and follow the instructions.
3. Use the remote control to fly the drone!
#### Control with USB remote control
If your drone doesn't have RC receiver installed, you can use USB remote control and QGroundControl app to fly it.
1. Install [QGroundControl](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html) app on your computer.
2. Connect your USB remote control to the computer.
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.
7. Use the USB remote control to fly the drone!
#### Adjusting parameters
You can adjust some of the drone's parameters (include PID coefficients) in QGroundControl app. In order to do that, go to the QGroundControl menu ⇒ *Vehicle Setup**Parameters*.
<img src="img/parameters.png" width="400">
#### CLI access
In addition to accessing the drone's command line interface (CLI) using the serial port, you can also access it with QGroundControl using Wi-Fi connection. To do that, go to the QGroundControl menu ⇒ *Vehicle Setup**Analyze Tools**MAVLink Console*.
<img src="img/cli.png" width="400">
> [!NOTE]
> If something goes wrong, go to the [Troubleshooting](troubleshooting.md) article.
### Firmware code structure
See [firmware overview](firmware.md) for more details.

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# Firmware overview # Firmware overview
The firmware is a regular Arduino sketch, and follows the classic Arduino one-threaded design. The initialization code is in the `setup()` function, and the main loop is in the `loop()` function. The sketch includes multiple files, each responsible for a specific part of the system. The firmware is a regular Arduino sketch, and it follows the classic Arduino one-threaded design. The initialization code is in the `setup()` function, and the main loop is in the `loop()` function. The sketch includes several files, each responsible for a specific subsystem.
## Dataflow ## Dataflow
<img src="img/dataflow.svg" width=800 alt="Firmware dataflow diagram"> <img src="img/dataflow.svg" width=600 alt="Firmware dataflow diagram">
The main loop is running at 1000 Hz. All the dataflow is happening through global variables (for simplicity): The main loop is running at 1000 Hz. The dataflow goes through global variables, including:
* `t` *(double)* current step time, *s*. * `t` *(float)* current step time, *s*.
* `dt` *(float)* — time delta between the current and previous steps, *s*. * `dt` *(float)* — time delta between the current and previous steps, *s*.
* `gyro` *(Vector)* — data from the gyroscope, *rad/s*. * `gyro` *(Vector)* — data from the gyroscope, *rad/s*.
* `acc` *(Vector)* — acceleration data from the accelerometer, *m/s<sup>2</sup>*. * `acc` *(Vector)* — acceleration data from the accelerometer, *m/s<sup>2</sup>*.
* `rates` *(Vector)* — filtered angular rates, *rad/s*. * `rates` *(Vector)* — filtered angular rates, *rad/s*.
* `attitude` *(Quaternion)* — estimated attitude (orientation) of drone. * `attitude` *(Quaternion)* — estimated attitude (orientation) of drone.
* `controlRoll`, `controlPitch`, ... *(float[])* pilot's control inputs, range [-1, 1]. * `controlRoll`, `controlPitch`, `controlYaw`, `controlThrottle`, `controlMode` *(float)* pilot control inputs, range [-1, 1].
* `motors` *(float[])* motor outputs, range [0, 1]. * `motors` *(float[4])* motor outputs, range [0, 1].
## Source files ## Source files
Firmware source files are located in `flix` directory. The key files are: Firmware source files are located in `flix` directory.
* [`flix.ino`](../flix/flix.ino) — main entry point, Arduino sketch. Includes global variables definition and the main loop. * [`flix.ino`](../flix/flix.ino) — Arduino sketch main file, entry point.Includes some global variable definitions and the main loop.
* [`imu.ino`](../flix/imu.ino) — reading data from the IMU sensor (gyroscope and accelerometer), IMU calibration. * [`imu.ino`](../flix/imu.ino) — reading data from the IMU sensor (gyroscope and accelerometer), IMU calibration.
* [`rc.ino`](../flix/rc.ino) — reading data from the RC receiver, RC calibration. * [`rc.ino`](../flix/rc.ino) — reading data from the RC receiver, RC calibration.
* [`estimate.ino`](../flix/estimate.ino) — drone's attitude estimation, complementary filter. * [`estimate.ino`](../flix/estimate.ino) — attitude estimation, complementary filter.
* [`control.ino`](../flix/control.ino) — drone's attitude and rates control, three-dimensional two-level cascade PID controller. * [`control.ino`](../flix/control.ino) — control subsystem, three-dimensional two-level cascade PID controller.
* [`motors.ino`](../flix/motors.ino) — PWM motor outputs control. * [`motors.ino`](../flix/motors.ino) — PWM motor output control.
* [`mavlink.ino`](../flix/mavlink.ino) — interaction with QGroundControl or [pyflix](../tools/pyflix) via MAVLink protocol.
* [`cli.ino`](../flix/cli.ino) — serial and MAVLink console.
Utility files include: Utility files:
* [`vector.h`](../flix/vector.h), [`quaternion.h`](../flix/quaternion.h) — project's vector and quaternion libraries implementation. * [`vector.h`](../flix/vector.h), [`quaternion.h`](../flix/quaternion.h) — vector and quaternion libraries.
* [`pid.h`](../flix/pid.h) — generic PID controller implementation. * [`pid.h`](../flix/pid.h) — generic PID controller.
* [`lpf.h`](../flix/lpf.h) — generic low-pass filter implementation. * [`lpf.h`](../flix/lpf.h) — generic low-pass filter.
## Building ### Control subsystem
See build instructions in [build.md](build.md). 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*.
* `torqueTarget` *(Vector)* — target torque, range [-1, 1].
* `thrustTarget` *(float)* — collective 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`.
<img src="img/control.svg" width=300 alt="Control subsystem diagram">
Armed state is stored in `armed` variable, and current mode is stored in `mode` variable.
### Console
To write into the console, `print()` function is used. This function sends data both to the Serial console and to the MAVLink console (which can be accessed wirelessly in QGroundControl). The function supports formatting:
```cpp
print("Test value: %.2f\n", testValue);
```
In order to add a console command, modify the `doCommand()` function in `cli.ino` file.
## Building the firmware
See build instructions in [usage.md](usage.md).

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Flix quadcopter uses RAM to store flight log data. The default log capacity is 10 seconds at 100 Hz. This configuration can be adjusted in the `log.ino` file. Flix quadcopter uses RAM to store flight log data. The default log capacity is 10 seconds at 100 Hz. This configuration can be adjusted in the `log.ino` file.
To perform log analysis, you need to download the log right after the flight without powering off the drone. Then you can use several tools to analyze the log data. To perform log analysis, you need to download the flight log. To to that, ensure you're connected to the drone using Wi-Fi and run the following command:
## Log download
To download the log, connect the ESP32 using USB right after the flight and run the following command:
```bash ```bash
make log make log

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Do the following: Do the following:
* **Check ESP32 core is installed**. Check if the version matches the one used in the [tutorial](build.md#firmware). * **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 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 the chosen board**. The correct board to choose in Arduino IDE for ESP32 Mini is *WEMOS D1 MINI ESP32*.
## The drone doesn't fly ## The drone doesn't fly
@@ -14,7 +15,7 @@ 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 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 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 baudrate is correct**. If you see garbage characters in the Serial Monitor, make sure the baudrate is set to 115200. * **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 board, change `MPU9250` to `ICM20948` everywhere in the `imu.ino` file. * **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 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*).
* **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**. * **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. * **If QGroundControl doesn't connect**, you might need to disable the firewall and/or VPN on your computer.
@@ -31,7 +32,8 @@ Do the following:
* `mfl` — should rotate front left motor (clockwise). * `mfl` — should rotate front left motor (clockwise).
* `mrl` — should rotate rear left motor (counter-clockwise). * `mrl` — should rotate rear left motor (counter-clockwise).
* `mrr` — should rotate rear right motor (clockwise). * `mrr` — should rotate rear right motor (clockwise).
* **Calibrate the RC** if you use it. Type `cr` command in Serial Monitor and follow the instructions. * **Check the propeller directions are correct**. Make sure your propeller types (A or B) are installed as on the picture:
* **Check the RC data** if you use it. Use `rc` command, `Control` should show correct values between -1 and 1, and between 0 and 1 for the throttle. <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. * **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.
* **Check the gyroscope only attitude estimation**. Comment out `applyAcc();` line in `estimate.ino` and check if the attitude estimation in QGroundControl. It should be stable, but only drift very slowly.

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# Usage: build, setup and flight
To fly Flix quadcopter, you need to build the firmware, upload it to the ESP32 board, and set up the drone for flight.
To get the firmware sources, clone the repository using git:
```bash
git clone https://github.com/okalachev/flix.git && cd flix
```
Beginners can [download the source code as a ZIP archive](https://github.com/okalachev/flix/archive/refs/heads/master.zip).
## Building the firmware
You can build and upload the firmware using either **Arduino IDE** (easier for beginners) or **command line**.
### Arduino IDE (Windows, Linux, macOS)
<img src="img/arduino-ide.png" width="400" alt="Flix firmware open in Arduino IDE">
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.
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.
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.
### Command line (Windows, Linux, macOS)
1. [Install Arduino CLI](https://arduino.github.io/arduino-cli/installation/).
On Linux, install it like this:
```bash
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
```
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. Compile the firmware using `make`. Arduino dependencies will be installed automatically:
```bash
make
```
You can flash the firmware to the board using command:
```bash
make upload
```
You can also compile the firmware, upload it and start serial port monitoring using command:
```bash
make upload monitor
```
See other available Make commands in [Makefile](../Makefile).
> [!TIP]
> You can test the firmware on a bare ESP32 board without connecting IMU and other peripherals. The Wi-Fi network `flix` should appear and all the basic functionality including console and QGroundControl connection should work.
## Before first flight
### Choose the IMU model
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
```
### Connect using QGroundControl
QGroundControl is a ground control station software that can be used to monitor and control the drone.
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
### Access console
The console is a command line interface (CLI) that allows to interact with the drone, change parameters, and perform various actions. There are two ways of accessing the console: using **serial port** or using **QGroundControl (wirelessly)**.
To access the console using serial port:
1. Connect the ESP32 board to the computer using USB cable.
2. Open Serial Monitor in Arduino IDE (or use `make monitor` in the command line).
3. In Arduino IDE, make sure the baudrate is set to 115200.
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*.
<img src="img/cli.png" width="400">
> [!TIP]
> Use `help` command to see the list of available commands.
### Access parameters
The drone is configured using parameters. To access and modify them, go to the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Parameters*:
<img src="img/parameters.png" width="400">
### 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 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:
<img src="img/imu-axes.png" width="200">
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|
### Calibrate accelerometer
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
1. 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.
* 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:
<img src="img/qgc-attitude.png" height="200">
3. Perform motor tests in the console. 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).
> [!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).
### Control with smartphone
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.
3. Connect your smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
4. Open QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
5. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
6. Use the virtual joystick to fly the drone!
> [!TIP]
> Decrease `CTL_TILT_MAX` parameter when flying using the smartphone to make the controls less sensitive.
### Control with remote control
Before using remote SBUS-connected remote control, you need to 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!
### Control with USB remote control
If your drone doesn't have RC receiver installed, you can use USB remote control and QGroundControl app to fly it.
1. Install [QGroundControl](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html) app on your computer.
2. Connect your USB remote control to the computer.
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.
7. Use the USB remote control to fly the drone!
## Flight
For both virtual sticks and a physical joystick, the default control scheme is left stick for throttle and yaw and right stick for pitch and roll:
<img src="img/controls.svg" width="300">
### Arming and disarming
To start the motors, you should **arm** the drone. To do that, move the left stick to the bottom right corner:
<img src="img/arming.svg" width="150">
After that, the motors **will start spinning** at low speed, indicating that the drone is armed and ready to fly.
When finished flying, **disarm** the drone, moving the left stick to the bottom left corner:
<img src="img/disarming.svg" width="150">
> [!NOTE]
> If something goes wrong, go to the [Troubleshooting](troubleshooting.md) article.
### Flight modes
Flight mode is changed using mode switch on the remote control or using the command line.
#### 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.
> [!IMPORTANT]
> The drone doesn't stabilize its position, so slight drift is possible. The pilot should compensate it manually.
#### ACRO
In this mode, the pilot controls the angular rates. This control method is difficult to fly and mostly used in FPV racing.
#### RAW
*RAW* mode disables all the stabilization, and the pilot inputs are mixed directly to the motors. The IMU sensor is not involved. This mode is intended for testing and demonstration purposes only, and basically the drone **cannot fly in this mode**.
#### 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.
If the pilot moves the control sticks, the drone will switch back to *STAB* mode.
<img src="img/parameters.png" width="400">
## Flight log
After the flight, you can download the flight log for analysis wirelessly. Use the following for that:
```bash
make log
```
See more details about log analysis in the [log analysis](log.md) article.

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@@ -4,6 +4,80 @@ This page contains user-built drones based on the Flix project. Publish your pro
--- ---
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>
**Flight video:**
<a href="https://drive.google.com/file/d/1nQtFjEcGGLx-l4xkL5ko9ZpOTVU-WDjL/view?usp=sharing"><img height=200 src="img/user/goldarte/video.jpg"></a>
---
## 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.
<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">
STL files and other materials: see [here](https://drive.google.com/drive/folders/1wTUzj087LjKQQl3Lz5CjHCuobxoykhyp?usp=share_link).
### Selected works
Author: [KiraFlux](https://t.me/@kiraflux_0XC0000005).<br>
Description: **custom ESPNOW remote control** is implemented, firmware modified 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>
Drone design: https://github.com/KiraFlux/Klyax.<br>
<img src="img/user/school548/kiraflux1.jpg" height=150> <img src="img/user/school548/kiraflux2.jpg" height=150>
**ESPNOW remote control demonstration**:
<img height=200 src="img/user/school548/kiraflux-video.jpg"><a href="https://drive.google.com/file/d/1soHDAeHQWnm97Y4dg4nWevJuMiTdJJXW/view?usp=sharing"></a>
Author: [tolyan4krut](https://t.me/tolyan4krut).<br>
Description: the first drone based on ESP32-S3-CAM board **with a camera**, implementing Wi-Fi video streaming. Runs HTTP server and HTTP video stream.<br>
Modified Flix firmware: https://github.com/CatRey/Flix-Camera-Streaming.<br>
[Telegram post](https://t.me/opensourcequadcopter/117).
<img src="img/user/school548/tolyan4krut.jpg" height=150>
**Video streaming and flight demonstration**:
<a href="https://drive.google.com/file/d/1KuOBsujLsk7q8FoqKD8u7uoq4ptS5onp/view?usp=sharing"><img height=200 src="img/user/school548/tolyan4krut-video.jpg"></a>
Author: [Vlad Tolshinov](https://t.me/Vlad_Tolshinov).<br>
Description: custom frame with enlarged arm length, which provides very high flight stability, 65 mm props.
<img src="img/user/school548/vlad_tolshinov1.jpg" height=150> <img src="img/user/school548/vlad_tolshinov2.jpg" height=150>
**Flight video**:
<a href="https://drive.google.com/file/d/1zu00DZxhC7DJ9Z2mYjtxdNQqOOLAyYbp/view?usp=sharing"><img height=200 src="img/user/school548/vlad_tolshinov-video.jpg"></a>
---
## RoboCamp
Author: RoboCamp participants.<br>
Description: 3D-printed and wooden frames, ESP32 Mini, DC-DC buck-boost converters. BetaFPV LiteRadio 3 to control the drones via Wi-Fi connection.<br>
Features: altitude hold, obstacle avoidance, autonomous flight elements.<br>
Some of the designed model files: see [here](https://drive.google.com/drive/folders/18YHWGquKeIevzrMH4-OUT-zKXMETTEUu?usp=share_link).
RoboCamp took place in July 2025, Saint Petersburg, where 9 participants designed and built their own drones using the Flix project, and then modified the firmware to complete specific flight tasks.
See the detailed video about the event:
<a href="https://youtu.be/Wd3yaorjTx0"><img width=500 src="https://img.youtube.com/vi/Wd3yaorjTx0/sddefault.jpg"></a>
Built drones:
<img src="img/user/robocamp/1.jpg" width=500>
---
Author: chkroko.<br> Author: chkroko.<br>
Description: the first Flix drone built with **brushless motors** (DShot interface).<br> Description: the first Flix drone built with **brushless motors** (DShot interface).<br>
Features: SpeedyBee BLS 35A Mini V2 ESC, ESP32-S3 board, EMAX ECO 2 2207 1700kv motors, ICM20948V2 IMU, INA226 power monitor and Bluetooth gamepad for control.<br> Features: SpeedyBee BLS 35A Mini V2 ESC, ESP32-S3 board, EMAX ECO 2 2207 1700kv motors, ICM20948V2 IMU, INA226 power monitor and Bluetooth gamepad for control.<br>

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@@ -14,7 +14,7 @@ Flix version 0 (obsolete):
|Motor|8520 3.7V brushed motor (**shaft 0.8mm!**)|<img src="img/motor.jpeg" width=100>|4| |Motor|8520 3.7V brushed motor (**shaft 0.8mm!**)|<img src="img/motor.jpeg" width=100>|4|
|Propeller|Hubsan 55 mm|<img src="img/prop.jpg" width=100>|4| |Propeller|Hubsan 55 mm|<img src="img/prop.jpg" width=100>|4|
|Motor ESC|2.7A 1S Dual Way Micro Brush ESC|<img src="img/esc.jpg" width=100>|4| |Motor ESC|2.7A 1S Dual Way Micro Brush ESC|<img src="img/esc.jpg" width=100>|4|
|RC transmitter|KINGKONG TINY X8|<img src="img/tx.jpg" width=100>|1| |RC transmitter|KINGKONG TINY X8|<img src="img/kingkong.jpg" width=100>|1|
|RC receiver|DF500 (SBUS)|<img src="img/rx.jpg" width=100>|1| |RC receiver|DF500 (SBUS)|<img src="img/rx.jpg" width=100>|1|
|~~SBUS inverter~~*||<img src="img/inv.jpg" width=100>|~~1~~| |~~SBUS inverter~~*||<img src="img/inv.jpg" width=100>|~~1~~|
|Battery|3.7 Li-Po 850 MaH 60C||| |Battery|3.7 Li-Po 850 MaH 60C|||

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@@ -8,10 +8,12 @@
#include "util.h" #include "util.h"
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT; extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern float loopRate, dt; extern const int RAW, ACRO, STAB, AUTO;
extern double t; extern float t, dt, loopRate;
extern uint16_t channels[16]; extern uint16_t channels[16];
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlArmed, controlMode; extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
extern int mode;
extern bool armed;
const char* motd = const char* motd =
"\nWelcome to\n" "\nWelcome to\n"
@@ -31,11 +33,16 @@ const char* motd =
"ps - show pitch/roll/yaw\n" "ps - show pitch/roll/yaw\n"
"psq - show attitude quaternion\n" "psq - show attitude quaternion\n"
"imu - show IMU data\n" "imu - show IMU data\n"
"arm - arm the drone\n"
"disarm - disarm the drone\n"
"raw/stab/acro/auto - set mode\n"
"rc - show RC data\n" "rc - show RC data\n"
"wifi - show Wi-Fi info\n"
"mot - show motor output\n" "mot - show motor output\n"
"log - dump in-RAM log\n" "log [dump] - print log header [and data]\n"
"cr - calibrate RC\n" "cr - calibrate RC\n"
"ca - calibrate accel\n" "ca - calibrate accel\n"
"cl - calibrate level\n"
"mfr, mfl, mrr, mrl - test motor (remove props)\n" "mfr, mfl, mrr, mrl - test motor (remove props)\n"
"sys - show system info\n" "sys - show system info\n"
"reset - reset drone's state\n" "reset - reset drone's state\n"
@@ -54,7 +61,7 @@ void print(const char* format, ...) {
} }
void pause(float duration) { void pause(float duration) {
double start = t; float start = t;
while (t - start < duration) { while (t - start < duration) {
step(); step();
handleInput(); handleInput();
@@ -69,9 +76,10 @@ void doCommand(String str, bool echo = false) {
// parse command // parse command
String command, arg0, arg1; String command, arg0, arg1;
splitString(str, command, arg0, arg1); splitString(str, command, arg0, arg1);
if (command.isEmpty()) return;
// echo command // echo command
if (echo && !command.isEmpty()) { if (echo) {
print("> %s\n", str.c_str()); print("> %s\n", str.c_str());
} }
@@ -101,31 +109,48 @@ void doCommand(String str, bool echo = false) {
Vector a = attitude.toEuler(); Vector a = attitude.toEuler();
print("roll: %f pitch: %f yaw: %f\n", degrees(a.x), degrees(a.y), degrees(a.z)); print("roll: %f pitch: %f yaw: %f\n", degrees(a.x), degrees(a.y), degrees(a.z));
} else if (command == "psq") { } else if (command == "psq") {
print("qx: %f qy: %f qz: %f qw: %f\n", attitude.x, attitude.y, attitude.z, attitude.w); print("qw: %f qx: %f qy: %f qz: %f\n", attitude.w, attitude.x, attitude.y, attitude.z);
} else if (command == "imu") { } else if (command == "imu") {
printIMUInfo(); printIMUInfo();
print("gyro: %f %f %f\n", rates.x, rates.y, rates.z);
print("acc: %f %f %f\n", acc.x, acc.y, acc.z);
printIMUCalibration(); printIMUCalibration();
print("rate: %.0f\n", loopRate);
print("landed: %d\n", landed); print("landed: %d\n", landed);
} else if (command == "arm") {
armed = true;
} else if (command == "disarm") {
armed = false;
} else if (command == "raw") {
mode = RAW;
} else if (command == "stab") {
mode = STAB;
} else if (command == "acro") {
mode = ACRO;
} else if (command == "auto") {
mode = AUTO;
} else if (command == "rc") { } else if (command == "rc") {
print("channels: "); print("channels: ");
for (int i = 0; i < 16; i++) { for (int i = 0; i < 16; i++) {
print("%u ", channels[i]); print("%u ", channels[i]);
} }
print("\nroll: %g pitch: %g yaw: %g throttle: %g armed: %g mode: %g\n", print("\nroll: %g pitch: %g yaw: %g throttle: %g mode: %g\n",
controlRoll, controlPitch, controlYaw, controlThrottle, controlArmed, controlMode); controlRoll, controlPitch, controlYaw, controlThrottle, controlMode);
print("mode: %s\n", getModeName()); print("mode: %s\n", getModeName());
print("armed: %d\n", armed);
} else if (command == "wifi") {
#if WIFI_ENABLED
printWiFiInfo();
#endif
} else if (command == "mot") { } else if (command == "mot") {
print("front-right %g front-left %g rear-right %g rear-left %g\n", 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]); motors[MOTOR_FRONT_RIGHT], motors[MOTOR_FRONT_LEFT], motors[MOTOR_REAR_RIGHT], motors[MOTOR_REAR_LEFT]);
} else if (command == "log") { } else if (command == "log") {
dumpLog(); printLogHeader();
if (arg0 == "dump") printLogData();
} else if (command == "cr") { } else if (command == "cr") {
calibrateRC(); calibrateRC();
} else if (command == "ca") { } else if (command == "ca") {
calibrateAccel(); calibrateAccel();
} else if (command == "cl") {
calibrateLevel();
} else if (command == "mfr") { } else if (command == "mfr") {
testMotor(MOTOR_FRONT_RIGHT); testMotor(MOTOR_FRONT_RIGHT);
} else if (command == "mfl") { } else if (command == "mfl") {
@@ -157,8 +182,6 @@ void doCommand(String str, bool echo = false) {
attitude = Quaternion(); attitude = Quaternion();
} else if (command == "reboot") { } else if (command == "reboot") {
ESP.restart(); ESP.restart();
} else if (command == "") {
// do nothing
} else { } else {
print("Invalid command: %s\n", command.c_str()); print("Invalid command: %s\n", command.c_str());
} }

View File

@@ -34,8 +34,8 @@
#define TILT_MAX radians(30) #define TILT_MAX radians(30)
#define RATES_D_LPF_ALPHA 0.2 // cutoff frequency ~ 40 Hz #define RATES_D_LPF_ALPHA 0.2 // cutoff frequency ~ 40 Hz
enum { MANUAL, ACRO, STAB, USER } mode = STAB; const int RAW = 0, ACRO = 1, STAB = 2, AUTO = 3; // flight modes
enum { YAW, YAW_RATE } yawMode = YAW; int mode = STAB;
bool armed = false; bool armed = false;
PID rollRatePID(ROLLRATE_P, ROLLRATE_I, ROLLRATE_D, ROLLRATE_I_LIM, RATES_D_LPF_ALPHA); PID rollRatePID(ROLLRATE_P, ROLLRATE_I, ROLLRATE_D, ROLLRATE_I_LIM, RATES_D_LPF_ALPHA);
@@ -49,75 +49,58 @@ float tiltMax = TILT_MAX;
Quaternion attitudeTarget; Quaternion attitudeTarget;
Vector ratesTarget; Vector ratesTarget;
Vector ratesExtra; // feedforward rates
Vector torqueTarget; Vector torqueTarget;
float thrustTarget; float thrustTarget;
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT; extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlArmed, controlMode; extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
void control() { void control() {
interpretRC(); interpretControls();
failsafe(); failsafe();
if (mode == STAB) { controlAttitude();
controlAttitude(); controlRates();
controlRate(); controlTorque();
controlTorque();
} else if (mode == ACRO) {
controlRate();
controlTorque();
} else if (mode == MANUAL) {
controlTorque();
}
} }
void interpretRC() { void interpretControls() {
armed = controlThrottle >= 0.05 && controlArmed >= 0.5; if (controlMode < 0.25) mode = STAB;
if (controlMode < 0.75) mode = STAB;
if (controlMode > 0.75) mode = STAB;
// NOTE: put ACRO or MANUAL modes there if you want to use them if (mode == AUTO) return; // pilot is not effective in AUTO mode
if (controlMode < 0.25) {
mode = STAB; if (controlThrottle < 0.05 && controlYaw > 0.95) armed = true; // arm gesture
} else if (controlMode < 0.75) { if (controlThrottle < 0.05 && controlYaw < -0.95) armed = false; // disarm gesture
mode = STAB;
} else { if (abs(controlYaw) < 0.1) controlYaw = 0; // yaw dead zone
mode = STAB;
}
thrustTarget = controlThrottle; thrustTarget = controlThrottle;
if (mode == ACRO) { if (mode == STAB) {
yawMode = YAW_RATE; float yawTarget = attitudeTarget.getYaw();
ratesTarget.x = controlRoll * maxRate.x; if (!armed || invalid(yawTarget) || controlYaw != 0) yawTarget = attitude.getYaw(); // reset yaw target
ratesTarget.y = controlPitch* maxRate.y; attitudeTarget = Quaternion::fromEuler(Vector(controlRoll * tiltMax, controlPitch * tiltMax, yawTarget));
ratesTarget.z = -controlYaw * maxRate.z; // positive yaw stick means clockwise rotation in FLU ratesExtra = Vector(0, 0, -controlYaw * maxRate.z); // positive yaw stick means clockwise rotation in FLU
} else if (mode == STAB) {
yawMode = controlYaw == 0 ? YAW : YAW_RATE;
attitudeTarget = Quaternion::fromEuler(Vector(
controlRoll * tiltMax,
controlPitch * tiltMax,
attitudeTarget.getYaw()));
ratesTarget.z = -controlYaw * maxRate.z; // positive yaw stick means clockwise rotation in FLU
} else if (mode == MANUAL) {
// passthrough mode
yawMode = YAW_RATE;
torqueTarget = Vector(controlRoll, controlPitch, -controlYaw) * 0.01;
} }
if (yawMode == YAW_RATE || !motorsActive()) { if (mode == ACRO) {
// update yaw target as we don't have control over the yaw attitudeTarget.invalidate(); // skip attitude control
attitudeTarget.setYaw(attitude.getYaw()); ratesTarget.x = controlRoll * maxRate.x;
ratesTarget.y = controlPitch * maxRate.y;
ratesTarget.z = -controlYaw * maxRate.z; // positive yaw stick means clockwise rotation in FLU
}
if (mode == RAW) { // direct torque control
attitudeTarget.invalidate(); // skip attitude control
ratesTarget.invalidate(); // skip rate control
torqueTarget = Vector(controlRoll, controlPitch, -controlYaw) * 0.1;
} }
} }
void controlAttitude() { void controlAttitude() {
if (!armed) { if (!armed || attitudeTarget.invalid() || thrustTarget < 0.1) return; // skip attitude control
rollPID.reset();
pitchPID.reset();
yawPID.reset();
return;
}
const Vector up(0, 0, 1); const Vector up(0, 0, 1);
Vector upActual = Quaternion::rotateVector(up, attitude); Vector upActual = Quaternion::rotateVector(up, attitude);
@@ -125,34 +108,38 @@ void controlAttitude() {
Vector error = Vector::rotationVectorBetween(upTarget, upActual); Vector error = Vector::rotationVectorBetween(upTarget, upActual);
ratesTarget.x = rollPID.update(error.x, dt); ratesTarget.x = rollPID.update(error.x) + ratesExtra.x;
ratesTarget.y = pitchPID.update(error.y, dt); ratesTarget.y = pitchPID.update(error.y) + ratesExtra.y;
if (yawMode == YAW) { float yawError = wrapAngle(attitudeTarget.getYaw() - attitude.getYaw());
float yawError = wrapAngle(attitudeTarget.getYaw() - attitude.getYaw()); ratesTarget.z = yawPID.update(yawError) + ratesExtra.z;
ratesTarget.z = yawPID.update(yawError, dt);
}
} }
void controlRate() {
if (!armed) { void controlRates() {
rollRatePID.reset(); if (!armed || ratesTarget.invalid() || thrustTarget < 0.1) return; // skip rates control
pitchRatePID.reset();
yawRatePID.reset();
return;
}
Vector error = ratesTarget - rates; Vector error = ratesTarget - rates;
// Calculate desired torque, where 0 - no torque, 1 - maximum possible torque // Calculate desired torque, where 0 - no torque, 1 - maximum possible torque
torqueTarget.x = rollRatePID.update(error.x, dt); torqueTarget.x = rollRatePID.update(error.x);
torqueTarget.y = pitchRatePID.update(error.y, dt); torqueTarget.y = pitchRatePID.update(error.y);
torqueTarget.z = yawRatePID.update(error.z, dt); torqueTarget.z = yawRatePID.update(error.z);
} }
void controlTorque() { void controlTorque() {
if (!torqueTarget.valid()) return; // skip torque control
if (!armed) { if (!armed) {
memset(motors, 0, sizeof(motors)); memset(motors, 0, sizeof(motors)); // stop motors if disarmed
return;
}
if (thrustTarget < 0.1) {
motors[0] = 0.1; // idle thrust
motors[1] = 0.1;
motors[2] = 0.1;
motors[3] = 0.1;
return; return;
} }
@@ -169,10 +156,10 @@ void controlTorque() {
const char* getModeName() { const char* getModeName() {
switch (mode) { switch (mode) {
case MANUAL: return "MANUAL"; case RAW: return "RAW";
case ACRO: return "ACRO"; case ACRO: return "ACRO";
case STAB: return "STAB"; case STAB: return "STAB";
case USER: return "USER"; case AUTO: return "AUTO";
default: return "UNKNOWN"; default: return "UNKNOWN";
} }
} }

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@@ -8,10 +8,8 @@
#include "lpf.h" #include "lpf.h"
#include "util.h" #include "util.h"
#define WEIGHT_ACC 0.003 float accWeight = 0.003;
#define RATES_LFP_ALPHA 0.2 // cutoff frequency ~ 40 Hz LowPassFilter<Vector> ratesFilter(0.2); // cutoff frequency ~ 40 Hz
LowPassFilter<Vector> ratesFilter(RATES_LFP_ALPHA);
void estimate() { void estimate() {
applyGyro(); applyGyro();
@@ -35,7 +33,7 @@ void applyAcc() {
// calculate accelerometer correction // calculate accelerometer correction
Vector up = Quaternion::rotateVector(Vector(0, 0, 1), attitude); Vector up = Quaternion::rotateVector(Vector(0, 0, 1), attitude);
Vector correction = Vector::rotationVectorBetween(acc, up) * WEIGHT_ACC; Vector correction = Vector::rotationVectorBetween(acc, up) * accWeight;
// apply correction // apply correction
attitude = Quaternion::rotate(attitude, Quaternion::fromRotationVector(correction)); attitude = Quaternion::rotate(attitude, Quaternion::fromRotationVector(correction));

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@@ -1,41 +0,0 @@
// Copyright (c) 2024 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Fail-safe functions
#define RC_LOSS_TIMEOUT 0.2
#define DESCEND_TIME 3.0 // time to descend from full throttle to zero
extern double controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw;
void failsafe() {
armingFailsafe();
rcLossFailsafe();
}
// Prevent arming without zero throttle input
void armingFailsafe() {
static double zeroThrottleTime;
static double armingTime;
if (!armed) armingTime = t; // stores the last time when the drone was disarmed, therefore contains arming time
if (controlTime > 0 && controlThrottle < 0.05) zeroThrottleTime = controlTime;
if (armingTime - zeroThrottleTime > 0.1) armed = false; // prevent arming if there was no zero throttle for 0.1 sec
}
// RC loss failsafe
void rcLossFailsafe() {
if (t - controlTime > RC_LOSS_TIMEOUT) {
descend();
}
}
// Smooth descend on RC lost
void descend() {
mode = STAB;
controlRoll = 0;
controlPitch = 0;
controlYaw = 0;
controlThrottle -= dt / DESCEND_TIME;
if (controlThrottle < 0) controlThrottle = 0;
}

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@@ -7,12 +7,12 @@
#include "quaternion.h" #include "quaternion.h"
#include "util.h" #include "util.h"
#define SERIAL_BAUDRATE 115200
#define WIFI_ENABLED 1 #define WIFI_ENABLED 1
double t = NAN; // current step time, s float t = NAN; // current step time, s
float dt; // time delta from previous step, s float dt; // time delta from previous step, s
float controlRoll, controlPitch, controlYaw, controlThrottle, controlArmed, controlMode; // pilot's inputs, range [-1, 1] float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
float controlMode = NAN;
Vector gyro; // gyroscope data Vector gyro; // gyroscope data
Vector acc; // accelerometer data, m/s/s Vector acc; // accelerometer data, m/s/s
Vector rates; // filtered angular rates, rad/s Vector rates; // filtered angular rates, rad/s
@@ -21,7 +21,7 @@ bool landed; // are we landed and stationary
float motors[4]; // normalized motors thrust in range [0..1] float motors[4]; // normalized motors thrust in range [0..1]
void setup() { void setup() {
Serial.begin(SERIAL_BAUDRATE); Serial.begin(115200);
print("Initializing flix\n"); print("Initializing flix\n");
disableBrownOut(); disableBrownOut();
setupParameters(); setupParameters();

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@@ -4,11 +4,13 @@
// Work with the IMU sensor // Work with the IMU sensor
#include <SPI.h> #include <SPI.h>
#include <MPU9250.h> #include <FlixPeriph.h>
#include "vector.h"
#include "lpf.h" #include "lpf.h"
#include "util.h" #include "util.h"
MPU9250 IMU(SPI); MPU9250 imu(SPI);
Vector imuRotation(0, 0, -PI / 2); // imu orientation as Euler angles
Vector accBias; Vector accBias;
Vector accScale(1, 1, 1); Vector accScale(1, 1, 1);
@@ -16,50 +18,43 @@ Vector gyroBias;
void setupIMU() { void setupIMU() {
print("Setup IMU\n"); print("Setup IMU\n");
IMU.begin(); imu.begin();
configureIMU(); configureIMU();
} }
void configureIMU() { void configureIMU() {
IMU.setAccelRange(IMU.ACCEL_RANGE_4G); imu.setAccelRange(imu.ACCEL_RANGE_4G);
IMU.setGyroRange(IMU.GYRO_RANGE_2000DPS); imu.setGyroRange(imu.GYRO_RANGE_2000DPS);
IMU.setDLPF(IMU.DLPF_MAX); imu.setDLPF(imu.DLPF_MAX);
IMU.setRate(IMU.RATE_1KHZ_APPROX); imu.setRate(imu.RATE_1KHZ_APPROX);
IMU.setupInterrupt(); imu.setupInterrupt();
} }
void readIMU() { void readIMU() {
IMU.waitForData(); imu.waitForData();
IMU.getGyro(gyro.x, gyro.y, gyro.z); imu.getGyro(gyro.x, gyro.y, gyro.z);
IMU.getAccel(acc.x, acc.y, acc.z); imu.getAccel(acc.x, acc.y, acc.z);
calibrateGyroOnce(); calibrateGyroOnce();
// apply scale and bias // apply scale and bias
acc = (acc - accBias) / accScale; acc = (acc - accBias) / accScale;
gyro = gyro - gyroBias; gyro = gyro - gyroBias;
// rotate // rotate to body frame
rotateIMU(acc); Quaternion rotation = Quaternion::fromEuler(imuRotation);
rotateIMU(gyro); acc = Quaternion::rotateVector(acc, rotation.inversed());
} gyro = Quaternion::rotateVector(gyro, rotation.inversed());
void rotateIMU(Vector& data) {
// Rotate from LFD to FLU
// NOTE: In case of using other IMU orientation, change this line:
data = Vector(data.y, data.x, -data.z);
// Axes orientation for various boards: https://github.com/okalachev/flixperiph#imu-axes-orientation
} }
void calibrateGyroOnce() { void calibrateGyroOnce() {
static float landedTime = 0; static Delay landedDelay(2);
landedTime = landed ? landedTime + dt : 0; if (!landedDelay.update(landed)) return; // calibrate only if definitely stationary
if (landedTime < 2) return; // calibrate only if definitely stationary
static LowPassFilter<Vector> gyroCalibrationFilter(0.001); static LowPassFilter<Vector> gyroBiasFilter(0.001);
gyroBias = gyroCalibrationFilter.update(gyro); gyroBias = gyroBiasFilter.update(gyro);
} }
void calibrateAccel() { void calibrateAccel() {
print("Calibrating accelerometer\n"); print("Calibrating accelerometer\n");
IMU.setAccelRange(IMU.ACCEL_RANGE_2G); // the most sensitive mode imu.setAccelRange(imu.ACCEL_RANGE_2G); // the most sensitive mode
print("1/6 Place level [8 sec]\n"); print("1/6 Place level [8 sec]\n");
pause(8); pause(8);
@@ -93,9 +88,9 @@ void calibrateAccelOnce() {
// Compute the average of the accelerometer readings // Compute the average of the accelerometer readings
acc = Vector(0, 0, 0); acc = Vector(0, 0, 0);
for (int i = 0; i < samples; i++) { for (int i = 0; i < samples; i++) {
IMU.waitForData(); imu.waitForData();
Vector sample; Vector sample;
IMU.getAccel(sample.x, sample.y, sample.z); imu.getAccel(sample.x, sample.y, sample.z);
acc = acc + sample; acc = acc + sample;
} }
acc = acc / samples; acc = acc / samples;
@@ -112,6 +107,14 @@ void calibrateAccelOnce() {
accBias = (accMax + accMin) / 2; 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() { void printIMUCalibration() {
print("gyro bias: %f %f %f\n", gyroBias.x, gyroBias.y, gyroBias.z); 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); print("accel bias: %f %f %f\n", accBias.x, accBias.y, accBias.z);
@@ -119,7 +122,16 @@ void printIMUCalibration() {
} }
void printIMUInfo() { void printIMUInfo() {
IMU.status() ? print("status: ERROR %d\n", IMU.status()) : print("status: OK\n"); imu.status() ? print("status: ERROR %d\n", imu.status()) : print("status: OK\n");
print("model: %s\n", IMU.getModel()); print("model: %s\n", imu.getModel());
print("who am I: 0x%02X\n", IMU.whoAmI()); 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("acc: %f %f %f\n", acc.x, acc.y, acc.z);
imu.waitForData();
Vector rawGyro, rawAcc;
imu.getGyro(rawGyro.x, rawGyro.y, rawGyro.z);
imu.getAccel(rawAcc.x, rawAcc.y, rawAcc.z);
print("raw gyro: %f %f %f\n", rawGyro.x, rawGyro.y, rawGyro.z);
print("raw acc: %f %f %f\n", rawAcc.x, rawAcc.y, rawAcc.z);
} }

View File

@@ -4,13 +4,12 @@
// In-RAM logging // In-RAM logging
#include "vector.h" #include "vector.h"
#include "util.h"
#define LOG_RATE 100 #define LOG_RATE 100
#define LOG_DURATION 10 #define LOG_DURATION 10
#define LOG_PERIOD 1.0 / LOG_RATE
#define LOG_SIZE LOG_DURATION * LOG_RATE #define LOG_SIZE LOG_DURATION * LOG_RATE
float tFloat;
Vector attitudeEuler; Vector attitudeEuler;
Vector attitudeTargetEuler; Vector attitudeTargetEuler;
@@ -20,7 +19,7 @@ struct LogEntry {
}; };
LogEntry logEntries[] = { LogEntry logEntries[] = {
{"t", &tFloat}, {"t", &t},
{"rates.x", &rates.x}, {"rates.x", &rates.x},
{"rates.y", &rates.y}, {"rates.y", &rates.y},
{"rates.z", &rates.z}, {"rates.z", &rates.z},
@@ -40,7 +39,6 @@ const int logColumns = sizeof(logEntries) / sizeof(logEntries[0]);
float logBuffer[LOG_SIZE][logColumns]; float logBuffer[LOG_SIZE][logColumns];
void prepareLogData() { void prepareLogData() {
tFloat = t;
attitudeEuler = attitude.toEuler(); attitudeEuler = attitude.toEuler();
attitudeTargetEuler = attitudeTarget.toEuler(); attitudeTargetEuler = attitudeTarget.toEuler();
} }
@@ -48,9 +46,8 @@ void prepareLogData() {
void logData() { void logData() {
if (!armed) return; if (!armed) return;
static int logPointer = 0; static int logPointer = 0;
static double logTime = 0; static Rate period(LOG_RATE);
if (t - logTime < LOG_PERIOD) return; if (!period) return;
logTime = t;
prepareLogData(); prepareLogData();
@@ -64,12 +61,13 @@ void logData() {
} }
} }
void dumpLog() { void printLogHeader() {
// Print header
for (int i = 0; i < logColumns; i++) { for (int i = 0; i < logColumns; i++) {
print("%s%s", logEntries[i].name, i < logColumns - 1 ? "," : "\n"); print("%s%s", logEntries[i].name, i < logColumns - 1 ? "," : "\n");
} }
// Print data }
void printLogData() {
for (int i = 0; i < LOG_SIZE; i++) { for (int i = 0; i < LOG_SIZE; i++) {
if (logBuffer[i][0] == 0) continue; // skip empty records if (logBuffer[i][0] == 0) continue; // skip empty records
for (int j = 0; j < logColumns; j++) { for (int j = 0; j < logColumns; j++) {

View File

@@ -6,17 +6,17 @@
#if WIFI_ENABLED #if WIFI_ENABLED
#include <MAVLink.h> #include <MAVLink.h>
#include "util.h"
#define SYSTEM_ID 1 #define SYSTEM_ID 1
#define PERIOD_SLOW 1.0 #define MAVLINK_RATE_SLOW 1
#define PERIOD_FAST 0.1 #define MAVLINK_RATE_FAST 10
#define MAVLINK_CONTROL_YAW_DEAD_ZONE 0.1f
float mavlinkControlScale = 0.7; bool mavlinkConnected = false;
String mavlinkPrintBuffer; String mavlinkPrintBuffer;
extern double controlTime; extern float controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlArmed, controlMode; extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
void processMavlink() { void processMavlink() {
sendMavlink(); sendMavlink();
@@ -26,28 +26,27 @@ void processMavlink() {
void sendMavlink() { void sendMavlink() {
sendMavlinkPrint(); sendMavlinkPrint();
static double lastSlow = 0;
static double lastFast = 0;
mavlink_message_t msg; mavlink_message_t msg;
uint32_t time = t * 1000; uint32_t time = t * 1000;
if (t - lastSlow >= PERIOD_SLOW) { static Rate slow(MAVLINK_RATE_SLOW), fast(MAVLINK_RATE_FAST);
lastSlow = t;
if (slow) {
mavlink_msg_heartbeat_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, MAV_TYPE_QUADROTOR, MAV_AUTOPILOT_GENERIC, mavlink_msg_heartbeat_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, MAV_TYPE_QUADROTOR, MAV_AUTOPILOT_GENERIC,
MAV_MODE_FLAG_MANUAL_INPUT_ENABLED | (armed * MAV_MODE_FLAG_SAFETY_ARMED) | ((mode == STAB) * MAV_MODE_FLAG_STABILIZE_ENABLED), (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); mode, MAV_STATE_STANDBY);
sendMessage(&msg); sendMessage(&msg);
if (!mavlinkConnected) return; // send only heartbeat until connected
mavlink_msg_extended_sys_state_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, mavlink_msg_extended_sys_state_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
MAV_VTOL_STATE_UNDEFINED, landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR); MAV_VTOL_STATE_UNDEFINED, landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR);
sendMessage(&msg); sendMessage(&msg);
} }
if (t - lastFast >= PERIOD_FAST) { if (fast && mavlinkConnected) {
lastFast = t;
const float zeroQuat[] = {0, 0, 0, 0}; const float zeroQuat[] = {0, 0, 0, 0};
mavlink_msg_attitude_quaternion_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, 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 time, attitude.w, attitude.x, -attitude.y, -attitude.z, rates.x, -rates.y, -rates.z, zeroQuat); // convert to frd
@@ -57,9 +56,9 @@ void sendMavlink() {
channels[0], channels[1], channels[2], channels[3], channels[4], channels[5], channels[6], channels[7], UINT8_MAX); 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 if (channels[0] != 0) sendMessage(&msg); // 0 means no RC input
float actuator[32]; float controls[8];
memcpy(actuator, motors, sizeof(motors)); memcpy(controls, motors, sizeof(motors));
mavlink_msg_actuator_output_status_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time, 4, actuator); mavlink_msg_actuator_control_target_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time, 0, controls);
sendMessage(&msg); sendMessage(&msg);
mavlink_msg_scaled_imu_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time, mavlink_msg_scaled_imu_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time,
@@ -79,6 +78,7 @@ void sendMessage(const void *msg) {
void receiveMavlink() { void receiveMavlink() {
uint8_t buf[MAVLINK_MAX_PACKET_LEN]; uint8_t buf[MAVLINK_MAX_PACKET_LEN];
int len = receiveWiFi(buf, MAVLINK_MAX_PACKET_LEN); int len = receiveWiFi(buf, MAVLINK_MAX_PACKET_LEN);
if (len) mavlinkConnected = true;
// New packet, parse it // New packet, parse it
mavlink_message_t msg; mavlink_message_t msg;
@@ -99,14 +99,11 @@ void handleMavlink(const void *_msg) {
if (m.target && m.target != SYSTEM_ID) return; // 0 is broadcast if (m.target && m.target != SYSTEM_ID) return; // 0 is broadcast
controlThrottle = m.z / 1000.0f; controlThrottle = m.z / 1000.0f;
controlPitch = m.x / 1000.0f * mavlinkControlScale; controlPitch = m.x / 1000.0f;
controlRoll = m.y / 1000.0f * mavlinkControlScale; controlRoll = m.y / 1000.0f;
controlYaw = m.r / 1000.0f * mavlinkControlScale; controlYaw = m.r / 1000.0f;
controlMode = 1; // STAB mode controlMode = NAN;
controlArmed = 1; // armed
controlTime = t; controlTime = t;
if (abs(controlYaw) < MAVLINK_CONTROL_YAW_DEAD_ZONE) controlYaw = 0;
} }
if (msg.msgid == MAVLINK_MSG_ID_PARAM_REQUEST_LIST) { if (msg.msgid == MAVLINK_MSG_ID_PARAM_REQUEST_LIST) {
@@ -174,24 +171,87 @@ void handleMavlink(const void *_msg) {
doCommand(data, true); doCommand(data, true);
} }
if (msg.msgid == MAVLINK_MSG_ID_SET_ATTITUDE_TARGET) {
if (mode != AUTO) return;
mavlink_set_attitude_target_t m;
mavlink_msg_set_attitude_target_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) 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) attitudeTarget.invalidate();
armed = m.thrust > 0;
}
if (msg.msgid == MAVLINK_MSG_ID_SET_ACTUATOR_CONTROL_TARGET) {
if (mode != AUTO) return;
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;
attitudeTarget.invalidate();
ratesTarget.invalidate();
torqueTarget.invalidate();
memcpy(motors, m.controls, sizeof(motors)); // copy motor thrusts
armed = motors[0] > 0 || motors[1] > 0 || motors[2] > 0 || motors[3] > 0;
}
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;
// 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);
}
}
// Handle commands // Handle commands
if (msg.msgid == MAVLINK_MSG_ID_COMMAND_LONG) { if (msg.msgid == MAVLINK_MSG_ID_COMMAND_LONG) {
mavlink_command_long_t m; mavlink_command_long_t m;
mavlink_msg_command_long_decode(&msg, &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 != SYSTEM_ID) return;
mavlink_message_t ack;
mavlink_message_t response; mavlink_message_t response;
bool accepted = false;
if (m.command == MAV_CMD_REQUEST_MESSAGE && m.param1 == MAVLINK_MSG_ID_AUTOPILOT_VERSION) { if (m.command == MAV_CMD_REQUEST_MESSAGE && m.param1 == MAVLINK_MSG_ID_AUTOPILOT_VERSION) {
mavlink_msg_command_ack_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &ack, m.command, MAV_RESULT_ACCEPTED, UINT8_MAX, 0, msg.sysid, msg.compid); accepted = true;
sendMessage(&ack);
mavlink_msg_autopilot_version_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &response, mavlink_msg_autopilot_version_pack(SYSTEM_ID, 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); MAV_PROTOCOL_CAPABILITY_PARAM_FLOAT | MAV_PROTOCOL_CAPABILITY_MAVLINK2, 1, 0, 1, 1, 0, 0, 0, 0, 0, 0, 0);
sendMessage(&response); sendMessage(&response);
} else {
mavlink_msg_command_ack_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &ack, m.command, MAV_RESULT_UNSUPPORTED, UINT8_MAX, 0, msg.sysid, msg.compid);
sendMessage(&ack);
} }
if (m.command == MAV_CMD_COMPONENT_ARM_DISARM) {
if (m.param1 && controlThrottle > 0.05) return; // don't arm if throttle is not low
accepted = true;
armed = m.param1 == 1;
}
if (m.command == MAV_CMD_DO_SET_MODE) {
if (m.param2 < 0 || m.param2 > AUTO) return; // incorrect mode
accepted = true;
mode = m.param2;
}
// 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);
sendMessage(&ack);
} }
} }

View File

@@ -38,9 +38,9 @@ void setupMotors() {
int getDutyCycle(float value) { int getDutyCycle(float value) {
value = constrain(value, 0, 1); value = constrain(value, 0, 1);
float pwm = mapff(value, 0, 1, PWM_MIN, PWM_MAX); float pwm = mapf(value, 0, 1, PWM_MIN, PWM_MAX);
if (value == 0) pwm = PWM_STOP; if (value == 0) pwm = PWM_STOP;
float duty = mapff(pwm, 0, 1000000 / PWM_FREQUENCY, 0, (1 << PWM_RESOLUTION) - 1); float duty = mapf(pwm, 0, 1000000 / PWM_FREQUENCY, 0, (1 << PWM_RESOLUTION) - 1);
return round(duty); return round(duty);
} }

View File

@@ -4,51 +4,57 @@
// Parameters storage in flash memory // Parameters storage in flash memory
#include <Preferences.h> #include <Preferences.h>
#include "util.h"
extern float channelZero[16]; extern float channelZero[16];
extern float channelMax[16]; extern float channelMax[16];
extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel; extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
extern float mavlinkControlScale;
Preferences storage; Preferences storage;
struct Parameter { struct Parameter {
const char *name; // max length is 16 const char *name; // max length is 15 (Preferences key limit)
float *variable; float *variable;
float value; // cache float value; // cache
}; };
Parameter parameters[] = { Parameter parameters[] = {
// control // control
{"ROLLRATE_P", &rollRatePID.p}, {"CTL_R_RATE_P", &rollRatePID.p},
{"ROLLRATE_I", &rollRatePID.i}, {"CTL_R_RATE_I", &rollRatePID.i},
{"ROLLRATE_D", &rollRatePID.d}, {"CTL_R_RATE_D", &rollRatePID.d},
{"ROLLRATE_I_LIM", &rollRatePID.windup}, {"CTL_R_RATE_WU", &rollRatePID.windup},
{"PITCHRATE_P", &pitchRatePID.p}, {"CTL_P_RATE_P", &pitchRatePID.p},
{"PITCHRATE_I", &pitchRatePID.i}, {"CTL_P_RATE_I", &pitchRatePID.i},
{"PITCHRATE_D", &pitchRatePID.d}, {"CTL_P_RATE_D", &pitchRatePID.d},
{"PITCHRATE_I_LIM", &pitchRatePID.windup}, {"CTL_P_RATE_WU", &pitchRatePID.windup},
{"YAWRATE_P", &yawRatePID.p}, {"CTL_Y_RATE_P", &yawRatePID.p},
{"YAWRATE_I", &yawRatePID.i}, {"CTL_Y_RATE_I", &yawRatePID.i},
{"YAWRATE_D", &yawRatePID.d}, {"CTL_Y_RATE_D", &yawRatePID.d},
{"ROLL_P", &rollPID.p}, {"CTL_R_P", &rollPID.p},
{"ROLL_I", &rollPID.i}, {"CTL_R_I", &rollPID.i},
{"ROLL_D", &rollPID.d}, {"CTL_R_D", &rollPID.d},
{"PITCH_P", &pitchPID.p}, {"CTL_P_P", &pitchPID.p},
{"PITCH_I", &pitchPID.i}, {"CTL_P_I", &pitchPID.i},
{"PITCH_D", &pitchPID.d}, {"CTL_P_D", &pitchPID.d},
{"YAW_P", &yawPID.p}, {"CTL_Y_P", &yawPID.p},
{"PITCHRATE_MAX", &maxRate.y}, {"CTL_P_RATE_MAX", &maxRate.y},
{"ROLLRATE_MAX", &maxRate.x}, {"CTL_R_RATE_MAX", &maxRate.x},
{"YAWRATE_MAX", &maxRate.z}, {"CTL_Y_RATE_MAX", &maxRate.z},
{"TILT_MAX", &tiltMax}, {"CTL_TILT_MAX", &tiltMax},
// imu // imu
{"ACC_BIAS_X", &accBias.x}, {"IMU_ROT_ROLL", &imuRotation.x},
{"ACC_BIAS_Y", &accBias.y}, {"IMU_ROT_PITCH", &imuRotation.y},
{"ACC_BIAS_Z", &accBias.z}, {"IMU_ROT_YAW", &imuRotation.z},
{"ACC_SCALE_X", &accScale.x}, {"IMU_ACC_BIAS_X", &accBias.x},
{"ACC_SCALE_Y", &accScale.y}, {"IMU_ACC_BIAS_Y", &accBias.y},
{"ACC_SCALE_Z", &accScale.z}, {"IMU_ACC_BIAS_Z", &accBias.z},
{"IMU_ACC_SCALE_X", &accScale.x},
{"IMU_ACC_SCALE_Y", &accScale.y},
{"IMU_ACC_SCALE_Z", &accScale.z},
// estimate
{"EST_ACC_WEIGHT", &accWeight},
{"EST_RATES_LPF_A", &ratesFilter.alpha},
// rc // rc
{"RC_ZERO_0", &channelZero[0]}, {"RC_ZERO_0", &channelZero[0]},
{"RC_ZERO_1", &channelZero[1]}, {"RC_ZERO_1", &channelZero[1]},
@@ -70,12 +76,7 @@ Parameter parameters[] = {
{"RC_PITCH", &pitchChannel}, {"RC_PITCH", &pitchChannel},
{"RC_THROTTLE", &throttleChannel}, {"RC_THROTTLE", &throttleChannel},
{"RC_YAW", &yawChannel}, {"RC_YAW", &yawChannel},
{"RC_ARMED", &armedChannel},
{"RC_MODE", &modeChannel}, {"RC_MODE", &modeChannel},
#if WIFI_ENABLED
// MAVLink
{"MAV_CTRL_SCALE", &mavlinkControlScale},
#endif
}; };
void setupParameters() { void setupParameters() {
@@ -124,10 +125,9 @@ bool setParameter(const char *name, const float value) {
} }
void syncParameters() { void syncParameters() {
static double lastSync = 0; static Rate rate(1);
if (t - lastSync < 1) return; // sync once per second if (!rate) return; // sync once per second
if (motorsActive()) return; // don't use flash while flying, it may cause a delay if (motorsActive()) return; // don't use flash while flying, it may cause a delay
lastSync = t;
for (auto &parameter : parameters) { for (auto &parameter : parameters) {
if (parameter.value == *parameter.variable) continue; if (parameter.value == *parameter.variable) continue;

View File

@@ -9,40 +9,44 @@
class PID { class PID {
public: public:
float p = 0; float p, i, d;
float i = 0; float windup;
float d = 0; float dtMax;
float windup = 0;
float derivative = 0; float derivative = 0;
float integral = 0; float integral = 0;
LowPassFilter<float> lpf; // low pass filter for derivative term LowPassFilter<float> lpf; // low pass filter for derivative term
PID(float p, float i, float d, float windup = 0, float dAlpha = 1) : p(p), i(i), d(d), windup(windup), lpf(dAlpha) {}; PID(float p, float i, float d, float windup = 0, float dAlpha = 1, float dtMax = 0.1) :
p(p), i(i), d(d), windup(windup), lpf(dAlpha), dtMax(dtMax) {}
float update(float error, float dt) { float update(float error) {
integral += error * dt; float dt = t - prevTime;
if (isfinite(prevError) && dt > 0) { if (dt > 0 && dt < dtMax) {
// calculate derivative if both dt and prevError are valid integral += error * dt;
derivative = (error - prevError) / dt; derivative = lpf.update((error - prevError) / dt); // compute derivative and apply low-pass filter
} else {
// apply low pass filter to derivative integral = 0;
derivative = lpf.update(derivative); derivative = 0;
} }
prevError = error; prevError = error;
prevTime = t;
return p * error + constrain(i * integral, -windup, windup) + d * derivative; // PID return p * error + constrain(i * integral, -windup, windup) + d * derivative; // PID
} }
void reset() { void reset() {
prevError = NAN; prevError = NAN;
prevTime = NAN;
integral = 0; integral = 0;
derivative = 0; derivative = 0;
lpf.reset();
} }
private: private:
float prevError = NAN; float prevError = NAN;
float prevTime = NAN;
}; };

View File

@@ -45,7 +45,7 @@ public:
cx * cy * sz - sx * sy * cz); cx * cy * sz - sx * sy * cz);
} }
static Quaternion fromBetweenVectors(Vector u, Vector v) { static Quaternion fromBetweenVectors(const Vector& u, const Vector& v) {
float dot = u.x * v.x + u.y * v.y + u.z * v.z; float dot = u.x * v.x + u.y * v.y + u.z * v.z;
float w1 = u.y * v.z - u.z * v.y; float w1 = u.y * v.z - u.z * v.y;
float w2 = u.z * v.x - u.x * v.z; float w2 = u.z * v.x - u.x * v.z;
@@ -64,6 +64,22 @@ public:
return isfinite(w) && isfinite(x) && isfinite(y) && isfinite(z); return isfinite(w) && isfinite(x) && isfinite(y) && isfinite(z);
} }
bool valid() const {
return finite();
}
bool invalid() const {
return !valid();
}
void invalidate() {
w = NAN;
x = NAN;
y = NAN;
z = NAN;
}
float norm() const { float norm() const {
return sqrt(w * w + x * x + y * y + z * z); return sqrt(w * w + x * x + y * y + z * z);
} }
@@ -116,29 +132,31 @@ public:
return euler; return euler;
} }
float getRoll() const {
return toEuler().x;
}
float getPitch() const {
return toEuler().y;
}
float getYaw() const { float getYaw() const {
// https://github.com/ros/geometry2/blob/589caf083cae9d8fae7effdb910454b4681b9ec1/tf2/include/tf2/impl/utils.h#L122 return toEuler().z;
float yaw; }
float sqx = x * x;
float sqy = y * y; void setRoll(float roll) {
float sqz = z * z; Vector euler = toEuler();
float sqw = w * w; *this = Quaternion::fromEuler(Vector(roll, euler.y, euler.z));
double sarg = -2 * (x * z - w * y) / (sqx + sqy + sqz + sqw); }
if (sarg <= -0.99999) {
yaw = -2 * atan2(y, x); void setPitch(float pitch) {
} else if (sarg >= 0.99999) { Vector euler = toEuler();
yaw = 2 * atan2(y, x); *this = Quaternion::fromEuler(Vector(euler.x, pitch, euler.z));
} else {
yaw = atan2(2 * (x * y + w * z), sqw + sqx - sqy - sqz);
}
return yaw;
} }
void setYaw(float yaw) { void setYaw(float yaw) {
// TODO: optimize?
Vector euler = toEuler(); Vector euler = toEuler();
euler.z = yaw; *this = Quaternion::fromEuler(Vector(euler.x, euler.y, yaw));
(*this) = Quaternion::fromEuler(euler);
} }
Quaternion operator * (const Quaternion& q) const { Quaternion operator * (const Quaternion& q) const {

View File

@@ -6,24 +6,24 @@
#include <SBUS.h> #include <SBUS.h>
#include "util.h" #include "util.h"
SBUS RC(Serial2); // NOTE: Use RC(Serial2, 16, 17) if you use the old UART2 pins SBUS rc(Serial2); // NOTE: Use RC(Serial2, 16, 17) if you use the old UART2 pins
uint16_t channels[16]; // raw rc channels uint16_t channels[16]; // raw rc channels
double controlTime; // time of the last controls update float controlTime; // time of the last controls update
float channelZero[16]; // calibration zero values float channelZero[16]; // calibration zero values
float channelMax[16]; // calibration max values float channelMax[16]; // calibration max values
// Channels mapping (using float to store in parameters): // Channels mapping (using float to store in parameters):
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, armedChannel = NAN, modeChannel = NAN; float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
void setupRC() { void setupRC() {
print("Setup RC\n"); print("Setup RC\n");
RC.begin(); rc.begin();
} }
bool readRC() { bool readRC() {
if (RC.read()) { if (rc.read()) {
SBUSData data = RC.data(); SBUSData data = rc.data();
for (int i = 0; i < 16; i++) channels[i] = data.ch[i]; // copy channels data for (int i = 0; i < 16; i++) channels[i] = data.ch[i]; // copy channels data
normalizeRC(); normalizeRC();
controlTime = t; controlTime = t;
@@ -42,7 +42,6 @@ void normalizeRC() {
controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : NAN; controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : NAN;
controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : NAN; controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : NAN;
controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : NAN; controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : NAN;
controlArmed = armedChannel >= 0 ? controls[(int)armedChannel] : 1; // assume armed by default
controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN; controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN;
} }
@@ -50,16 +49,15 @@ void calibrateRC() {
uint16_t zero[16]; uint16_t zero[16];
uint16_t center[16]; uint16_t center[16];
uint16_t max[16]; uint16_t max[16];
print("1/9 Calibrating RC: put all switches to default positions [3 sec]\n"); print("1/8 Calibrating RC: put all switches to default positions [3 sec]\n");
pause(3); pause(3);
calibrateRCChannel(NULL, zero, zero, "2/9 Move sticks [3 sec]\n... ...\n... .o.\n.o. ...\n"); calibrateRCChannel(NULL, zero, zero, "2/8 Move sticks [3 sec]\n... ...\n... .o.\n.o. ...\n");
calibrateRCChannel(NULL, center, center, "3/9 Move sticks [3 sec]\n... ...\n.o. .o.\n... ...\n"); calibrateRCChannel(NULL, center, center, "3/8 Move sticks [3 sec]\n... ...\n.o. .o.\n... ...\n");
calibrateRCChannel(&throttleChannel, zero, max, "4/9 Move sticks [3 sec]\n.o. ...\n... .o.\n... ...\n"); calibrateRCChannel(&throttleChannel, zero, max, "4/8 Move sticks [3 sec]\n.o. ...\n... .o.\n... ...\n");
calibrateRCChannel(&yawChannel, center, max, "5/9 Move sticks [3 sec]\n... ...\n..o .o.\n... ...\n"); calibrateRCChannel(&yawChannel, center, max, "5/8 Move sticks [3 sec]\n... ...\n..o .o.\n... ...\n");
calibrateRCChannel(&pitchChannel, zero, max, "6/9 Move sticks [3 sec]\n... .o.\n... ...\n.o. ...\n"); calibrateRCChannel(&pitchChannel, zero, max, "6/8 Move sticks [3 sec]\n... .o.\n... ...\n.o. ...\n");
calibrateRCChannel(&rollChannel, zero, max, "7/9 Move sticks [3 sec]\n... ...\n... ..o\n.o. ...\n"); calibrateRCChannel(&rollChannel, zero, max, "7/8 Move sticks [3 sec]\n... ...\n... ..o\n.o. ...\n");
calibrateRCChannel(&armedChannel, zero, max, "8/9 Switch to armed [3 sec]\n"); calibrateRCChannel(&modeChannel, zero, max, "8/8 Put mode switch to max [3 sec]\n");
calibrateRCChannel(&modeChannel, zero, max, "9/9 Disarm and switch mode to max [3 sec]\n");
printRCCalibration(); printRCCalibration();
} }
@@ -94,6 +92,5 @@ void printRCCalibration() {
print("Pitch %-7g%-7g%-7g\n", pitchChannel, pitchChannel >= 0 ? channelZero[(int)pitchChannel] : NAN, pitchChannel >= 0 ? channelMax[(int)pitchChannel] : 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("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("Throttle %-7g%-7g%-7g\n", throttleChannel, throttleChannel >= 0 ? channelZero[(int)throttleChannel] : NAN, throttleChannel >= 0 ? channelMax[(int)throttleChannel] : NAN);
print("Armed %-7g%-7g%-7g\n", armedChannel, armedChannel >= 0 ? channelZero[(int)armedChannel] : NAN, armedChannel >= 0 ? channelMax[(int)armedChannel] : NAN);
print("Mode %-7g%-7g%-7g\n", modeChannel, modeChannel >= 0 ? channelZero[(int)modeChannel] : NAN, modeChannel >= 0 ? channelMax[(int)modeChannel] : NAN); print("Mode %-7g%-7g%-7g\n", modeChannel, modeChannel >= 0 ? channelZero[(int)modeChannel] : NAN, modeChannel >= 0 ? channelMax[(int)modeChannel] : NAN);
} }

48
flix/safety.ino Normal file
View File

@@ -0,0 +1,48 @@
// Copyright (c) 2024 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Fail-safe functions
#define RC_LOSS_TIMEOUT 1
#define DESCEND_TIME 10
extern float controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw;
void failsafe() {
rcLossFailsafe();
autoFailsafe();
}
// RC loss failsafe
void rcLossFailsafe() {
if (controlTime == 0) return; // no RC at all
if (!armed) return;
if (t - controlTime > RC_LOSS_TIMEOUT) {
descend();
}
}
// Smooth descend on RC lost
void descend() {
mode = AUTO;
attitudeTarget = Quaternion();
thrustTarget -= dt / DESCEND_TIME;
if (thrustTarget < 0) {
thrustTarget = 0;
armed = false;
}
}
// 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
}
roll = controlRoll;
pitch = controlPitch;
yaw = controlYaw;
throttle = controlThrottle;
}

View File

@@ -6,7 +6,7 @@
float loopRate; // Hz float loopRate; // Hz
void step() { void step() {
double now = micros() / 1000000.0; float now = micros() / 1000000.0;
dt = now - t; dt = now - t;
t = now; t = now;
@@ -18,7 +18,7 @@ void step() {
} }
void computeLoopRate() { void computeLoopRate() {
static double windowStart = 0; static float windowStart = 0;
static uint32_t rate = 0; static uint32_t rate = 0;
rate++; rate++;
if (t - windowStart >= 1) { // 1 second window if (t - windowStart >= 1) { // 1 second window

View File

@@ -10,13 +10,18 @@
#include <soc/rtc_cntl_reg.h> #include <soc/rtc_cntl_reg.h>
const float ONE_G = 9.80665; const float ONE_G = 9.80665;
extern float t;
float mapf(long x, long in_min, long in_max, float out_min, float out_max) { float mapf(float x, float in_min, float in_max, float out_min, float out_max) {
return (float)(x - in_min) * (out_max - out_min) / (float)(in_max - in_min) + out_min; return (x - in_min) * (out_max - out_min) / (in_max - in_min) + out_min;
} }
float mapff(float x, float in_min, float in_max, float out_min, float out_max) { bool invalid(float x) {
return (x - in_min) * (out_max - out_min) / (in_max - in_min) + out_min; return !isfinite(x);
}
bool valid(float x) {
return isfinite(x);
} }
// Wrap angle to [-PI, PI) // Wrap angle to [-PI, PI)
@@ -44,3 +49,37 @@ void splitString(String& str, String& token0, String& token1, String& token2) {
token1 = strtok(NULL, " "); // String(NULL) creates empty string token1 = strtok(NULL, " "); // String(NULL) creates empty string
token2 = strtok(NULL, ""); token2 = strtok(NULL, "");
} }
// Rate limiter
class Rate {
public:
float rate;
float last = 0;
Rate(float rate) : rate(rate) {}
operator bool() {
if (t - last >= 1 / rate) {
last = t;
return true;
}
return false;
}
};
// Delay filter for boolean signals - ensures the signal is on for at least 'delay' seconds
class Delay {
public:
float delay;
float start = NAN;
Delay(float delay) : delay(delay) {}
bool update(bool on) {
if (!on) {
start = NAN;
return false;
} else if (isnan(start)) {
start = t;
}
return t - start >= delay;
}
};

View File

@@ -21,6 +21,21 @@ public:
return isfinite(x) && isfinite(y) && isfinite(z); return isfinite(x) && isfinite(y) && isfinite(z);
} }
bool valid() const {
return finite();
}
bool invalid() const {
return !valid();
}
void invalidate() {
x = NAN;
y = NAN;
z = NAN;
}
float norm() const { float norm() const {
return sqrt(x * x + y * y + z * z); return sqrt(x * x + y * y + z * z);
} }

View File

@@ -13,6 +13,7 @@
#define WIFI_PASSWORD "flixwifi" #define WIFI_PASSWORD "flixwifi"
#define WIFI_UDP_PORT 14550 #define WIFI_UDP_PORT 14550
#define WIFI_UDP_REMOTE_PORT 14550 #define WIFI_UDP_REMOTE_PORT 14550
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
WiFiUDP udp; WiFiUDP udp;
@@ -24,7 +25,7 @@ void setupWiFi() {
void sendWiFi(const uint8_t *buf, int len) { void sendWiFi(const uint8_t *buf, int len) {
if (WiFi.softAPIP() == IPAddress(0, 0, 0, 0) && WiFi.status() != WL_CONNECTED) return; if (WiFi.softAPIP() == IPAddress(0, 0, 0, 0) && WiFi.status() != WL_CONNECTED) return;
udp.beginPacket(WiFi.softAPBroadcastIP(), WIFI_UDP_REMOTE_PORT); udp.beginPacket(udp.remoteIP() ? udp.remoteIP() : WIFI_UDP_REMOTE_ADDR, WIFI_UDP_REMOTE_PORT);
udp.write(buf, len); udp.write(buf, len);
udp.endPacket(); udp.endPacket();
} }
@@ -34,4 +35,15 @@ int receiveWiFi(uint8_t *buf, int len) {
return udp.read(buf, len); 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());
print("MAVLink connected: %d\n", mavlinkConnected);
}
#endif #endif

View File

@@ -1,7 +1,7 @@
cmake_minimum_required(VERSION 3.5 FATAL_ERROR) cmake_minimum_required(VERSION 3.5 FATAL_ERROR)
project(flix_gazebo) project(flix_gazebo)
# === gazebo plugin # Gazebo plugin
find_package(gazebo REQUIRED) find_package(gazebo REQUIRED)
find_package(SDL2 REQUIRED) find_package(SDL2 REQUIRED)
include_directories(${GAZEBO_INCLUDE_DIRS}) include_directories(${GAZEBO_INCLUDE_DIRS})

View File

@@ -1,15 +1,99 @@
# Gazebo Simulation # Simulation
<img src="../docs/img/simulator.png" width=500 alt="Flix simulator"> The Flix drone simulator is based on Gazebo 11 and runs the firmware code in virtual physical environment.
## Building and running Gazebo 11 works on **Ubuntu 20.04** and used to work on macOS. However, on the recent macOS versions it seems to be broken, so Ubuntu 20.04 is recommended.
See [building and running instructions](../docs/build.md#simulation). <img src="../docs/img/simulator1.png" width=600 alt="Flix simulator running on macOS">
## Installation
1. Clone the Flix repository using it:
```bash
git clone https://github.com/okalachev/flix.git && cd flix
```
2. Install Arduino CLI:
```bash
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
```
3. Install Gazebo 11:
```bash
sudo sh -c 'echo "deb http://packages.osrfoundation.org/gazebo/ubuntu-stable `lsb_release -cs` main" > /etc/apt/sources.list.d/gazebo-stable.list'
wget https://packages.osrfoundation.org/gazebo.key -O - | sudo apt-key add -
sudo apt-get update
sudo apt-get install -y gazebo11 libgazebo11-dev
```
Set up your Gazebo environment variables:
```bash
echo "source /usr/share/gazebo/setup.sh" >> ~/.bashrc
source ~/.bashrc
```
4. Install SDL2 and other dependencies:
```bash
sudo apt-get update && sudo apt-get install build-essential libsdl2-dev
```
5. Add your user to the `input` group to enable joystick support (you need to re-login after this command):
```bash
sudo usermod -a -G input $USER
```
6. Run the simulation:
```bash
make simulator
```
## Usage
Just like the real drone, the simulator can be controlled using a USB remote control or a smartphone.
### Control with smartphone
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone. For **iOS**, use [QGroundControl build from TAJISOFT](https://apps.apple.com/ru/app/qgc-from-tajisoft/id1618653051).
2. Connect your smartphone to the same Wi-Fi network as the machine running the simulator.
3. If you're using a virtual machine, make sure that its network is set to the **bridged** mode with Wi-Fi adapter selected.
4. Run the simulation.
5. Open QGroundControl app. It should connect and begin showing the virtual drone's telemetry automatically.
6. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
7. Use the virtual joystick to fly the drone!
> [!TIP]
> Decrease `CTL_TILT_MAX` parameter when flying using the smartphone to make the controls less sensitive.
### Control with USB remote control
1. Connect your USB remote control to the machine running the simulator.
2. Run the simulation.
3. Calibrate the RC using `cr` command in the command line interface.
4. Use the USB remote control to fly the drone!
### Piloting
To start the flight, arm the drone moving the throttle stick to the bottom right position:
<img src="../docs/img/arming.svg" width="150">
To disarm, move the throttle stick to the bottom left position:
<img src="../docs/img/disarming.svg" width="150">
See other piloting and usage details in general [usage article](../docs/usage.md).
## Code structure ## Code structure
Flix simulator is based on [Gazebo Classic](https://classic.gazebosim.org) and consists of the following components: Flix simulator consists of the following components:
* Physical model of the drone: [`models/flix/flix.sdf`](models/flix/flix.sdf). * Physical model of the drone in Gazebo format: [`models/flix/flix.sdf`](models/flix/flix.sdf).
* Plugin for Gazebo: [`simulator.cpp`](simulator.cpp). The plugin is attached to the physical model. It receives stick positions from the controller, gets the data from the virtual sensors, and then passes this data to the Arduino code. * Plugin for Gazebo: [`simulator.cpp`](simulator.cpp). The plugin is attached to the physical model. It receives stick positions from the controller, gets the data from the virtual sensors, and then passes this data to the Arduino code.
* Arduino imitation: [`Arduino.h`](Arduino.h). This file contains partial implementation of the Arduino API, that is working within Gazebo plugin environment. * Arduino emulation: [`Arduino.h`](Arduino.h). This file contains partial implementation of the Arduino API, that is working within Gazebo plugin environment.

View File

@@ -12,15 +12,17 @@
#define WIFI_ENABLED 1 #define WIFI_ENABLED 1
double t = NAN; float t = NAN;
float dt; float dt;
float motors[4]; float motors[4];
float controlRoll, controlPitch, controlYaw, controlThrottle, controlArmed, controlMode; float controlRoll, controlPitch, controlYaw, controlThrottle = NAN;
float controlMode = NAN;
Vector acc; Vector acc;
Vector gyro; Vector gyro;
Vector rates; Vector rates;
Quaternion attitude; Quaternion attitude;
bool landed; bool landed;
Vector imuRotation;
// declarations // declarations
void step(); void step();
@@ -28,9 +30,9 @@ void computeLoopRate();
void applyGyro(); void applyGyro();
void applyAcc(); void applyAcc();
void control(); void control();
void interpretRC(); void interpretControls();
void controlAttitude(); void controlAttitude();
void controlRate(); void controlRates();
void controlTorque(); void controlTorque();
const char* getModeName(); const char* getModeName();
void sendMotors(); void sendMotors();
@@ -44,7 +46,8 @@ void normalizeRC();
void calibrateRC(); void calibrateRC();
void calibrateRCChannel(float *channel, uint16_t zero[16], uint16_t max[16], const char *str); void calibrateRCChannel(float *channel, uint16_t zero[16], uint16_t max[16], const char *str);
void printRCCalibration(); void printRCCalibration();
void dumpLog(); void printLogHeader();
void printLogData();
void processMavlink(); void processMavlink();
void sendMavlink(); void sendMavlink();
void sendMessage(const void *msg); void sendMessage(const void *msg);
@@ -54,9 +57,9 @@ void mavlinkPrint(const char* str);
void sendMavlinkPrint(); void sendMavlinkPrint();
inline Quaternion fluToFrd(const Quaternion &q); inline Quaternion fluToFrd(const Quaternion &q);
void failsafe(); void failsafe();
void armingFailsafe();
void rcLossFailsafe(); void rcLossFailsafe();
void descend(); void descend();
void autoFailsafe();
int parametersCount(); int parametersCount();
const char *getParameterName(int index); const char *getParameterName(int index);
float getParameter(int index); float getParameter(int index);
@@ -69,6 +72,8 @@ void resetParameters();
void setLED(bool on) {}; void setLED(bool on) {};
void calibrateGyro() { print("Skip gyro calibrating\n"); }; void calibrateGyro() { print("Skip gyro calibrating\n"); };
void calibrateAccel() { print("Skip accel calibrating\n"); }; void calibrateAccel() { print("Skip accel calibrating\n"); };
void calibrateLevel() { print("Skip level calibrating\n"); };
void printIMUCalibration() { print("cal: N/A\n"); }; void printIMUCalibration() { print("cal: N/A\n"); };
void printIMUInfo() {}; void printIMUInfo() {};
void printWiFiInfo() {};
Vector accBias, gyroBias, accScale(1, 1, 1); Vector accBias, gyroBias, accScale(1, 1, 1);

View File

@@ -21,7 +21,7 @@
#include "cli.ino" #include "cli.ino"
#include "control.ino" #include "control.ino"
#include "estimate.ino" #include "estimate.ino"
#include "failsafe.ino" #include "safety.ino"
#include "log.ino" #include "log.ino"
#include "lpf.h" #include "lpf.h"
#include "mavlink.ino" #include "mavlink.ino"
@@ -59,6 +59,7 @@ public:
void OnReset() { void OnReset() {
attitude = Quaternion(); // reset estimated attitude attitude = Quaternion(); // reset estimated attitude
armed = false;
__resetTime += __micros; __resetTime += __micros;
gzmsg << "Flix plugin reset" << endl; gzmsg << "Flix plugin reset" << endl;
} }

View File

@@ -13,6 +13,7 @@
#define WIFI_UDP_PORT 14580 #define WIFI_UDP_PORT 14580
#define WIFI_UDP_REMOTE_PORT 14550 #define WIFI_UDP_REMOTE_PORT 14550
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
int wifiSocket; int wifiSocket;
@@ -35,7 +36,7 @@ void sendWiFi(const uint8_t *buf, int len) {
if (wifiSocket == 0) setupWiFi(); if (wifiSocket == 0) setupWiFi();
sockaddr_in addr; // remote address sockaddr_in addr; // remote address
addr.sin_family = AF_INET; addr.sin_family = AF_INET;
addr.sin_addr.s_addr = INADDR_BROADCAST; // send UDP broadcast addr.sin_addr.s_addr = inet_addr(WIFI_UDP_REMOTE_ADDR);
addr.sin_port = htons(WIFI_UDP_REMOTE_PORT); addr.sin_port = htons(WIFI_UDP_REMOTE_PORT);
sendto(wifiSocket, buf, len, 0, (sockaddr *)&addr, sizeof(addr)); sendto(wifiSocket, buf, len, 0, (sockaddr *)&addr, sizeof(addr));
} }

View File

@@ -49,6 +49,8 @@ for configuration in props['configurations']:
print('Check configuration', configuration['name']) print('Check configuration', configuration['name'])
for include_path in configuration.get('includePath', []): for include_path in configuration.get('includePath', []):
if include_path.startswith('/opt/') or include_path.startswith('/usr/'): # don't check non-Arduino libs
continue
check_path(include_path) check_path(include_path)
for forced_include in configuration.get('forcedInclude', []): for forced_include in configuration.get('forcedInclude', []):

View File

@@ -3,21 +3,49 @@
# Download flight log remotely and save to file # Download flight log remotely and save to file
import os import os
import time
import datetime import datetime
import struct
from pymavlink.dialects.v20.common import MAVLink_log_data_message
from pyflix import Flix from pyflix import Flix
DIR = os.path.dirname(os.path.realpath(__file__)) DIR = os.path.dirname(os.path.realpath(__file__))
flix = Flix() flix = Flix()
print('Downloading log...') print('Downloading log...')
lines = flix.cli('log').splitlines()
# sort by timestamp header = flix.cli('log')
header = lines.pop(0) print('Received header:\n- ' + '\n- '.join(header.split(',')))
lines.sort(key=lambda line: float(line.split(',')[0]))
records = []
def on_record(msg: MAVLink_log_data_message):
global stop
stop = time.time() + 1 # extend timeout
records.append([])
i = 0
data = bytes(msg.data)
while i + 4 <= msg.count:
records[-1].append(struct.unpack('<f', data[i:i+4])[0])
i += 4
stop = time.time() + 3
flix.on('mavlink.LOG_DATA', on_record)
flix.mavlink.log_request_data_send(flix.system_id, 0, 0, 0, 0xFFFFFFFF)
while time.time() < stop:
time.sleep(1)
flix.off(on_record)
records.sort(key=lambda record: record[0])
records = [record for record in records if record[0] != 0]
print(f'Received records: {len(records)}')
log = open(f'{DIR}/log/{datetime.datetime.now().isoformat()}.csv', 'wb') log = open(f'{DIR}/log/{datetime.datetime.now().isoformat()}.csv', 'wb')
content = header.encode() + b'\n' + b'\n'.join(line.encode() for line in lines) log.write(header.encode() + b'\n')
log.write(content) for record in records:
line = ','.join(f'{value}' for value in record)
log.write(line.encode() + b'\n')
print(f'Written {os.path.relpath(log.name, os.curdir)}') print(f'Written {os.path.relpath(log.name, os.curdir)}')

View File

@@ -1,8 +1,8 @@
# Flix Python library # Flix Python library
The Flix Python library allows you to remotely connect to a Flix quadcopter. It provides access to telemetry data, supports executing CLI commands, and controlling the drone's flight. The Flix Python library allows you to remotely connect to a Flix quadcopter. It provides access to telemetry data, supports executing console commands, and controlling the drone's flight.
To use the library, connect to the drone's Wi-Fi. To use it with the simulator, ensure the script runs on the same local network as the simulator. To use the library, connect to the drone's Wi-Fi. To use it with the simulator, ensure the script runs on the same network as the simulator.
## Installation ## Installation
@@ -30,7 +30,7 @@ flix = Flix() # create a Flix object and wait for connection
### Telemetry ### Telemetry
Basic telemetry is available through object properties. The properties 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 itself:
```python ```python
print(flix.connected) # True if connected to the drone print(flix.connected) # True if connected to the drone
@@ -41,13 +41,16 @@ print(flix.attitude) # attitude quaternion [w, x, y, z]
print(flix.attitude_euler) # attitude as Euler angles [roll, pitch, yaw] print(flix.attitude_euler) # attitude as Euler angles [roll, pitch, yaw]
print(flix.rates) # angular rates [roll_rate, pitch_rate, yaw_rate] print(flix.rates) # angular rates [roll_rate, pitch_rate, yaw_rate]
print(flix.channels) # raw RC channels (list) print(flix.channels) # raw RC channels (list)
print(flix.motors) # motors outputs (list) print(flix.motors) # motor outputs (list)
print(flix.acc) # accelerometer output (list) print(flix.acc) # accelerometer output (list)
print(flix.gyro) # gyroscope output (list) print(flix.gyro) # gyroscope output (list)
``` ```
> [!NOTE] The library uses the Front-Left-Up coordinate system — the same as the firmware:
> The library uses the Front-Left-Up coordinate system — the same as in the firmware. All angles are in radians.
<img src="../../docs/img/drone-axes-rotate.svg" width="300">
All angles are in radians.
### Events ### Events
@@ -59,6 +62,13 @@ flix.on('disconnected', lambda: print('Disconnected from Flix'))
flix.on('print', lambda text: print(f'Flix says: {text}')) flix.on('print', lambda text: print(f'Flix says: {text}'))
``` ```
Unsubscribe from events using `off` method:
```python
flix.off('print') # unsubscribe from print events
flix.off(callback) # unsubscribe specific callback
```
You can also wait for specific events using `wait` method. This method returns the data associated with the event: You can also wait for specific events using `wait` method. This method returns the data associated with the event:
```python ```python
@@ -66,13 +76,14 @@ gyro = flix.wait('gyro') # wait for gyroscope update
attitude = flix.wait('attitude', timeout=3) # wait for attitude update, raise TimeoutError after 3 seconds attitude = flix.wait('attitude', timeout=3) # wait for attitude update, raise TimeoutError after 3 seconds
``` ```
The `value` argument specifies a condition for filtering events. It can be either an expected value or a callable: The second argument (`value`) specifies a condition for filtering events. It can be either an expected value or a callable:
```python ```python
flix.wait('armed', value=True) # wait until armed flix.wait('armed', True) # wait until armed
flix.wait('armed', value=False) # wait until disarmed flix.wait('armed', False) # wait until disarmed
flix.wait('motors', value=lambda motors: not any(motors)) # wait until all motors stop flix.wait('mode', 'AUTO') # wait until flight mode is switched to AUTO
flix.wait('attitude_euler', value=lambda att: att[0] > 0) # wait until roll angle is positive flix.wait('motors', lambda motors: not any(motors)) # wait until all motors stop
flix.wait('attitude_euler', lambda att: att[0] > 0) # wait until roll angle is positive
``` ```
Full list of events: Full list of events:
@@ -89,17 +100,17 @@ Full list of events:
|`attitude_euler`|Attitude update|Euler angles (*list*)| |`attitude_euler`|Attitude update|Euler angles (*list*)|
|`rates`|Angular rates update|Angular rates (*list*)| |`rates`|Angular rates update|Angular rates (*list*)|
|`channels`|Raw RC channels update|Raw RC channels (*list*)| |`channels`|Raw RC channels update|Raw RC channels (*list*)|
|`motors`|Motors outputs update|Motors outputs (*list*)| |`motors`|Motor outputs update|Motor outputs (*list*)|
|`acc`|Accelerometer update|Accelerometer output (*list*)| |`acc`|Accelerometer update|Accelerometer output (*list*)|
|`gyro`|Gyroscope update|Gyroscope output (*list*)| |`gyro`|Gyroscope update|Gyroscope output (*list*)|
|`mavlink`|Received MAVLink message|Message object| |`mavlink`|Received MAVLink message|Message object|
|`mavlink.<message_name>`|Received specific MAVLink message|Message object| |`mavlink.<message_name>`|Received specific MAVLink message|Message object|
|`mavlink.<message_id>`|Received specific MAVLink message|Message object| |`mavlink.<message_id>`|Received specific MAVLink message|Message object|
|`value`|Named value update (see below)|Name, value| |`value`|Named value update (see below)|Name, value|
|`value.<name>`|Specific named value update (see bellow)|Value| |`value.<name>`|Specific named value update (see below)|Value|
> [!NOTE] > [!NOTE]
> Update events trigger on every new data from the drone, and do not mean the value is changed. > Update events trigger on every new piece of data from the drone, and do not mean the value has changed.
### Common methods ### Common methods
@@ -107,10 +118,10 @@ Get and set firmware parameters using `get_param` and `set_param` methods:
```python ```python
pitch_p = flix.get_param('PITCH_P') # get parameter value pitch_p = flix.get_param('PITCH_P') # get parameter value
flix.set_param('PITCH_P', 5) # set parameter value flix.set_param('PITCH_P', 5) # set parameter value
``` ```
Execute CLI commands using `cli` method. This method returns command response: Execute console commands using `cli` method. This method returns the command response:
```python ```python
imu = flix.cli('imu') # get detailed IMU data imu = flix.cli('imu') # get detailed IMU data
@@ -121,21 +132,65 @@ flix.cli('reboot') # reboot the drone
> [!TIP] > [!TIP]
> Use `help` command to get the list of available commands. > Use `help` command to get the list of available commands.
You can arm and disarm the drone using `set_armed` method (warning: the drone will fall if disarmed in the air):
```python
flix.set_armed(True) # arm the drone
flix.set_armed(False) # disarm the drone
```
You can pass pilot's controls using `set_controls` method:
```python
flix.set_controls(roll=0, pitch=0, yaw=0, throttle=0.6)
```
> [!WARNING]
> This method **is not intended for automatic flights**, only for adding support for a custom pilot input device.
### Automatic flight ### Automatic flight
The flight control feature is in development. List of methods intended for automatic flight control: To perform automatic flight, switch the mode to *AUTO*, either from the remote control, or from the code:
* `set_position` ```python
* `set_velocity` flix.set_mode('AUTO')
* `set_attitude` ```
* `set_rates`
* `set_motors` In this mode you can set flight control targets. Setting attitude target:
* `set_controls`
* `set_mode` ```python
flix.set_attitude([0.1, 0.2, 0.3], 0.6) # set target roll, pitch, yaw and thrust
flix.set_attitude([1, 0, 0, 0], 0.6) # set target attitude quaternion and thrust
```
Setting angular rates target:
```python
flix.set_rates([0.1, 0.2, 0.3], 0.6) # set target roll rate, pitch rate, yaw rate and thrust
```
You also can control raw motor outputs directly:
```python
flix.set_motors([0.5, 0.5, 0.5, 0.5]) # set motor outputs in range [0, 1]
```
In *AUTO* mode, the drone will arm automatically if the thrust is greater than zero, and disarm if thrust is zero. Therefore, to disarm the drone, set thrust to zero:
```python
flix.set_attitude([0, 0, 0], 0) # disarm the drone
```
The following methods are in development and are not functional yet:
* `set_position` — set target position.
* `set_velocity` — set target velocity.
To exit *AUTO* mode move control sticks and the drone will switch to *STAB* mode.
## Usage alongside QGroundControl ## Usage alongside QGroundControl
You can use the Flix library alongside the QGroundControl app, using a proxy mode. To do that: You can use the Flix library alongside the QGroundControl app, using proxy mode. To do that:
1. Run proxy for `pyflix` and QGroundControl in background: 1. Run proxy for `pyflix` and QGroundControl in background:
@@ -151,6 +206,8 @@ You can use the Flix library alongside the QGroundControl app, using a proxy mod
* *Port*: 14560 * *Port*: 14560
4. Restart QGroundControl. 4. Restart QGroundControl.
<img src="../../docs/img/qgc-proxy.png" width="300">
Now you can run `pyflix` scripts and QGroundControl simultaneously. Now you can run `pyflix` scripts and QGroundControl simultaneously.
## Tools ## Tools
@@ -201,11 +258,11 @@ You can send values from the firmware like this (`mavlink.ino`):
```cpp ```cpp
// Send float named value // Send float named value
mavlink_msg_named_value_float_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, t, "some_value", loopRate); mavlink_msg_named_value_float_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, t, "loop_rate", loopRate);
sendMessage(&msg); sendMessage(&msg);
// Send vector named value // Send vector named value
mavlink_msg_debug_vect_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, "some_vector", t, gyroBias.x, gyroBias.y, gyroBias.z); mavlink_msg_debug_vect_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, "gyro_bias", t, gyroBias.x, gyroBias.y, gyroBias.z);
sendMessage(&msg); sendMessage(&msg);
``` ```

View File

@@ -6,7 +6,7 @@
import os import os
import time import time
from queue import Queue, Empty from queue import Queue, Empty
from typing import Literal, Optional, Callable, List, Dict, Any, Union from typing import Optional, Callable, List, Dict, Any, Union, Sequence
import logging import logging
import errno import errno
from threading import Thread, Timer from threading import Thread, Timer
@@ -17,7 +17,7 @@ from pymavlink.dialects.v20 import common as mavlink
logger = logging.getLogger('flix') logger = logging.getLogger('flix')
if not logger.hasHandlers(): if not logger.hasHandlers():
handler = logging.StreamHandler() handler = logging.StreamHandler()
handler.setFormatter(logging.Formatter('%(name)s - %(levelname)s - %(message)s')) handler.setFormatter(logging.Formatter('%(name)s: %(message)s'))
logger.addHandler(handler) logger.addHandler(handler)
logger.setLevel(logging.INFO) logger.setLevel(logging.INFO)
@@ -36,10 +36,11 @@ class Flix:
system_id: int system_id: int
messages: Dict[str, Dict[str, Any]] # MAVLink messages storage messages: Dict[str, Dict[str, Any]] # MAVLink messages storage
values: Dict[Union[str, int], Union[float, List[float]]] = {} # named values values: Dict[Union[str, int], Union[float, List[float]]] # named values
_connection_timeout = 3 _connection_timeout = 3
_print_buffer: str = '' _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):
if not (0 <= system_id < 256): if not (0 <= system_id < 256):
@@ -55,12 +56,11 @@ class Flix:
if e.errno != errno.EADDRINUSE: if e.errno != errno.EADDRINUSE:
raise raise
# Port busy - using proxy # Port busy - using proxy
logger.debug('Listening on port 14560 (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: mavutil.mavfile = mavutil.mavlink_connection('udpin:0.0.0.0:14555', source_system=254) # type: ignore
self.connection.target_system = system_id self.connection.target_system = system_id
self.mavlink: mavlink.MAVLink = self.connection.mav self.mavlink: mavlink.MAVLink = self.connection.mav
self._event_listeners: Dict[str, List[Callable[..., Any]]] = {} self._event_listeners: Dict[str, List[Callable[..., Any]]] = {}
self.messages = {}
self._disconnected_timer = Timer(0, self._disconnected) self._disconnected_timer = Timer(0, self._disconnected)
self._reader_thread = Thread(target=self._read_mavlink, daemon=True) self._reader_thread = Thread(target=self._read_mavlink, daemon=True)
self._reader_thread.start() self._reader_thread.start()
@@ -78,6 +78,8 @@ class Flix:
self.motors = [0, 0, 0, 0] self.motors = [0, 0, 0, 0]
self.acc = [0, 0, 0] self.acc = [0, 0, 0]
self.gyro = [0, 0, 0] self.gyro = [0, 0, 0]
self.messages = {}
self.values = {}
def on(self, event: str, callback: Callable): def on(self, event: str, callback: Callable):
event = event.lower() event = event.lower()
@@ -85,10 +87,15 @@ class Flix:
self._event_listeners[event] = [] self._event_listeners[event] = []
self._event_listeners[event].append(callback) self._event_listeners[event].append(callback)
def off(self, callback: Callable): def off(self, event_or_callback: Union[str, Callable]):
for event in self._event_listeners: if isinstance(event_or_callback, str):
if callback in self._event_listeners[event]: event = event_or_callback.lower()
self._event_listeners[event].remove(callback) if event in self._event_listeners:
del self._event_listeners[event]
else:
for event in self._event_listeners:
if event_or_callback in self._event_listeners[event]:
self._event_listeners[event].remove(event_or_callback)
def _trigger(self, event: str, *args): def _trigger(self, event: str, *args):
event = event.lower() event = event.lower()
@@ -147,7 +154,7 @@ class Flix:
def _handle_mavlink_message(self, msg: mavlink.MAVLink_message): def _handle_mavlink_message(self, msg: mavlink.MAVLink_message):
if isinstance(msg, mavlink.MAVLink_heartbeat_message): if isinstance(msg, mavlink.MAVLink_heartbeat_message):
self.mode = ['MANUAL', 'ACRO', 'STAB', 'USER'][msg.custom_mode] self.mode = self._modes[msg.custom_mode] if msg.custom_mode < len(self._modes) else f'UNKNOWN({msg.custom_mode})'
self.armed = msg.base_mode & mavlink.MAV_MODE_FLAG_SAFETY_ARMED != 0 self.armed = msg.base_mode & mavlink.MAV_MODE_FLAG_SAFETY_ARMED != 0
self._trigger('mode', self.mode) self._trigger('mode', self.mode)
self._trigger('armed', self.armed) self._trigger('armed', self.armed)
@@ -168,6 +175,11 @@ class Flix:
msg.chan5_raw, msg.chan6_raw, msg.chan7_raw, msg.chan8_raw] msg.chan5_raw, msg.chan6_raw, msg.chan7_raw, msg.chan8_raw]
self._trigger('channels', self.channels) self._trigger('channels', self.channels)
if isinstance(msg, mavlink.MAVLink_actuator_control_target_message):
self.motors = msg.controls[:4] # type: ignore
self._trigger('motors', self.motors)
# TODO: to be removed: the old way of passing motor outputs
if isinstance(msg, mavlink.MAVLink_actuator_output_status_message): if isinstance(msg, mavlink.MAVLink_actuator_output_status_message):
self.motors = msg.actuator[:4] # type: ignore self.motors = msg.actuator[:4] # type: ignore
self._trigger('motors', self.motors) self._trigger('motors', self.motors)
@@ -231,6 +243,19 @@ class Flix:
def _flu_to_mavlink(v: List[float]) -> List[float]: def _flu_to_mavlink(v: List[float]) -> List[float]:
return Flix._mavlink_to_flu(v) return Flix._mavlink_to_flu(v)
def _command_send(self, command: int, params: Sequence[float]):
if len(params) != 7:
raise ValueError('Command must have 7 parameters')
for attempt in range(3):
try:
logger.debug(f'Send command {command} with params {params} (attempt #{attempt + 1})')
self.mavlink.command_long_send(self.system_id, 0, command, 0, *params) # type: ignore
self.wait('mavlink.COMMAND_ACK', value=lambda msg: msg.command == command and msg.result == mavlink.MAV_RESULT_ACCEPTED, timeout=0.1)
return
except TimeoutError:
continue
raise RuntimeError(f'Failed to send command {command} after 3 attempts')
def _connected(self): def _connected(self):
# Reset disconnection timer # Reset disconnection timer
self._disconnected_timer.cancel() self._disconnected_timer.cancel()
@@ -275,6 +300,14 @@ class Flix:
continue continue
raise RuntimeError(f'Failed to set parameter {name} to {value} after 3 attempts') raise RuntimeError(f'Failed to set parameter {name} to {value} after 3 attempts')
def set_mode(self, mode: Union[str, int]):
if isinstance(mode, str):
mode = self._modes.index(mode.upper())
self._command_send(mavlink.MAV_CMD_DO_SET_MODE, (0, mode, 0, 0, 0, 0, 0))
def set_armed(self, armed: bool):
self._command_send(mavlink.MAV_CMD_COMPONENT_ARM_DISARM, (1 if armed else 0, 0, 0, 0, 0, 0, 0))
def set_position(self, position: List[float], yaw: Optional[float] = None, wait: bool = False, tolerance: float = 0.1): def set_position(self, position: List[float], yaw: Optional[float] = None, wait: bool = False, tolerance: float = 0.1):
raise NotImplementedError('Position control is not implemented yet') raise NotImplementedError('Position control is not implemented yet')
@@ -282,17 +315,37 @@ class Flix:
raise NotImplementedError('Velocity control is not implemented yet') raise NotImplementedError('Velocity control is not implemented yet')
def set_attitude(self, attitude: List[float], thrust: float): def set_attitude(self, attitude: List[float], thrust: float):
raise NotImplementedError('Automatic flight is not implemented yet') if len(attitude) == 3:
attitude = Quaternion([attitude[0], attitude[1], attitude[2]]).q # type: ignore
elif len(attitude) != 4:
raise ValueError('Attitude must be [roll, pitch, yaw] or [w, x, y, z] quaternion')
if not (0 <= thrust <= 1):
raise ValueError('Thrust must be in range [0, 1]')
attitude = self._flu_to_mavlink(attitude)
for _ in range(2): # duplicate to ensure delivery
self.mavlink.set_attitude_target_send(0, self.system_id, 0, 0,
[attitude[0], attitude[1], attitude[2], attitude[3]],
0, 0, 0, thrust)
def set_rates(self, rates: List[float], thrust: float): def set_rates(self, rates: List[float], thrust: float):
raise NotImplementedError('Automatic flight is not implemented yet') if len(rates) != 3:
raise ValueError('Rates must be [roll_rate, pitch_rate, yaw_rate]')
if not (0 <= thrust <= 1):
raise ValueError('Thrust must be in range [0, 1]')
rates = self._flu_to_mavlink(rates)
for _ in range(2): # duplicate to ensure delivery
self.mavlink.set_attitude_target_send(0, self.system_id, 0,
mavlink.ATTITUDE_TARGET_TYPEMASK_ATTITUDE_IGNORE,
[1, 0, 0, 0],
rates[0], rates[1], rates[2], thrust)
def set_motors(self, motors: List[float]): def set_motors(self, motors: List[float]):
if len(motors) != 4: if len(motors) != 4:
raise ValueError('motors must have 4 values') raise ValueError('motors must have 4 values')
if not all(0 <= m <= 1 for m in motors): if not all(0 <= m <= 1 for m in motors):
raise ValueError('motors must be in range [0, 1]') raise ValueError('motors must be in range [0, 1]')
raise NotImplementedError for _ in range(2): # duplicate to ensure delivery
self.mavlink.set_actuator_control_target_send(int(time.time() * 1000000), 0, self.system_id, 0, motors + [0] * 4) # type: ignore
def set_controls(self, roll: float, pitch: float, yaw: float, throttle: float): def set_controls(self, roll: float, pitch: float, yaw: float, throttle: float):
"""Send pilot's controls. Warning: not intended for automatic control""" """Send pilot's controls. Warning: not intended for automatic control"""
@@ -300,10 +353,7 @@ class Flix:
raise ValueError('roll, pitch, yaw must be in range [-1, 1]') raise ValueError('roll, pitch, yaw must be in range [-1, 1]')
if not 0 <= throttle <= 1: if not 0 <= throttle <= 1:
raise ValueError('throttle must be in range [0, 1]') raise ValueError('throttle must be in range [0, 1]')
self.mavlink.manual_control_send(self.system_id, roll * 1000, pitch * 1000, yaw * 1000, throttle * 1000, 0) # type: ignore self.mavlink.manual_control_send(self.system_id, int(pitch * 1000), int(roll * 1000), int(throttle * 1000), int(yaw * 1000), 0) # type: ignore
def set_mode(self, mode: Literal['MANUAL', 'ACRO', 'STAB', 'USER']):
raise NotImplementedError('Setting mode is not implemented yet')
def cli(self, cmd: str, wait_response: bool = True) -> str: def cli(self, cmd: str, wait_response: bool = True) -> str:
cmd = cmd.strip() cmd = cmd.strip()
@@ -320,7 +370,9 @@ class Flix:
self.mavlink.serial_control_send(0, 0, 0, 0, len(cmd_bytes), cmd_bytes) self.mavlink.serial_control_send(0, 0, 0, 0, len(cmd_bytes), cmd_bytes)
if not wait_response: if not wait_response:
return '' return ''
response = self.wait('print_full', timeout=0.1, value=lambda text: text.startswith(response_prefix)) timeout = 0.1
if cmd == 'log': timeout = 10 # log download may take more time
response = self.wait('print_full', timeout=timeout, value=lambda text: text.startswith(response_prefix))
return response[len(response_prefix):].strip() return response[len(response_prefix):].strip()
except TimeoutError: except TimeoutError:
continue continue

View File

@@ -24,13 +24,16 @@ def main():
if addr in TARGETS: # packet from target if addr in TARGETS: # packet from target
if source_addr is None: if source_addr is None:
continue continue
sock.sendto(data, source_addr) try:
sock.sendto(data, source_addr)
packets += 1
except: pass
else: # packet from source else: # packet from source
source_addr = addr source_addr = addr
for target in TARGETS: for target in TARGETS:
sock.sendto(data, target) sock.sendto(data, target)
packets += 1
packets += 1
print(f'\rPackets: {packets}', end='') print(f'\rPackets: {packets}', end='')
if __name__ == '__main__': if __name__ == '__main__':

View File

@@ -1,6 +1,6 @@
[project] [project]
name = "pyflix" name = "pyflix"
version = "0.5" version = "0.11"
description = "Python API for Flix drone" description = "Python API for Flix drone"
authors = [{ name="Oleg Kalachev", email="okalachev@gmail.com" }] authors = [{ name="Oleg Kalachev", email="okalachev@gmail.com" }]
license = "MIT" license = "MIT"