42 Commits

Author SHA1 Message Date
Oleg Kalachev fa848e589e Use Serial1 for sbus on all platforms 2026-05-10 01:17:00 +03:00
Oleg Kalachev bcacad7ff8 Use Serial1 for for rc on esp32-c3 2026-05-09 19:25:03 +03:00
Oleg Kalachev 3e59688818 Add esp32-c3 build to ci 2026-05-09 18:59:58 +03:00
Oleg Kalachev b62f2f9427 Rename some wifi parameters for better alphabetical sort 2026-05-09 17:55:55 +03:00
Oleg Kalachev 7dfef17165 Add Ina Tix' build
Co-authored-by: Marina Tikhomirova <Ina.tix@yandex.ru>
2026-05-09 17:49:59 +03:00
Oleg Kalachev 8c8046676b Simplify port definition in Makefile 2026-05-09 17:14:29 +03:00
Oleg Kalachev 702ec9792e Some updates in troubleshooting article 2026-05-09 15:57:25 +03:00
Oleg Kalachev 06e2047097 Make motor testing signal 0.2 instead of full power
Testing with full power is too dangerous and inconvenient.
2026-05-08 00:53:19 +03:00
Oleg Kalachev 87480476c2 Fix motors pwm frequency for esp32s3 etc in the docs 2026-05-08 00:47:29 +03:00
Oleg Kalachev 68271c508c Print firmware build date and time in sys command 2026-05-08 00:31:51 +03:00
Oleg Kalachev e81e84e7fc Some updates to docs 2026-05-07 20:15:55 +03:00
Oleg Kalachev 5f1a938d4f Fix imu rotation definition
The X axis should be pointing to the mounting holes, not pins side.
2026-05-07 19:54:16 +03:00
Oleg Kalachev bd270db493 Reduce angle drift by adding level correction to the estimator
Leverage a priori knowledge that the drone's average attitude is level.
Explanation: https://t.me/opensourcequadcopter/158.
2026-05-05 21:27:47 +03:00
Oleg Kalachev dbf24ea611 Expose lpf alpha of rate pids to parameters
Add parameters: CTL_R_RATE_D_A, CTL_P_RATE_D_A, CTL_Y_RATE_D_A.
2026-05-03 15:04:16 +03:00
Oleg Kalachev 08683d696d Some updates in the usage doc 2026-05-01 15:26:59 +03:00
Oleg Kalachev 9ca6841558 Exit auto mode when sticks moved only when mode switch is not configured 2026-04-29 15:07:44 +03:00
Oleg Kalachev 28da2d3c8e Fix in pyflix documentation
pyflix@0.14
2026-04-28 20:46:49 +03:00
Oleg Kalachev c6632ae6e4 Add info on setting flight modes using rc mode switch 2026-04-28 20:43:52 +03:00
Oleg Kalachev 35ca754583 Fix Vector::rotationVectorBetween implementation for parallel vectors 2026-04-28 15:38:52 +03:00
Oleg Kalachev 2ccda03573 Implement motors output desaturation
So the drone continues stabilization on max thrust.
2026-04-28 13:23:42 +03:00
Oleg Kalachev 485a39e740 Disable wi-fi power save to improve responsiveness 2026-04-27 16:46:36 +03:00
Oleg Kalachev 9bffe5b52f Some fixes in docs 2026-04-26 06:05:02 +03:00
Oleg Kalachev d6a79d6c66 Pass acc data in mG in SCALED_IMU to comply with mavlink standard
https://mavlink.io/en/messages/common.html#SCALED_IMU
pyflix@0.13
2026-04-24 07:42:39 +03:00
Oleg Kalachev 350a82bfed Minor fix 2026-04-23 15:34:54 +03:00
Oleg Kalachev 6e439859bc Move disabling brown-out code to power subsystem 2026-04-23 15:06:07 +03:00
Oleg Kalachev 835b2243e8 Minor fix in sys command
String works with printf %s, but actually it's a UB.
2026-04-23 07:25:59 +03:00
Oleg Kalachev ed4e2d87d1 Fix imu command output
Gyro field contained filtered gyro instead of scaled only gyro.
2026-04-23 07:12:25 +03:00
Oleg Kalachev 51cd5fc691 Implement battery voltage monitoring
Add power subsystem.
Add PWR_VOLT_PIN, PWR_VOLT_SCALE, PWR_VOLT_LPF_A parameters.
Support BATTERY_STATUS mavlink messages streaming.
Add pw cli command.
Add voltage field to pyflix library.
pyflix@0.12.
2026-04-22 11:35:37 +03:00
Oleg Kalachev d8591ea2a9 Fix working with parameters in pyflix examples
PITCH_P parameter was renamed to CTL_P_P
2026-04-18 05:23:47 +03:00
Oleg Kalachev c434107eaf Add parameter for configuring sbus pin number, disable sbus by default 2026-03-27 00:56:34 +03:00
Oleg Kalachev 814427dbfd Minor docs change 2026-03-27 00:40:19 +03:00
Oleg Kalachev 0730ceeffa Add new user builds 2026-02-21 07:12:36 +03:00
Oleg Kalachev a687303062 Make motor parameters apply without reboot
Add callback to parameter definition to call after parameter is changed.
2026-02-19 04:56:12 +03:00
Oleg Kalachev b2daf2587f Minor parameters code simplifications
readOnly is false by default
INFINITY == INFINITY, so remove redundant check
2026-02-19 02:59:38 +03:00
Oleg Kalachev a8c25d8ac0 Minor updates to usage article 2026-02-04 17:52:23 +03:00
Oleg Kalachev 3e49d41986 Make rc channel numbers and calibration params use int instead of float
As parameter subsystems supports int now, and int is much more natural here.
2026-02-02 20:36:22 +03:00
Oleg Kalachev 67430c7aac Several minor changes 2026-02-02 18:46:36 +03:00
Oleg Kalachev 3631743a29 Drop messages from another systems in pyflix
We shouldn't pass messages where system id != our system id. 
This change may be useful when there are many drones in one network.
2026-02-02 18:28:20 +03:00
Oleg Kalachev 3dde380bb7 Add parameters for list of modes bound to rc switch
Parameters: CTL_FLT_MODE_0, CTL_FLT_MODE_1, CTL_FLT_MODE_2.
Also fix a bug with incorrect choosing the mode from controlMode.
2026-01-27 16:38:20 +03:00
Oleg Kalachev 377b21429b Fix error when launching the sim
Also make the parameters WIFI_LOC_PORT and WIFI_REM_PORT work in the sim.
2026-01-27 16:32:52 +03:00
Oleg Kalachev 1ac443d6f8 Add a build by Arky Matsekh 2026-01-27 15:17:58 +03:00
Oleg Kalachev 964c0f7bc1 Make setting parameter in console printing actual parameter value.
In some cases, it would not be equal to the requested value.
2026-01-27 09:28:01 +03:00
44 changed files with 307 additions and 126 deletions
+2
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@@ -25,6 +25,8 @@ jobs:
path: flix/build path: flix/build
- name: Build firmware for ESP32-S3 - name: Build firmware for ESP32-S3
run: make BOARD=esp32:esp32:esp32s3 run: make BOARD=esp32:esp32:esp32s3
- name: Build firmware for ESP32-C3
run: make BOARD=esp32:esp32:esp32c3
- 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
+1 -2
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@@ -1,6 +1,5 @@
BOARD = esp32:esp32:d1_mini32 BOARD = esp32:esp32:d1_mini32
PORT := $(wildcard /dev/serial/by-id/usb-Silicon_Labs_CP21* /dev/serial/by-id/usb-1a86_USB_Single_Serial_* /dev/cu.usbserial-*) PORT := $(strip $(wildcard /dev/serial/by-id/usb-Silicon_Labs_CP21* /dev/serial/by-id/usb-1a86_USB_Single_Serial_* /dev/cu.usbserial-* /dev/cu.usbmodem*))
PORT := $(strip $(PORT))
build: .dependencies build: .dependencies
arduino-cli compile --fqbn $(BOARD) flix arduino-cli compile --fqbn $(BOARD) flix
+9 -5
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@@ -53,7 +53,7 @@ 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">
## Documentation ## Documentation articles
1. [Assembly instructions](docs/assembly.md). 1. [Assembly instructions](docs/assembly.md).
2. [Usage: build, setup and flight](docs/usage.md). 2. [Usage: build, setup and flight](docs/usage.md).
@@ -75,10 +75,10 @@ Additional articles:
|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| |IMU (and barometer¹) board|GY91, MPU-9265 (or other MPU9250/MPU6500 board)<br>ICM20948V2 (ICM20948)³<br>GY-521 (MPU-6050)³⁻¹|<img src="docs/img/gy-91.jpg" width=90 align=center><br><img src="docs/img/icm-20948.jpg" width=100><br><img src="docs/img/gy-521.jpg" width=100>|1|
|Boost converter (optional, for more stable power supply)|5V output|<img src="docs/img/buck-boost.jpg" width=100>|1| |Boost converter (optional, for more stable power supply)|5V output|<img src="docs/img/buck-boost.jpg" width=100>|1|
|Motor|8520 3.7V brushed motor.<br>Motor with exact 3.7V voltage is needed, not ranged working voltage (3.7V — 6V).<br>Make sure the motor shaft diameter and propeller hole diameter match!|<img src="docs/img/motor.jpeg" width=100>|4| |Motor|8520 3.7V brushed motor.<br>Motor with exact 3.7V voltage is needed, not ranged working voltage (3.7V — 6V).<br>Make sure the motor shaft diameter and propeller hole diameter match!|<img src="docs/img/motor.jpeg" width=100>|4|
|Propeller|55 mm (alternatively 65 mm)|<img src="docs/img/prop.jpg" width=100>|4| |Propeller|55 mm or 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<br>Voltage measurement resistor|10 kΩ|<img src="docs/img/resistor10k.jpg" width=100>|6|
|3.7V Li-Po battery|LW 952540 (or any compatible by the size)|<img src="docs/img/battery.jpg" width=100>|1| |3.7V Li-Po battery|LW 952540 (or any compatible by the size).<br>Make sure the battery has enough discharge rate — 25C or more!|<img src="docs/img/battery.jpg" width=100>|1|
|Battery connector cable|MX2.0 2P female|<img src="docs/img/mx.png" width=100>|1| |Battery connector cable|MX2.0 2P female|<img src="docs/img/mx.png" width=100>|1|
|Li-Po Battery charger|Any|<img src="docs/img/charger.jpg" width=100>|1| |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|
@@ -154,7 +154,11 @@ You can see a user-contributed [variant of complete circuit diagram](https://mir
|VIN|VCC (or 3.3V depending on the receiver)| |VIN|VCC (or 3.3V depending on the receiver)|
|Signal (TX)|GPIO4¹| |Signal (TX)|GPIO4¹|
*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.* *¹ — UART2 RX pin was [changed](https://docs.espressif.com/projects/arduino-esp32/en/latest/migration_guides/2.x_to_3.0.html#id14) to GPIO4 in Arduino ESP32 core 3.0.*
* Optionally connect the battery voltage divider for voltage monitoring to any ADC1 pin (e. g. *GPIO32* on ESP32, *GPIO3* on ESP32S3).
ESP32 and ESP32S3 [can measure](https://docs.espressif.com/projects/arduino-esp32/en/latest/api/adc.html#analogsetattenuation) up to 3.1 V and ESP32S3/ESP32C3 can measure up to 2.5 V, so choose the voltage divider resistors accordingly.
## Resources ## Resources
+2
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@@ -28,6 +28,8 @@ Soldered components ([schematics variant](https://miro.com/app/board/uXjVN-dTjoo
<img src="img/assembly/7.jpg" width=600> <img src="img/assembly/7.jpg" width=600>
See an alternative assembly process photos here: https://drive.google.com/drive/folders/1FG5BH9RCzdf1XmJcC70PymiRMXcz6Fx7?usp=sharing.
## Motor directions ## Motor directions
> [!WARNING] > [!WARNING]
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@@ -12,20 +12,25 @@ Do the following:
Do the following: 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. The fully charged battery should have about 4.2V.
* **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 startup output. * **Check the battery you use has enough discharge current**. The battery should be able to provide 15A of current. So the C-rating for a 1000 mAh battery should be at least 15C (higher is better).
* **Check if there are some startup errors**. Connect the ESP32 to the computer and check the Serial Monitor output. Use the Reset button or `reboot` command to see the whole startup output.
* **Check the baudrate is correct**. If you see garbage characters in the Serial Monitor, make sure the baudrate is set to 115200. * **Check the baudrate is correct**. If you see garbage characters in the Serial Monitor, make sure the baudrate is set to 115200.
* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
* **Check if the console is working**. Perform `help` command in Serial Monitor. You should see the list of available commands. You can also access the console using QGroundControl *(Vehicle Setup**Analyze Tools**MAVLink Console)*. * **Check if the console is working**. Perform `help` command in Serial Monitor. You should see the list of available commands. You can also access the console using QGroundControl *(Vehicle Setup**Analyze Tools**MAVLink Console)*.
* **Configure QGroundControl correctly before connecting to the drone** if you use it to control the drone. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**. * **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.
* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
* **Check the IMU is working**. Perform `imu` command and check its output: * **Check the IMU is working**. Perform `imu` command and check its output:
* The `status` field should be `OK`. * The `status` field should be `OK`.
* The `rate` field should be about 1000 (Hz). * The `rate` field should be about 1000 (Hz).
* The `accel` and `gyro` fields should change as you move the drone. * The `accel` and `gyro` fields should change as you move the drone.
* **Calibrate the accelerometer.** if is wasn't done before. Type `ca` command in Serial Monitor and follow the instructions.
* **Check the attitude estimation**. Connect to the drone using QGroundControl. Rotate the drone in different orientations and check if the attitude estimation shown in QGroundControl is correct.
* **Check the IMU orientation is set correctly**. If the attitude estimation is rotated, set the correct IMU orientation as described in the [tutorial](usage.md#define-imu-orientation). * **Check the IMU orientation is set correctly**. If the attitude estimation is rotated, set the correct IMU orientation as described in the [tutorial](usage.md#define-imu-orientation).
* **Calibrate the accelerometer.** if is wasn't done before. Type `ca` command in Serial Monitor and follow the instructions.
* **Check the attitude estimation**. Connect to the drone using QGroundControl. Rotate the drone in different orientations and check if the attitude estimation is shown exactly as on the video below:
<a href="https://youtu.be/yVRN23-GISU"><img width=200 src="https://i3.ytimg.com/vi/yVRN23-GISU/maxresdefault.jpg"></a>
* **Check the IMU output**. Connect to the drone using QGroundControl on your computer. Go to the *Analyze* tab, *MAVLINK Inspector*. Plot the data from the `SCALED_IMU` message. The gyroscope and accelerometer data should change according to the drone movement.
* **Check the motors type**. Motors with exact 3.7V voltage are needed, not ranged working voltage (3.7V — 6V). * **Check the motors type**. Motors with exact 3.7V voltage are needed, not ranged working voltage (3.7V — 6V).
* **Check the motors**. Perform the following commands using Serial Monitor: * **Check the motors**. Perform the following commands using Serial Monitor:
* `mfr` — should rotate front right motor (counter-clockwise). * `mfr` — should rotate front right motor (counter-clockwise).
@@ -33,7 +38,10 @@ Do the following:
* `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).
* **Check the propeller directions are correct**. Make sure your propeller types (A or B) are installed as on the picture: * **Check the propeller directions are correct**. Make sure your propeller types (A or B) are installed as on the picture:
<img src="img/user/peter_ukhov-2/1.jpg" width="200"> <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. * **If using an SBUS receiver**:
* **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. * **Define the used GPIO pin** in `RC_RX_PIN` parameter.
* **Calibrate the RC** using `cr` command in the console.
* **Check the controls** using `rc` command. All the controls should change between -1 and 1, and the throttle between 0 and 1.
+37 -24
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@@ -112,9 +112,9 @@ You can also work with parameters using `p` command in the console. Parameter na
### Define IMU orientation ### Define IMU orientation
Use parameters, to define the IMU board axes orientation relative to the drone's axes: `IMU_ROT_ROLL`, `IMU_ROT_PITCH`, and `IMU_ROT_YAW`. The IMU orientation (relative to the drone's axes) is defined using the parameters: `IMU_ROT_ROLL`, `IMU_ROT_PITCH`, and `IMU_ROT_YAW`.
The drone has *X* axis pointing forward, *Y* axis pointing left, and *Z* axis pointing up, and the supported IMU boards have *X* axis pointing to the pins side and *Z* axis pointing up from the component side: The drone has *X* axis pointing forward, *Y* axis pointing left, and *Z* axis pointing up, and the supported IMU boards have *X* axis pointing to the mounting holes side and *Z* axis pointing up from the component side:
<img src="img/imu-axes.png" width="200"> <img src="img/imu-axes.png" width="200">
@@ -122,10 +122,10 @@ Use the following table to set the parameters for common IMU orientations:
|Orientation|Parameters|Orientation|Parameters| |Orientation|Parameters|Orientation|Parameters|
|:-:|-|-|-| |:-:|-|-|-|
|<img src="img/imu-rot-1.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0 |<img src="img/imu-rot-5.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0| |<img src="img/imu-rot-3.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0 |<img src="img/imu-rot-7.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0|
|<img src="img/imu-rot-2.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|<img src="img/imu-rot-6.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571| |<img src="img/imu-rot-2.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|<img src="img/imu-rot-6.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|
|<img src="img/imu-rot-3.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|<img src="img/imu-rot-7.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142| |<img src="img/imu-rot-1.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|<img src="img/imu-rot-5.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|
|<img src="img/imu-rot-4.png" width="180"><br>☑️ **Default**|<br>`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|<img src="img/imu-rot-8.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571| |<img src="img/imu-rot-4.png" width="180"><br>☑️ **Default**|<br>`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|<img src="img/imu-rot-8.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|
### Calibrate accelerometer ### Calibrate accelerometer
@@ -138,37 +138,48 @@ Before flight you need to calibrate the accelerometer:
If using non-default motor pins, set the pin numbers using the parameters: `MOTOR_PIN_FL`, `MOTOR_PIN_FR`, `MOTOR_PIN_RL`, `MOTOR_PIN_RR` (front-left, front-right, rear-left, rear-right respectively). If using non-default motor pins, set the pin numbers using the parameters: `MOTOR_PIN_FL`, `MOTOR_PIN_FR`, `MOTOR_PIN_RL`, `MOTOR_PIN_RR` (front-left, front-right, rear-left, rear-right respectively).
Certain ESP32 models (such as ESP32-S3) support a lower maximum PWM frequency; on these boards the parameter `MOT_PWM_FREQ` should be set to 38000 Hz.
If using brushless motors and ESCs: If using brushless motors and ESCs:
1. Set the appropriate PWM using the parameters: `MOT_PWM_STOP`, `MOT_PWM_MIN`, and `MOT_PWM_MAX` (1000, 1000, and 2000 is typical). 1. Set the appropriate PWM using the parameters: `MOT_PWM_STOP`, `MOT_PWM_MIN`, and `MOT_PWM_MAX` (1000, 1000, and 2000 is typical).
2. Decrease the PWM frequency using the `MOT_PWM_FREQ` parameter (400 is typical). 2. Decrease the PWM frequency using the `MOT_PWM_FREQ` parameter (400 is typical).
Reboot the drone to apply the changes.
> [!CAUTION] > [!CAUTION]
> **Remove the props when configuring the motors!** If improperly configured, you may not be able to stop them. > **Remove the props when configuring the motors!** If improperly configured, you may not be able to stop them.
### Check everything works ### Battery voltage monitoring
1. Check the IMU is working: perform `imu` command and check its output: ESP32 ADC can measure only up to 3.3 V, so you need to use a voltage divider to monitor the battery voltage. To enable voltage measurement, set the following parameters:
1. `PWR_VOLT_PIN` — GPIO pin number where the voltage divider is connected (*-1* to disable).
2. `PWR_VOLT_SCALE` — voltage divider coefficient (*2* for two equal resistors).
After this setup, you should see the battery voltage in QGroundControl top panel or using `pw` command in the console.
### Important: check everything works
1. Check the IMU is working: perform `imu` command in the console and check the output:
* The `status` field should be `OK`. * The `status` field should be `OK`.
* The `rate` field should be about 1000 (Hz). * The `rate` field should be about 1000 (Hz).
* The `accel` and `gyro` fields should change as you move the drone. * The `accel` and `gyro` fields should change as you move the drone.
* The `accel bias` and `accel scale` fields should contain calibration parameters (not zeros and ones).
* The `gyro bias` field should contain estimated gyro bias (not zeros).
* The `landed` field should be `1` when the drone is still on the ground and `0` when you lift it up. * 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. Compare your attitude indicator (in the *large vertical* mode) to the video: 2. Check the attitude estimation: connect to the drone using QGroundControl, rotate the drone in different orientations and check if the attitude estimation shown in QGroundControl is correct. Compare your attitude indicator (in the *large vertical* mode) to the video:
<a href="https://youtu.be/yVRN23-GISU"><img width=300 src="https://i3.ytimg.com/vi/yVRN23-GISU/maxresdefault.jpg"></a> <a href="https://youtu.be/yVRN23-GISU"><img width=300 src="https://i3.ytimg.com/vi/yVRN23-GISU/maxresdefault.jpg"></a>
3. Perform motor tests in the console. Use the following commands **— remove the propellers before running the tests!** 3. Perform motor tests. Use the following commands **— remove the propellers before running the tests!**
* `mfr` — should rotate front right motor (counter-clockwise). * `mfr` — rotate front right motor (counter-clockwise).
* `mfl` — should rotate front left motor (clockwise). * `mfl` — rotate front left motor (clockwise).
* `mrl` — should rotate rear left motor (counter-clockwise). * `mrl` — rotate rear left motor (counter-clockwise).
* `mrr` — should rotate rear right motor (clockwise). * `mrr` — rotate rear right motor (clockwise).
Rotation diagram: Make sure rotation directions and propeller types match the following diagram:
<img src="img/motors.svg" width=200> <img src="img/motors.svg" width=200>
@@ -193,11 +204,13 @@ There are several ways to control the drone's flight: using **smartphone** (Wi-F
### Control with a remote control ### Control with a remote control
Before using remote SBUS-connected remote control, you need to calibrate it: Before using SBUS-connected remote control you need to enable SBUS and calibrate it:
1. Access the console using QGroundControl (recommended) or Serial Monitor. 1. Connect to the drone using QGroundControl.
2. Type `cr` command and follow the instructions. 2. In parameters, set the `RC_RX_PIN` parameter to the GPIO pin number where the SBUS signal is connected, for example: 4. Negative value disables SBUS.
3. Use the remote control to fly the drone! 3. Reboot the drone to apply changes.
4. Open the console, type `cr` command and follow the instructions to calibrate the remote control.
5. Use the remote control to fly the drone!
### Control with a USB remote control ### Control with a USB remote control
@@ -234,11 +247,11 @@ When finished flying, **disarm** the drone, moving the left stick to the bottom
### Flight modes ### Flight modes
Flight mode is changed using mode switch on the remote control or using the command line. Flight mode is changed using mode switch on the remote control (if configured) or using the console commands. The main flight mode is *STAB*. In order to change modes using SBUS remote control, set the parameters: `CTL_FLT_MODE_0`, `CTL_FLT_MODE_1`, and `CTL_FLT_MODE_2` to required mode numbers (0 for *RAW*, 1 for *ACRO*, 2 for *STAB*, 3 for *AUTO*).
#### STAB #### STAB
The default mode is *STAB*. In this mode, the drone stabilizes its attitude (orientation). The left stick controls throttle and yaw rate, the right stick controls pitch and roll angles. In this mode, the drone stabilizes its attitude (orientation). The left stick controls throttle and yaw rate, the right stick controls pitch and roll angles.
> [!IMPORTANT] > [!IMPORTANT]
> The drone doesn't stabilize its position, so slight drift is possible. The pilot should compensate it manually. > The drone doesn't stabilize its position, so slight drift is possible. The pilot should compensate it manually.
@@ -253,9 +266,9 @@ In this mode, the pilot controls the angular rates. This control method is diffi
#### AUTO #### AUTO
In this mode, the pilot inputs are ignored (except the mode switch, if configured). The drone can be controlled using [pyflix](../tools/pyflix/) Python library, or by modifying the firmware to implement the needed autonomous behavior. In this mode, the pilot inputs are ignored (except the mode switch). The drone can be controlled using [pyflix](../tools/pyflix/) Python library, or by modifying the firmware to implement the needed behavior.
If the pilot moves the control sticks, the drone will switch back to *STAB* mode. If the pilot moves the control sticks and mode switch is not configured, the drone will switch back to *STAB* mode.
## Wi-Fi configuration ## Wi-Fi configuration
+35
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@@ -4,6 +4,41 @@ This page contains user-built drones based on the Flix project. Publish your pro
--- ---
Author: [Ina Tix](https://t.me/ina_tix).<br>
Description: XR2981 based DC-DC converter, ELRS MINI 2.4GHz RX SX1280 receiver (SBUS interface), Radiomaster TX12 remote control.<br>
[Flight validation](https://drive.google.com/file/d/1yqkKNuz4R_yxGqUNQxVpixJbXqEEcUSj/view?usp=share_link).
<img src="img/user/ina_tix/1.jpg" height=200> <img src="img/user/ina_tix/2.jpg" height=200> <img src="img/user/ina_tix/3.jpg" height=200>
---
Author: [FanBy0ru](https://https://github.com/FanBy0ru).<br>
Description: custom 3D-printed frame.<br>
Frame STLs and flight validation: https://cults3d.com/en/3d-model/gadget/armature-pour-flix-drone.
<img src="img/user/fanby0ru/1.jpg" height=200> <img src="img/user/fanby0ru/2.jpg" height=200>
---
Author: Ivan44 Phalko.<br>
Description: custom PCB, cusom test bench.<br>
[Flight validation](https://drive.google.com/file/d/17DNDJ1gPmCmDRAwjedCbJ9RXAyqMqqcX/view?usp=sharing).
<img src="img/user/phalko/1.jpg" height=200> <img src="img/user/phalko/2.jpg" height=200> <img src="img/user/phalko/3.jpg" height=200>
---
Author: **Arkadiy "Arky" Matsekh**, Foucault Dynamics, Gold Coast, Australia.<br>
The drone was built for the University of Queensland industry-led Master's capstone project.
**Flight video:**
<a href="https://drive.google.com/file/d/1NNYSVXBY-w0JjCo07D8-PgnVq3ca9plj/view?usp=sharing"><img height=300 src="img/user/arkymatsekh/video.jpg"></a>
<img src="img/user/arkymatsekh/1.jpg" height=150> <img src="img/user/arkymatsekh/2.jpg" height=150> <img src="img/user/arkymatsekh/3.jpg" height=150>
---
Author: [goldarte](https://t.me/goldarte).<br> 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> <img src="img/user/goldarte/1.jpg" height=150> <img src="img/user/goldarte/2.jpg" height=150>
+7 -2
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@@ -16,6 +16,7 @@ extern float controlTime;
extern int mode; extern int mode;
extern bool armed; extern bool armed;
extern LowPassFilter<Vector> gyroBiasFilter; extern LowPassFilter<Vector> gyroBiasFilter;
extern float voltage;
const char* motd = const char* motd =
"\nWelcome to\n" "\nWelcome to\n"
@@ -39,6 +40,7 @@ const char* motd =
"disarm - disarm the drone\n" "disarm - disarm the drone\n"
"raw/stab/acro/auto - set mode\n" "raw/stab/acro/auto - set mode\n"
"rc - show RC data\n" "rc - show RC data\n"
"pw - show power info\n"
"wifi - show Wi-Fi info\n" "wifi - show Wi-Fi info\n"
"ap <ssid> <password> - setup Wi-Fi access point\n" "ap <ssid> <password> - setup Wi-Fi access point\n"
"sta <ssid> <password> - setup Wi-Fi client mode\n" "sta <ssid> <password> - setup Wi-Fi client mode\n"
@@ -94,7 +96,7 @@ void doCommand(String str, bool echo = false) {
} else if (command == "p") { } else if (command == "p") {
bool success = setParameter(arg0.c_str(), arg1.toFloat()); bool success = setParameter(arg0.c_str(), arg1.toFloat());
if (success) { if (success) {
print("%s = %g\n", arg0.c_str(), arg1.toFloat()); print("%s = %g\n", arg0.c_str(), getParameter(arg0.c_str()));
} else { } else {
print("Parameter not found: %s\n", arg0.c_str()); print("Parameter not found: %s\n", arg0.c_str());
} }
@@ -135,6 +137,8 @@ void doCommand(String str, bool echo = false) {
print("time: %.1f\n", controlTime); print("time: %.1f\n", controlTime);
print("mode: %s\n", getModeName()); print("mode: %s\n", getModeName());
print("armed: %d\n", armed); print("armed: %d\n", armed);
} else if (command == "pw") {
print("Voltage: %.1f V\n", voltage);
} else if (command == "wifi") { } else if (command == "wifi") {
printWiFiInfo(); printWiFiInfo();
} else if (command == "ap") { } else if (command == "ap") {
@@ -164,6 +168,7 @@ void doCommand(String str, bool echo = false) {
print("Chip: %s\n", ESP.getChipModel()); print("Chip: %s\n", ESP.getChipModel());
print("Temperature: %.1f °C\n", temperatureRead()); print("Temperature: %.1f °C\n", temperatureRead());
print("Free heap: %d\n", ESP.getFreeHeap()); print("Free heap: %d\n", ESP.getFreeHeap());
print("Firmware: " __DATE__ " " __TIME__ "\n");
// Print tasks table // Print tasks table
print("Num Task Stack Prio Core CPU%%\n"); print("Num Task Stack Prio Core CPU%%\n");
int taskCount = uxTaskGetNumberOfTasks(); int taskCount = uxTaskGetNumberOfTasks();
@@ -174,7 +179,7 @@ void doCommand(String str, bool echo = false) {
String core = systemState[i].xCoreID == tskNO_AFFINITY ? "*" : String(systemState[i].xCoreID); String core = systemState[i].xCoreID == tskNO_AFFINITY ? "*" : String(systemState[i].xCoreID);
int cpuPercentage = systemState[i].ulRunTimeCounter / (totalRunTime / 100); int cpuPercentage = systemState[i].ulRunTimeCounter / (totalRunTime / 100);
print("%-5d%-20s%-7d%-6d%-6s%d\n",systemState[i].xTaskNumber, systemState[i].pcTaskName, print("%-5d%-20s%-7d%-6d%-6s%d\n",systemState[i].xTaskNumber, systemState[i].pcTaskName,
systemState[i].usStackHighWaterMark, systemState[i].uxCurrentPriority, core, cpuPercentage); systemState[i].usStackHighWaterMark, systemState[i].uxCurrentPriority, core.c_str(), cpuPercentage);
} }
delete[] systemState; delete[] systemState;
#endif #endif
+17 -3
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@@ -52,6 +52,7 @@ PID pitchPID(PITCH_P, PITCH_I, PITCH_D);
PID yawPID(YAW_P, 0, 0); PID yawPID(YAW_P, 0, 0);
Vector maxRate(ROLLRATE_MAX, PITCHRATE_MAX, YAWRATE_MAX); Vector maxRate(ROLLRATE_MAX, PITCHRATE_MAX, YAWRATE_MAX);
float tiltMax = TILT_MAX; float tiltMax = TILT_MAX;
int flightModes[] = {STAB, STAB, STAB}; // map for rc mode switch
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT; extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode; extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
@@ -65,9 +66,9 @@ void control() {
} }
void interpretControls() { void interpretControls() {
if (controlMode < 0.25) mode = STAB; if (controlMode < 0.25) mode = flightModes[0];
if (controlMode < 0.75) mode = STAB; else if (controlMode <= 0.75) mode = flightModes[1];
if (controlMode > 0.75) mode = STAB; else if (controlMode > 0.75) mode = flightModes[2];
if (mode == AUTO) return; // pilot is not effective in AUTO mode if (mode == AUTO) return; // pilot is not effective in AUTO mode
@@ -148,12 +149,25 @@ void controlTorque() {
motors[MOTOR_REAR_LEFT] = thrustTarget + torqueTarget.x + torqueTarget.y - torqueTarget.z; motors[MOTOR_REAR_LEFT] = thrustTarget + torqueTarget.x + torqueTarget.y - torqueTarget.z;
motors[MOTOR_REAR_RIGHT] = thrustTarget - torqueTarget.x + torqueTarget.y + torqueTarget.z; motors[MOTOR_REAR_RIGHT] = thrustTarget - torqueTarget.x + torqueTarget.y + torqueTarget.z;
desaturate(motors[MOTOR_FRONT_LEFT], motors[MOTOR_FRONT_RIGHT], motors[MOTOR_REAR_LEFT], motors[MOTOR_REAR_RIGHT]);
motors[0] = constrain(motors[0], 0, 1); motors[0] = constrain(motors[0], 0, 1);
motors[1] = constrain(motors[1], 0, 1); motors[1] = constrain(motors[1], 0, 1);
motors[2] = constrain(motors[2], 0, 1); motors[2] = constrain(motors[2], 0, 1);
motors[3] = constrain(motors[3], 0, 1); motors[3] = constrain(motors[3], 0, 1);
} }
void desaturate(float& a, float& b, float& c, float& d) {
float maxThrust = max(max(a, b), max(c, d));
if (maxThrust > 1) {
float diff = maxThrust - 1;
a -= diff;
b -= diff;
c -= diff;
d -= diff;
}
}
const char* getModeName() { const char* getModeName() {
switch (mode) { switch (mode) {
case RAW: return "RAW"; case RAW: return "RAW";
+12 -1
View File
@@ -1,7 +1,7 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com> // Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix // Repository: https://github.com/okalachev/flix
// Attitude estimation from gyro and accelerometer // Attitude estimation using gyro and accelerometer
#include "quaternion.h" #include "quaternion.h"
#include "vector.h" #include "vector.h"
@@ -13,11 +13,13 @@ Quaternion attitude; // estimated attitude
bool landed; bool landed;
float accWeight = 0.003; float accWeight = 0.003;
float levelWeight = 0.0002;
LowPassFilter<Vector> ratesFilter(0.2); // cutoff frequency ~ 40 Hz LowPassFilter<Vector> ratesFilter(0.2); // cutoff frequency ~ 40 Hz
void estimate() { void estimate() {
applyGyro(); applyGyro();
applyAcc(); applyAcc();
applyLevel();
} }
void applyGyro() { void applyGyro() {
@@ -42,3 +44,12 @@ void applyAcc() {
// apply correction // apply correction
attitude = Quaternion::rotate(attitude, Quaternion::fromRotationVector(correction)); attitude = Quaternion::rotate(attitude, Quaternion::fromRotationVector(correction));
} }
void applyLevel() {
if (landed) return;
// assume the pilot keeps the drone more or less level in flight
Vector up = Quaternion::rotateVector(Vector(0, 0, 1), attitude);
Vector correction = Vector::rotationVectorBetween(Vector(0, 0, 1), up) * levelWeight;
attitude = Quaternion::rotate(attitude, Quaternion::fromRotationVector(correction));
}
+3 -2
View File
@@ -18,11 +18,11 @@ extern float motors[4];
void setup() { void setup() {
Serial.begin(115200); Serial.begin(115200);
print("Initializing flix\n"); print("Initializing flix\n");
disableBrownOut();
setupParameters(); setupParameters();
setupPower();
setupLED(); setupLED();
setupMotors();
setLED(true); setLED(true);
setupMotors();
setupWiFi(); setupWiFi();
setupIMU(); setupIMU();
setupRC(); setupRC();
@@ -39,6 +39,7 @@ void loop() {
sendMotors(); sendMotors();
handleInput(); handleInput();
processMavlink(); processMavlink();
readVoltage();
logData(); logData();
syncParameters(); syncParameters();
} }
+2 -2
View File
@@ -10,7 +10,7 @@
#include "util.h" #include "util.h"
MPU9250 imu(SPI); MPU9250 imu(SPI);
Vector imuRotation(0, 0, -PI / 2); // imu orientation as Euler angles Vector imuRotation(0, 0, PI / 2); // imu orientation as Euler angles
Vector gyro; // gyroscope output, rad/s Vector gyro; // gyroscope output, rad/s
Vector gyroBias; Vector gyroBias;
@@ -121,7 +121,7 @@ void printIMUInfo() {
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("rate: %.0f\n", loopRate);
print("gyro: %f %f %f\n", rates.x, rates.y, rates.z); print("gyro: %f %f %f\n", gyro.x, gyro.y, gyro.z);
print("acc: %f %f %f\n", acc.x, acc.y, acc.z); print("acc: %f %f %f\n", acc.x, acc.y, acc.z);
imu.waitForData(); imu.waitForData();
Vector rawGyro, rawAcc; Vector rawGyro, rawAcc;
+14 -5
View File
@@ -7,13 +7,15 @@
#include "util.h" #include "util.h"
extern float controlTime; extern float controlTime;
extern float voltage;
bool mavlinkConnected = false;
String mavlinkPrintBuffer;
int mavlinkSysId = 1; int mavlinkSysId = 1;
Rate telemetryFast(10); Rate telemetryFast(10);
Rate telemetrySlow(2); Rate telemetrySlow(2);
bool mavlinkConnected = false;
String mavlinkPrintBuffer;
void processMavlink() { void processMavlink() {
sendMavlink(); sendMavlink();
receiveMavlink(); receiveMavlink();
@@ -38,12 +40,19 @@ void sendMavlink() {
mavlink_msg_extended_sys_state_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, mavlink_msg_extended_sys_state_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
MAV_VTOL_STATE_UNDEFINED, landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR); MAV_VTOL_STATE_UNDEFINED, landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR);
sendMessage(&msg); sendMessage(&msg);
uint16_t voltages[] = {voltage * 1000, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX};
uint16_t voltagesExt[] = {0, 0, 0, 0};
float remaining = constrain(mapf(voltage, 3.4, 4.2, 0, 1), 0, 1);
mavlink_msg_battery_status_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, 0, MAV_BATTERY_FUNCTION_ALL,
MAV_BATTERY_TYPE_LIPO, INT16_MAX, voltages, -1, -1, -1, remaining * 100, 0, MAV_BATTERY_CHARGE_STATE_OK, voltagesExt, 0, 0);
sendMessage(&msg);
} }
if (telemetryFast && mavlinkConnected) { if (telemetryFast && mavlinkConnected) {
const float zeroQuat[] = {0, 0, 0, 0}; const float offset[] = {0, 0, 0, 0};
mavlink_msg_attitude_quaternion_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, mavlink_msg_attitude_quaternion_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
time, attitude.w, attitude.x, -attitude.y, -attitude.z, rates.x, -rates.y, -rates.z, zeroQuat); // convert to frd time, attitude.w, attitude.x, -attitude.y, -attitude.z, rates.x, -rates.y, -rates.z, offset); // convert to frd
sendMessage(&msg); sendMessage(&msg);
mavlink_msg_rc_channels_raw_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, controlTime * 1000, 0, mavlink_msg_rc_channels_raw_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, controlTime * 1000, 0,
@@ -56,7 +65,7 @@ void sendMavlink() {
sendMessage(&msg); sendMessage(&msg);
mavlink_msg_scaled_imu_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, time, mavlink_msg_scaled_imu_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, time,
acc.x * 1000, -acc.y * 1000, -acc.z * 1000, // convert to frd acc.x / ONE_G * 1000, -acc.y / ONE_G * 1000, -acc.z / ONE_G * 1000, // convert to frd
gyro.x * 1000, -gyro.y * 1000, -gyro.z * 1000, gyro.x * 1000, -gyro.y * 1000, -gyro.z * 1000,
0, 0, 0, 0); 0, 0, 0, 0);
sendMessage(&msg); sendMessage(&msg);
+2 -1
View File
@@ -24,6 +24,7 @@ void setupMotors() {
// configure pins // configure pins
for (int i = 0; i < 4; i++) { for (int i = 0; i < 4; i++) {
ledcAttach(motorPins[i], pwmFrequency, pwmResolution); ledcAttach(motorPins[i], pwmFrequency, pwmResolution);
pwmFrequency = ledcChangeFrequency(motorPins[i], pwmFrequency, pwmResolution); // when reconfiguring
} }
sendMotors(); sendMotors();
print("Motors initialized\n"); print("Motors initialized\n");
@@ -53,7 +54,7 @@ bool motorsActive() {
void testMotor(int n) { void testMotor(int n) {
print("Testing motor %d\n", n); print("Testing motor %d\n", n);
motors[n] = 1; motors[n] = 0.2;
delay(50); // ESP32 may need to wait until the end of the current cycle to change duty https://github.com/espressif/arduino-esp32/issues/5306 delay(50); // ESP32 may need to wait until the end of the current cycle to change duty https://github.com/espressif/arduino-esp32/issues/5306
sendMotors(); sendMotors();
pause(3); pause(3);
+36 -18
View File
@@ -6,21 +6,26 @@
#include <Preferences.h> #include <Preferences.h>
#include "util.h" #include "util.h"
extern float channelZero[16]; extern int channelZero[16];
extern float channelMax[16]; extern int channelMax[16];
extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel; extern int rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
extern int rcRxPin;
extern int wifiMode, udpLocalPort, udpRemotePort; extern int wifiMode, udpLocalPort, udpRemotePort;
extern float rcLossTimeout, descendTime; extern float rcLossTimeout, descendTime;
extern int voltagePin;
extern float voltageScale;
extern LowPassFilter<float> voltageFilter;
Preferences storage; Preferences storage;
struct Parameter { struct Parameter {
const char *name; // max length is 15 (Preferences key limit) const char *name; // max length is 15
bool integer; bool integer;
union { float *f; int *i; }; // pointer to variable union { float *f; int *i; }; // pointer to the variable
float cache; // what's stored in flash float cache; // what's stored in flash
Parameter(const char *name, float *variable) : name(name), integer(false), f(variable) {}; void (*callback)(); // called after parameter change
Parameter(const char *name, int *variable) : name(name), integer(true), i(variable) {}; Parameter(const char *name, float *variable, void (*callback)() = nullptr) : name(name), integer(false), f(variable), callback(callback) {};
Parameter(const char *name, int *variable, void (*callback)() = nullptr) : name(name), integer(true), i(variable), callback(callback) {};
float getValue() const { return integer ? *i : *f; }; float getValue() const { return integer ? *i : *f; };
void setValue(const float value) { if (integer) *i = value; else *f = value; }; void setValue(const float value) { if (integer) *i = value; else *f = value; };
}; };
@@ -31,13 +36,16 @@ Parameter parameters[] = {
{"CTL_R_RATE_I", &rollRatePID.i}, {"CTL_R_RATE_I", &rollRatePID.i},
{"CTL_R_RATE_D", &rollRatePID.d}, {"CTL_R_RATE_D", &rollRatePID.d},
{"CTL_R_RATE_WU", &rollRatePID.windup}, {"CTL_R_RATE_WU", &rollRatePID.windup},
{"CTL_R_RATE_D_A", &rollRatePID.lpf.alpha},
{"CTL_P_RATE_P", &pitchRatePID.p}, {"CTL_P_RATE_P", &pitchRatePID.p},
{"CTL_P_RATE_I", &pitchRatePID.i}, {"CTL_P_RATE_I", &pitchRatePID.i},
{"CTL_P_RATE_D", &pitchRatePID.d}, {"CTL_P_RATE_D", &pitchRatePID.d},
{"CTL_P_RATE_WU", &pitchRatePID.windup}, {"CTL_P_RATE_WU", &pitchRatePID.windup},
{"CTL_P_RATE_D_A", &pitchRatePID.lpf.alpha},
{"CTL_Y_RATE_P", &yawRatePID.p}, {"CTL_Y_RATE_P", &yawRatePID.p},
{"CTL_Y_RATE_I", &yawRatePID.i}, {"CTL_Y_RATE_I", &yawRatePID.i},
{"CTL_Y_RATE_D", &yawRatePID.d}, {"CTL_Y_RATE_D", &yawRatePID.d},
{"CTL_Y_RATE_D_A", &yawRatePID.lpf.alpha},
{"CTL_R_P", &rollPID.p}, {"CTL_R_P", &rollPID.p},
{"CTL_R_I", &rollPID.i}, {"CTL_R_I", &rollPID.i},
{"CTL_R_D", &rollPID.d}, {"CTL_R_D", &rollPID.d},
@@ -49,6 +57,9 @@ Parameter parameters[] = {
{"CTL_R_RATE_MAX", &maxRate.x}, {"CTL_R_RATE_MAX", &maxRate.x},
{"CTL_Y_RATE_MAX", &maxRate.z}, {"CTL_Y_RATE_MAX", &maxRate.z},
{"CTL_TILT_MAX", &tiltMax}, {"CTL_TILT_MAX", &tiltMax},
{"CTL_FLT_MODE_0", &flightModes[0]},
{"CTL_FLT_MODE_1", &flightModes[1]},
{"CTL_FLT_MODE_2", &flightModes[2]},
// imu // imu
{"IMU_ROT_ROLL", &imuRotation.x}, {"IMU_ROT_ROLL", &imuRotation.x},
{"IMU_ROT_PITCH", &imuRotation.y}, {"IMU_ROT_PITCH", &imuRotation.y},
@@ -62,18 +73,20 @@ Parameter parameters[] = {
{"IMU_GYRO_BIAS_A", &gyroBiasFilter.alpha}, {"IMU_GYRO_BIAS_A", &gyroBiasFilter.alpha},
// estimate // estimate
{"EST_ACC_WEIGHT", &accWeight}, {"EST_ACC_WEIGHT", &accWeight},
{"EST_LVL_WEIGHT", &levelWeight},
{"EST_RATES_LPF_A", &ratesFilter.alpha}, {"EST_RATES_LPF_A", &ratesFilter.alpha},
// motors // motors
{"MOT_PIN_FL", &motorPins[MOTOR_FRONT_LEFT]}, {"MOT_PIN_FL", &motorPins[MOTOR_FRONT_LEFT], setupMotors},
{"MOT_PIN_FR", &motorPins[MOTOR_FRONT_RIGHT]}, {"MOT_PIN_FR", &motorPins[MOTOR_FRONT_RIGHT], setupMotors},
{"MOT_PIN_RL", &motorPins[MOTOR_REAR_LEFT]}, {"MOT_PIN_RL", &motorPins[MOTOR_REAR_LEFT], setupMotors},
{"MOT_PIN_RR", &motorPins[MOTOR_REAR_RIGHT]}, {"MOT_PIN_RR", &motorPins[MOTOR_REAR_RIGHT], setupMotors},
{"MOT_PWM_FREQ", &pwmFrequency}, {"MOT_PWM_FREQ", &pwmFrequency, setupMotors},
{"MOT_PWM_RES", &pwmResolution}, {"MOT_PWM_RES", &pwmResolution, setupMotors},
{"MOT_PWM_STOP", &pwmStop}, {"MOT_PWM_STOP", &pwmStop},
{"MOT_PWM_MIN", &pwmMin}, {"MOT_PWM_MIN", &pwmMin},
{"MOT_PWM_MAX", &pwmMax}, {"MOT_PWM_MAX", &pwmMax},
// rc // rc
{"RC_RX_PIN", &rcRxPin},
{"RC_ZERO_0", &channelZero[0]}, {"RC_ZERO_0", &channelZero[0]},
{"RC_ZERO_1", &channelZero[1]}, {"RC_ZERO_1", &channelZero[1]},
{"RC_ZERO_2", &channelZero[2]}, {"RC_ZERO_2", &channelZero[2]},
@@ -97,19 +110,24 @@ Parameter parameters[] = {
{"RC_MODE", &modeChannel}, {"RC_MODE", &modeChannel},
// wifi // wifi
{"WIFI_MODE", &wifiMode}, {"WIFI_MODE", &wifiMode},
{"WIFI_LOC_PORT", &udpLocalPort}, {"WIFI_PORT_LOC", &udpLocalPort},
{"WIFI_REM_PORT", &udpRemotePort}, {"WIFI_PORT_REM", &udpRemotePort},
// mavlink // mavlink
{"MAV_SYS_ID", &mavlinkSysId}, {"MAV_SYS_ID", &mavlinkSysId},
{"MAV_RATE_SLOW", &telemetrySlow.rate}, {"MAV_RATE_SLOW", &telemetrySlow.rate},
{"MAV_RATE_FAST", &telemetryFast.rate}, {"MAV_RATE_FAST", &telemetryFast.rate},
// power
{"PWR_VOLT_PIN", &voltagePin},
{"PWR_VOLT_SCALE", &voltageScale},
{"PWR_VOLT_LPF_A", &voltageFilter.alpha},
// safety // safety
{"SF_RC_LOSS_TIME", &rcLossTimeout}, {"SF_RC_LOSS_TIME", &rcLossTimeout},
{"SF_DESCEND_TIME", &descendTime}, {"SF_DESCEND_TIME", &descendTime},
}; };
void setupParameters() { void setupParameters() {
storage.begin("flix", false); print("Setup parameters\n");
storage.begin("flix");
// Read parameters from storage // Read parameters from storage
for (auto &parameter : parameters) { for (auto &parameter : parameters) {
if (!storage.isKey(parameter.name)) { if (!storage.isKey(parameter.name)) {
@@ -148,6 +166,7 @@ bool setParameter(const char *name, const float value) {
if (strcasecmp(parameter.name, name) == 0) { if (strcasecmp(parameter.name, name) == 0) {
if (parameter.integer && !isfinite(value)) return false; // can't set integer to NaN or Inf if (parameter.integer && !isfinite(value)) return false; // can't set integer to NaN or Inf
parameter.setValue(value); parameter.setValue(value);
if (parameter.callback) parameter.callback();
return true; return true;
} }
} }
@@ -161,8 +180,7 @@ void syncParameters() {
for (auto &parameter : parameters) { for (auto &parameter : parameters) {
if (parameter.getValue() == parameter.cache) continue; // no change if (parameter.getValue() == parameter.cache) continue; // no change
if (isnan(parameter.getValue()) && isnan(parameter.cache)) continue; // both are NaN if (isnan(parameter.getValue()) && isnan(parameter.cache)) continue; // both are NAN
if (isinf(parameter.getValue()) && isinf(parameter.cache)) continue; // both are Inf
storage.putFloat(parameter.name, parameter.getValue()); storage.putFloat(parameter.name, parameter.getValue());
parameter.cache = parameter.getValue(); // update cache parameter.cache = parameter.getValue(); // update cache
+28
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@@ -0,0 +1,28 @@
// Copyright (c) 2026 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Power management
#include <soc/soc.h>
#include <soc/rtc_cntl_reg.h>
#include "lpf.h"
#include "util.h"
float voltage;
LowPassFilter<float> voltageFilter(0.2);
int voltagePin = -1;
float voltageScale = 2;
void setupPower() {
// Disable reset on low voltage
REG_CLR_BIT(RTC_CNTL_BROWN_OUT_REG, RTC_CNTL_BROWN_OUT_ENA);
}
void readVoltage() {
if (voltagePin < 0) return;
static Rate rate(10);
if (!rate) return;
float v = analogReadMilliVolts(voltagePin) * voltageScale / 1000.0f;
voltage = voltageFilter.update(v);
}
+24 -18
View File
@@ -6,25 +6,27 @@
#include <SBUS.h> #include <SBUS.h>
#include "util.h" #include "util.h"
SBUS rc(Serial2); SBUS rc(Serial1);
int rcRxPin = -1; // -1 means disabled
uint16_t channels[16]; // raw rc channels uint16_t channels[16]; // raw rc channels
float channelZero[16]; // calibration zero values int channelZero[16]; // calibration zero values
float channelMax[16]; // calibration max values int channelMax[16]; // calibration max values
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1] float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
float controlMode = NAN; float controlMode = NAN;
float controlTime = NAN; // time of the last controls update float controlTime = NAN; // time of the last controls update
// Channels mapping (nan means not assigned): int rollChannel = -1, pitchChannel = -1, throttleChannel = -1, yawChannel = -1, modeChannel = -1; // channel mapping
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
void setupRC() { void setupRC() {
if (rcRxPin < 0) return;
print("Setup RC\n"); print("Setup RC\n");
rc.begin(); rc.begin(rcRxPin);
} }
bool readRC() { bool readRC() {
if (rcRxPin < 0) return false;
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
@@ -41,14 +43,18 @@ void normalizeRC() {
controls[i] = mapf(channels[i], channelZero[i], channelMax[i], 0, 1); controls[i] = mapf(channels[i], channelZero[i], channelMax[i], 0, 1);
} }
// Update control values // Update control values
controlRoll = rollChannel >= 0 ? controls[(int)rollChannel] : 0; controlRoll = rollChannel < 0 ? 0 : controls[rollChannel];
controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : 0; controlPitch = pitchChannel < 0 ? 0 : controls[pitchChannel];
controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : 0; controlYaw = yawChannel < 0 ? 0 : controls[yawChannel];
controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : 0; controlThrottle = throttleChannel < 0 ? 0 : controls[throttleChannel];
controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN; // mode switch should not have affect if not set controlMode = modeChannel < 0 ? NAN : controls[modeChannel]; // mode control is ineffective if not mapped
} }
void calibrateRC() { void calibrateRC() {
if (rcRxPin < 0) {
print("RC_RX_PIN = %d, set the RC pin!\n", rcRxPin);
return;
}
uint16_t zero[16]; uint16_t zero[16];
uint16_t center[16]; uint16_t center[16];
uint16_t max[16]; uint16_t max[16];
@@ -64,7 +70,7 @@ void calibrateRC() {
printRCCalibration(); printRCCalibration();
} }
void calibrateRCChannel(float *channel, uint16_t in[16], uint16_t out[16], const char *str) { void calibrateRCChannel(int *channel, uint16_t in[16], uint16_t out[16], const char *str) {
print("%s", str); print("%s", str);
pause(3); pause(3);
for (int i = 0; i < 30; i++) readRC(); // try update 30 times max for (int i = 0; i < 30; i++) readRC(); // try update 30 times max
@@ -85,15 +91,15 @@ void calibrateRCChannel(float *channel, uint16_t in[16], uint16_t out[16], const
channelZero[ch] = in[ch]; channelZero[ch] = in[ch];
channelMax[ch] = out[ch]; channelMax[ch] = out[ch];
} else { } else {
*channel = NAN; *channel = -1;
} }
} }
void printRCCalibration() { void printRCCalibration() {
print("Control Ch Zero Max\n"); print("Control Ch Zero Max\n");
print("Roll %-7g%-7g%-7g\n", rollChannel, rollChannel >= 0 ? channelZero[(int)rollChannel] : NAN, rollChannel >= 0 ? channelMax[(int)rollChannel] : NAN); print("Roll %-7d%-7d%-7d\n", rollChannel, rollChannel < 0 ? 0 : channelZero[rollChannel], rollChannel < 0 ? 0 : channelMax[rollChannel]);
print("Pitch %-7g%-7g%-7g\n", pitchChannel, pitchChannel >= 0 ? channelZero[(int)pitchChannel] : NAN, pitchChannel >= 0 ? channelMax[(int)pitchChannel] : NAN); print("Pitch %-7d%-7d%-7d\n", pitchChannel, pitchChannel < 0 ? 0 : channelZero[pitchChannel], pitchChannel < 0 ? 0 : channelMax[pitchChannel]);
print("Yaw %-7g%-7g%-7g\n", yawChannel, yawChannel >= 0 ? channelZero[(int)yawChannel] : NAN, yawChannel >= 0 ? channelMax[(int)yawChannel] : NAN); print("Yaw %-7d%-7d%-7d\n", yawChannel, yawChannel < 0 ? 0 : channelZero[yawChannel], yawChannel < 0 ? 0 : channelMax[yawChannel]);
print("Throttle %-7g%-7g%-7g\n", throttleChannel, throttleChannel >= 0 ? channelZero[(int)throttleChannel] : NAN, throttleChannel >= 0 ? channelMax[(int)throttleChannel] : NAN); print("Throttle %-7d%-7d%-7d\n", throttleChannel, throttleChannel < 0 ? 0 : channelZero[throttleChannel], throttleChannel < 0 ? 0 : channelMax[throttleChannel]);
print("Mode %-7g%-7g%-7g\n", modeChannel, modeChannel >= 0 ? channelZero[(int)modeChannel] : NAN, modeChannel >= 0 ? channelMax[(int)modeChannel] : NAN); print("Mode %-7d%-7d%-7d\n", modeChannel, modeChannel < 0 ? 0 : channelZero[modeChannel], modeChannel < 0 ? 0 : channelMax[modeChannel]);
} }
+2 -2
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@@ -37,8 +37,8 @@ void descend() {
void autoFailsafe() { void autoFailsafe() {
static float roll, pitch, yaw, throttle; static float roll, pitch, yaw, throttle;
if (roll != controlRoll || pitch != controlPitch || yaw != controlYaw || abs(throttle - controlThrottle) > 0.05) { if (roll != controlRoll || pitch != controlPitch || yaw != controlYaw || abs(throttle - controlThrottle) > 0.05) {
// controls changed // controls changed and mode switch is not configured
if (mode == AUTO) mode = STAB; // regain control by the pilot if (mode == AUTO && invalid(controlMode)) mode = STAB; // regain control by the pilot
} }
roll = controlRoll; roll = controlRoll;
pitch = controlPitch; pitch = controlPitch;
-7
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@@ -6,8 +6,6 @@
#pragma once #pragma once
#include <math.h> #include <math.h>
#include <soc/soc.h>
#include <soc/rtc_cntl_reg.h>
const float ONE_G = 9.80665; const float ONE_G = 9.80665;
extern float t; extern float t;
@@ -35,11 +33,6 @@ float wrapAngle(float angle) {
return angle; return angle;
} }
// Disable reset on low voltage
void disableBrownOut() {
REG_CLR_BIT(RTC_CNTL_BROWN_OUT_REG, RTC_CNTL_BROWN_OUT_ENA);
}
// Trim and split string by spaces // Trim and split string by spaces
void splitString(String& str, String& token0, String& token1, String& token2) { void splitString(String& str, String& token0, String& token1, String& token2) {
str.trim(); str.trim();
+16 -3
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@@ -105,10 +105,23 @@ public:
} }
static Vector rotationVectorBetween(const Vector& a, const Vector& b) { static Vector rotationVectorBetween(const Vector& a, const Vector& b) {
float an = a.norm();
float bn = b.norm();
if (an < 1e-6 || bn < 1e-6) {
return Vector(0, 0, 0);
}
Vector direction = cross(a, b); Vector direction = cross(a, b);
if (direction.zero()) { if (direction.norm() < 1e-6) { // vectors are parallel
// vectors are opposite, return any perpendicular vector if (dot(a, b) > 0) { // same direction
return cross(a, Vector(1, 0, 0)); return Vector(0, 0, 0);
}
// opposite direction
Vector perp = cross(a, Vector(1, 0, 0));
if (perp.norm() < 1e-6) {
perp = cross(a, Vector(0, 1, 0));
}
perp.normalize();
return perp * PI;
} }
direction.normalize(); direction.normalize();
float angle = angleBetween(a, b); float angle = angleBetween(a, b);
+1
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@@ -25,6 +25,7 @@ void setupWiFi() {
} else if (wifiMode == W_STA) { } else if (wifiMode == W_STA) {
WiFi.begin(storage.getString("WIFI_STA_SSID", "").c_str(), storage.getString("WIFI_STA_PASS", "").c_str()); WiFi.begin(storage.getString("WIFI_STA_SSID", "").c_str(), storage.getString("WIFI_STA_PASS", "").c_str());
} }
WiFi.setSleep(false); // disable power save
udp.begin(udpLocalPort); udp.begin(udpLocalPort);
} }
+5 -1
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@@ -21,6 +21,8 @@
#define degrees(rad) ((rad)*RAD_TO_DEG) #define degrees(rad) ((rad)*RAD_TO_DEG)
#define constrain(amt,low,high) ((amt)<(low)?(low):((amt)>(high)?(high):(amt))) #define constrain(amt,low,high) ((amt)<(low)?(low):((amt)>(high)?(high):(amt)))
template<typename T> T max(T a, T b) { return a > b ? a : b; }
template<typename T> T min(T a, T b) { return a < b ? a : b; }
long map(long x, long in_min, long in_max, long out_min, long out_max) { long map(long x, long in_min, long in_max, long out_min, long out_max) {
const long run = in_max - in_min; const long run = in_max - in_min;
@@ -149,7 +151,7 @@ public:
void setRxInvert(bool invert) {}; void setRxInvert(bool invert) {};
}; };
HardwareSerial Serial, Serial2; HardwareSerial Serial, Serial1, Serial2;
class EspClass { class EspClass {
public: public:
@@ -165,6 +167,8 @@ void delay(uint32_t ms) {
bool ledcAttach(uint8_t pin, uint32_t freq, uint8_t resolution) { return true; } bool ledcAttach(uint8_t pin, uint32_t freq, uint8_t resolution) { return true; }
bool ledcWrite(uint8_t pin, uint32_t duty) { return true; } bool ledcWrite(uint8_t pin, uint32_t duty) { return true; }
uint32_t ledcChangeFrequency(uint8_t pin, uint32_t freq, uint8_t resolution) { return freq; }
uint32_t analogReadMilliVolts(uint8_t pin) { return 0; }
unsigned long __micros; unsigned long __micros;
unsigned long __resetTime = 0; unsigned long __resetTime = 0;
+1 -1
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@@ -13,7 +13,7 @@ class SBUS {
public: public:
SBUS(HardwareSerial& bus, const bool inv = true) {}; SBUS(HardwareSerial& bus, const bool inv = true) {};
SBUS(HardwareSerial& bus, const int8_t rxpin, const int8_t txpin, const bool inv = true) {}; SBUS(HardwareSerial& bus, const int8_t rxpin, const int8_t txpin, const bool inv = true) {};
void begin() {}; void begin(int rxpin = -1, int txpin = -1, bool inv = true, bool fast = false) {};
bool read() { return joystickInit(); }; bool read() { return joystickInit(); };
SBUSData data() { SBUSData data() {
SBUSData data; SBUSData data;
+5 -1
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@@ -9,6 +9,7 @@
#include "quaternion.h" #include "quaternion.h"
#include "Arduino.h" #include "Arduino.h"
#include "wifi.h" #include "wifi.h"
#include "lpf.h"
extern float t, dt; extern float t, dt;
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode; extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
@@ -19,17 +20,20 @@ extern float motors[4];
Vector gyro, acc, imuRotation; Vector gyro, acc, imuRotation;
Vector accBias, gyroBias, accScale(1, 1, 1); Vector accBias, gyroBias, accScale(1, 1, 1);
LowPassFilter<Vector> gyroBiasFilter(0);
// declarations // declarations
void step(); void step();
void computeLoopRate(); void computeLoopRate();
void applyGyro(); void applyGyro();
void applyAcc(); void applyAcc();
void applyLevel();
void control(); void control();
void interpretControls(); void interpretControls();
void controlAttitude(); void controlAttitude();
void controlRates(); void controlRates();
void controlTorque(); void controlTorque();
void desaturate(float& a, float& b, float& c, float& d);
const char* getModeName(); const char* getModeName();
void sendMotors(); void sendMotors();
int getDutyCycle(float value); int getDutyCycle(float value);
@@ -41,7 +45,7 @@ void doCommand(String str, bool echo);
void handleInput(); void handleInput();
void normalizeRC(); void normalizeRC();
void calibrateRC(); void calibrateRC();
void calibrateRCChannel(float *channel, uint16_t zero[16], uint16_t max[16], const char *str); void calibrateRCChannel(int *channel, uint16_t zero[16], uint16_t max[16], const char *str);
void printRCCalibration(); void printRCCalibration();
void printLogHeader(); void printLogHeader();
void printLogData(); void printLogData();
+1
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@@ -27,6 +27,7 @@
#include "mavlink.ino" #include "mavlink.ino"
#include "motors.ino" #include "motors.ino"
#include "parameters.ino" #include "parameters.ino"
#include "power.ino"
#include "rc.ino" #include "rc.ino"
#include "time.ino" #include "time.ino"
-1
View File
@@ -1,4 +1,3 @@
// Dummy file to make it possible to compile simulator with Flix' util.h // Dummy file to make it possible to compile simulator with Flix' util.h
#define WRITE_PERI_REG(addr, val) {}
#define REG_CLR_BIT(_r, _b) {} #define REG_CLR_BIT(_r, _b) {}
+9 -8
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@@ -11,9 +11,10 @@
#include <sys/poll.h> #include <sys/poll.h>
#include <gazebo/gazebo.hh> #include <gazebo/gazebo.hh>
#define WIFI_UDP_PORT 14580 int wifiMode = 1; // mock
#define WIFI_UDP_REMOTE_PORT 14550 int udpLocalPort = 14580;
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255" int udpRemotePort = 14550;
const char *udpRemoteIP = "255.255.255.255";
int wifiSocket; int wifiSocket;
@@ -22,22 +23,22 @@ void setupWiFi() {
sockaddr_in addr; // local address sockaddr_in addr; // local address
addr.sin_family = AF_INET; addr.sin_family = AF_INET;
addr.sin_addr.s_addr = INADDR_ANY; addr.sin_addr.s_addr = INADDR_ANY;
addr.sin_port = htons(WIFI_UDP_PORT); addr.sin_port = htons(udpLocalPort);
if (bind(wifiSocket, (sockaddr *)&addr, sizeof(addr))) { if (bind(wifiSocket, (sockaddr *)&addr, sizeof(addr))) {
gzerr << "Failed to bind WiFi UDP socket on port " << WIFI_UDP_PORT << std::endl; gzerr << "Failed to bind WiFi UDP socket on port " << udpLocalPort << std::endl;
return; return;
} }
int broadcast = 1; int broadcast = 1;
setsockopt(wifiSocket, SOL_SOCKET, SO_BROADCAST, &broadcast, sizeof(broadcast)); // enable broadcast setsockopt(wifiSocket, SOL_SOCKET, SO_BROADCAST, &broadcast, sizeof(broadcast)); // enable broadcast
gzmsg << "WiFi UDP socket initialized on port " << WIFI_UDP_PORT << " (remote port " << WIFI_UDP_REMOTE_PORT << ")" << std::endl; gzmsg << "WiFi UDP socket initialized on port " << udpLocalPort << " (remote port " << udpRemotePort << ")" << std::endl;
} }
void sendWiFi(const uint8_t *buf, int len) { 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 = inet_addr(WIFI_UDP_REMOTE_ADDR); addr.sin_addr.s_addr = inet_addr(udpRemoteIP);
addr.sin_port = htons(WIFI_UDP_REMOTE_PORT); addr.sin_port = htons(udpRemotePort);
sendto(wifiSocket, buf, len, 0, (sockaddr *)&addr, sizeof(addr)); sendto(wifiSocket, buf, len, 0, (sockaddr *)&addr, sizeof(addr));
} }
+4 -3
View File
@@ -10,6 +10,7 @@ print('Connected:', flix.connected)
print('Mode:', flix.mode) print('Mode:', flix.mode)
print('Armed:', flix.armed) print('Armed:', flix.armed)
print('Landed:', flix.landed) print('Landed:', flix.landed)
print('Voltage:', flix.voltage, 'V')
print('Rates:', *[f'{math.degrees(r):.0f}°/s' for r in flix.rates]) print('Rates:', *[f'{math.degrees(r):.0f}°/s' for r in flix.rates])
print('Attitude:', *[f'{math.degrees(a):.0f}°' for a in flix.attitude_euler]) print('Attitude:', *[f'{math.degrees(a):.0f}°' for a in flix.attitude_euler])
print('Motors:', flix.motors) print('Motors:', flix.motors)
@@ -23,11 +24,11 @@ print('> imu')
print(flix.cli('imu')) print(flix.cli('imu'))
print('=== Get parameter...') print('=== Get parameter...')
pitch_p = flix.get_param('PITCH_P') pitch_p = flix.get_param('CTL_P_P')
print('PITCH_P = ', pitch_p) print('CTL_P_P = ', pitch_p)
print('=== Set parameter...') print('=== Set parameter...')
flix.set_param('PITCH_P', pitch_p) flix.set_param('CTL_P_P', pitch_p)
print('=== Wait for gyro update...') print('=== Wait for gyro update...')
print('Gyro: ', flix.wait('gyro')) print('Gyro: ', flix.wait('gyro'))
+6 -4
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@@ -24,19 +24,20 @@ pip install pyflix
The API is accessed through the `Flix` class: The API is accessed through the `Flix` class:
```python ```python
from flix import Flix from pyflix import Flix
flix = Flix() # create a Flix object and wait for connection flix = Flix() # create a Flix object and wait for connection
``` ```
### Telemetry ### Telemetry
Basic telemetry is available through object properties. The property names generally match the corresponding variables in the firmware itself: Basic telemetry is available through object properties. The property names generally match the corresponding variables in the firmware code:
```python ```python
print(flix.connected) # True if connected to the drone print(flix.connected) # True if connected to the drone
print(flix.mode) # current flight mode (str) print(flix.mode) # current flight mode (str)
print(flix.armed) # True if the drone is armed print(flix.armed) # True if the drone is armed
print(flix.landed) # True if the drone is landed print(flix.landed) # True if the drone is landed
print(flix.voltage) # battery voltage
print(flix.attitude) # attitude quaternion [w, x, y, z] 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]
@@ -95,6 +96,7 @@ Full list of events:
|`armed`|Armed state update|Armed state *(bool)*| |`armed`|Armed state update|Armed state *(bool)*|
|`mode`|Flight mode update|Flight mode *(str)*| |`mode`|Flight mode update|Flight mode *(str)*|
|`landed`|Landed state update|Landed state *(bool)*| |`landed`|Landed state update|Landed state *(bool)*|
|`voltage`|Battery voltage update|Voltage *(float)*|
|`print`|The drone prints text to the console|Text| |`print`|The drone prints text to the console|Text|
|`attitude`|Attitude update|Attitude quaternion *(list)*| |`attitude`|Attitude update|Attitude quaternion *(list)*|
|`attitude_euler`|Attitude update|Euler angles *(list)*| |`attitude_euler`|Attitude update|Euler angles *(list)*|
@@ -117,8 +119,8 @@ Full list of events:
Get and set firmware parameters using `get_param` and `set_param` methods: 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('CTL_P_P') # get parameter value
flix.set_param('PITCH_P', 5) # set parameter value flix.set_param('CTL_P_P', 5) # set parameter value
``` ```
Execute console commands using `cli` method. This method returns the command response: Execute console commands using `cli` method. This method returns the command response:
+9 -3
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@@ -26,6 +26,7 @@ class Flix:
mode: str = '' mode: str = ''
armed: bool = False armed: bool = False
landed: bool = False landed: bool = False
voltage: float = 0
attitude: List[float] attitude: List[float]
attitude_euler: List[float] # roll, pitch, yaw attitude_euler: List[float] # roll, pitch, yaw
rates: List[float] rates: List[float]
@@ -68,7 +69,7 @@ class Flix:
self._heartbeat_thread.start() self._heartbeat_thread.start()
if wait_connection: if wait_connection:
self.wait('mavlink.HEARTBEAT') self.wait('mavlink.HEARTBEAT')
time.sleep(0.2) # give some time to receive initial state time.sleep(0.6) # give some time to receive initial state
def _init_state(self): def _init_state(self):
self.attitude = [1, 0, 0, 0] self.attitude = [1, 0, 0, 0]
@@ -138,7 +139,7 @@ class Flix:
while True: while True:
try: try:
msg: Optional[mavlink.MAVLink_message] = self.connection.recv_match(blocking=True) msg: Optional[mavlink.MAVLink_message] = self.connection.recv_match(blocking=True)
if msg is None: if msg is None or msg.get_srcSystem() != self.system_id:
continue continue
self._connected() self._connected()
msg_dict = msg.to_dict() msg_dict = msg.to_dict()
@@ -185,11 +186,16 @@ class Flix:
self._trigger('motors', self.motors) self._trigger('motors', self.motors)
if isinstance(msg, mavlink.MAVLink_scaled_imu_message): if isinstance(msg, mavlink.MAVLink_scaled_imu_message):
self.acc = self._mavlink_to_flu([msg.xacc / 1000, msg.yacc / 1000, msg.zacc / 1000]) ONE_G = 9.80665
self.acc = self._mavlink_to_flu([msg.xacc * ONE_G / 1000, msg.yacc * ONE_G / 1000, msg.zacc * ONE_G / 1000])
self.gyro = self._mavlink_to_flu([msg.xgyro / 1000, msg.ygyro / 1000, msg.zgyro / 1000]) self.gyro = self._mavlink_to_flu([msg.xgyro / 1000, msg.ygyro / 1000, msg.zgyro / 1000])
self._trigger('acc', self.acc) self._trigger('acc', self.acc)
self._trigger('gyro', self.gyro) self._trigger('gyro', self.gyro)
if isinstance(msg, mavlink.MAVLink_battery_status_message):
self.voltage = msg.voltages[0] / 1000
self._trigger('voltage', self.voltage)
if isinstance(msg, mavlink.MAVLink_serial_control_message): if isinstance(msg, mavlink.MAVLink_serial_control_message):
# new chunk of data # new chunk of data
text = bytes(msg.data)[:msg.count].decode('utf-8', errors='ignore') text = bytes(msg.data)[:msg.count].decode('utf-8', errors='ignore')
+1 -1
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@@ -1,6 +1,6 @@
[project] [project]
name = "pyflix" name = "pyflix"
version = "0.11" version = "0.14"
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"