Compare commits
47 Commits
level-calib
...
v1.5
| Author | SHA1 | Date | |
|---|---|---|---|
| 4530c05b5c | |||
| 3816ae376f | |||
| 72a72fde80 | |||
| e53051a349 | |||
| f8a9f1f838 | |||
| 76af83fc88 | |||
| dd176180a7 | |||
| 48c33c7050 | |||
| 35e94f6ea6 | |||
| 1f48e379e3 | |||
| ee3c6999ab | |||
| 34c6993842 | |||
| b62f2f9427 | |||
| 7dfef17165 | |||
| 8c8046676b | |||
| 702ec9792e | |||
| 06e2047097 | |||
| 87480476c2 | |||
| 68271c508c | |||
| e81e84e7fc | |||
| 5f1a938d4f | |||
| bd270db493 | |||
| dbf24ea611 | |||
| 08683d696d | |||
| 9ca6841558 | |||
| 28da2d3c8e | |||
| c6632ae6e4 | |||
| 35ca754583 | |||
| 2ccda03573 | |||
| 485a39e740 | |||
| 9bffe5b52f | |||
| d6a79d6c66 | |||
| 350a82bfed | |||
| 6e439859bc | |||
| 835b2243e8 | |||
| ed4e2d87d1 | |||
| 51cd5fc691 | |||
| d8591ea2a9 | |||
| c434107eaf | |||
| 814427dbfd | |||
| 0730ceeffa | |||
| a687303062 | |||
| b2daf2587f | |||
| a8c25d8ac0 | |||
| 3e49d41986 | |||
| 67430c7aac | |||
| 3631743a29 |
@@ -23,6 +23,8 @@ jobs:
|
||||
with:
|
||||
name: firmware-binary
|
||||
path: flix/build
|
||||
- name: Build firmware for ESP32-C3
|
||||
run: make BOARD=esp32:esp32:esp32c3
|
||||
- name: Build firmware for ESP32-S3
|
||||
run: make BOARD=esp32:esp32:esp32s3
|
||||
- name: Check c_cpp_properties.json
|
||||
|
||||
@@ -1,6 +1,5 @@
|
||||
BOARD = esp32:esp32:d1_mini32
|
||||
PORT := $(wildcard /dev/serial/by-id/usb-Silicon_Labs_CP21* /dev/serial/by-id/usb-1a86_USB_Single_Serial_* /dev/cu.usbserial-*)
|
||||
PORT := $(strip $(PORT))
|
||||
PORT := $(strip $(wildcard /dev/serial/by-id/usb-Silicon_Labs_CP21* /dev/serial/by-id/usb-1a86_USB_Single_Serial_* /dev/cu.usbserial-* /dev/cu.usbmodem*))
|
||||
|
||||
build: .dependencies
|
||||
arduino-cli compile --fqbn $(BOARD) flix
|
||||
|
||||
@@ -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">
|
||||
|
||||
## Documentation
|
||||
## Documentation articles
|
||||
|
||||
1. [Assembly instructions](docs/assembly.md).
|
||||
2. [Usage: build, setup and flight](docs/usage.md).
|
||||
@@ -71,14 +71,14 @@ Additional articles:
|
||||
|
||||
|Type|Part|Image|Quantity|
|
||||
|-|-|:-:|:-:|
|
||||
|Microcontroller board|ESP32 Mini|<img src="docs/img/esp32.jpg" width=100>|1|
|
||||
|IMU (and barometer¹) board|GY‑91, MPU-9265 (or other MPU‑9250/MPU‑6500 board)<br>ICM20948V2 (ICM‑20948)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|
|
||||
|Microcontroller board|ESP32 Mini.<br>ESP32-S3/ESP32-C3 boards are also supported.|<img src="docs/img/esp32.jpg" width=100>|1|
|
||||
|IMU (and barometer¹) board|GY‑91, MPU-9265 (or other MPU‑9250/MPU‑6500 board)<br>ICM20948V2 (ICM‑20948)<br>GY-521 (MPU-6050)|<img src="docs/img/gy-91.jpg" width=90 align=center><br><img src="docs/img/icm-20948.jpg" width=100><br><img src="docs/img/gy-521.jpg" width=100>|1|
|
||||
|Boost converter (optional, for more stable power supply)|5V output|<img src="docs/img/buck-boost.jpg" width=100>|1|
|
||||
|Motor|8520 3.7V brushed motor.<br>Motor with exact 3.7V voltage is needed, not ranged working voltage (3.7V — 6V).<br>Make sure the motor shaft diameter and propeller hole diameter match!|<img src="docs/img/motor.jpeg" width=100>|4|
|
||||
|Propeller|55 mm (alternatively 65 mm)|<img src="docs/img/prop.jpg" width=100>|4|
|
||||
|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|
|
||||
|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|
|
||||
|Pull-down resistor<br>Voltage measurement resistor|10 kΩ|<img src="docs/img/resistor10k.jpg" width=100>|6|
|
||||
|3.7V Li-Po battery|LW 952540 (or any compatible by the size).<br>Make sure the battery has enough discharge rate — 25C or more!|<img src="docs/img/battery.jpg" width=100>|1|
|
||||
|Battery connector cable|MX2.0 2P female|<img src="docs/img/mx.png" width=100>|1|
|
||||
|Li-Po Battery charger|Any|<img src="docs/img/charger.jpg" width=100>|1|
|
||||
|Screws for IMU board mounting|M3x5|<img src="docs/img/screw-m3.jpg" width=100>|2|
|
||||
@@ -152,14 +152,16 @@ You can see a user-contributed [variant of complete circuit diagram](https://mir
|
||||
|-|-|
|
||||
|GND|GND|
|
||||
|VIN|VCC (or 3.3V depending on the receiver)|
|
||||
|Signal (TX)|GPIO4¹|
|
||||
|Signal (TX)|GPIO4|
|
||||
|
||||
*¹ — UART2 RX pin was [changed](https://docs.espressif.com/projects/arduino-esp32/en/latest/migration_guides/2.x_to_3.0.html#id14) to GPIO4 in Arduino ESP32 core 3.0.*
|
||||
* Optionally connect the battery voltage divider for voltage monitoring to any ADC1 pin (e. g. *GPIO32* on ESP32, *GPIO3* on ESP32-S3).
|
||||
|
||||
ESP32 and ESP32-S3 [can measure](https://docs.espressif.com/projects/arduino-esp32/en/latest/api/adc.html#analogsetattenuation) up to 3.1 V and ESP32-S3/ESP32-C3 can measure up to 2.5 V, so choose the voltage divider resistors accordingly.
|
||||
|
||||
## Resources
|
||||
|
||||
* Telegram channel on developing the drone and the flight controller (in Russian): https://t.me/opensourcequadcopter.
|
||||
* Official Telegram chat: https://t.me/opensourcequadcopterchat.
|
||||
* Official Telegram chat: https://t.me/opensourcequadcopterchat (English / Russian).
|
||||
* Detailed article on Habr.com about the development of the drone (in Russian): https://habr.com/ru/articles/814127/.
|
||||
|
||||
## Disclaimer
|
||||
|
||||
@@ -28,6 +28,8 @@ Soldered components ([schematics variant](https://miro.com/app/board/uXjVN-dTjoo
|
||||
|
||||
<img src="img/assembly/7.jpg" width=600>
|
||||
|
||||
See an alternative assembly process photos here: https://drive.google.com/drive/folders/1FG5BH9RCzdf1XmJcC70PymiRMXcz6Fx7?usp=sharing.
|
||||
|
||||
## Motor directions
|
||||
|
||||
> [!WARNING]
|
||||
|
||||
@@ -67,6 +67,35 @@ In order to add a console command, modify the `doCommand()` function in `cli.ino
|
||||
>
|
||||
> For on-the-ground commands, use `pause()` function, instead of `delay()`. This function allows to pause in a way that MAVLink connection will continue working.
|
||||
|
||||
### Parameter subsystem
|
||||
|
||||
Parameters subsystem (`parameters.ino`) uses standard [Preferences.h](https://docs.espressif.com/projects/arduino-esp32/en/latest/tutorials/preferences.html) ESP32 library to store parameters in non-volatile memory. Each parameter is a regular global variable, which is registered in the `parameters` array.
|
||||
|
||||
To add a new parameter:
|
||||
|
||||
1. Define a global variable for the parameter, two types are supported: `float` and `int`.
|
||||
2. Add an entry to the `parameters` array, with the parameter name, a pointer to the variable, and optionally a callback function to call when the parameter is changed.
|
||||
3. Everything else will be handled automatically.
|
||||
|
||||
See examples of adding new parameters in commits: [c434107](https://github.com/okalachev/flix/commit/c434107), [a687303](https://github.com/okalachev/flix/commit/a687303).
|
||||
|
||||
## Adding a subsystem
|
||||
|
||||
To add a new subsystem:
|
||||
|
||||
1. Create a new `*.ino` file for your subsystem.
|
||||
2. Define setup and loop functions for the subsystem, for example `setupMySubsystem()` and `loopMySubsystem()`.
|
||||
3. Use `Rate` class if you need to limit the loop frequency, for example:
|
||||
|
||||
```cpp
|
||||
Rate mySubsystemRate(100); // 100 Hz
|
||||
|
||||
void loopMySubsystem() {
|
||||
if (!mySubsystemRate) return;
|
||||
// Do something...
|
||||
}
|
||||
4. Add setup and loop calls in to `setup()` and `loop()` functions in `flix.ino`.
|
||||
|
||||
## Building the firmware
|
||||
|
||||
See build instructions in [usage.md](usage.md).
|
||||
|
||||
|
After Width: | Height: | Size: 101 KiB |
|
Before Width: | Height: | Size: 23 KiB After Width: | Height: | Size: 33 KiB |
|
After Width: | Height: | Size: 44 KiB |
|
After Width: | Height: | Size: 55 KiB |
|
After Width: | Height: | Size: 60 KiB |
|
After Width: | Height: | Size: 38 KiB |
|
After Width: | Height: | Size: 50 KiB |
|
After Width: | Height: | Size: 105 KiB |
|
After Width: | Height: | Size: 34 KiB |
|
After Width: | Height: | Size: 36 KiB |
@@ -12,20 +12,25 @@ 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 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 voltage**. Use a multimeter to measure the battery voltage. The fully charged battery should have about 4.2V.
|
||||
* **Check the battery you use has enough discharge current**. The battery should be able to provide 15A of current. So the C-rating for a 1000 mAh battery should be at least 15C (higher is better).
|
||||
* **Check if there are some startup errors**. Connect the ESP32 to the computer and check the Serial Monitor output. Use the Reset button or `reboot` command to see the whole startup output.
|
||||
* **Check the baudrate is correct**. If you see garbage characters in the Serial Monitor, make sure the baudrate is set to 115200.
|
||||
* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
|
||||
* **Check if the console is working**. Perform `help` command in Serial Monitor. You should see the list of available commands. You can also access the console using QGroundControl *(Vehicle Setup* ⇒ *Analyze Tools* ⇒ *MAVLink Console)*.
|
||||
* **Configure QGroundControl correctly before connecting to the drone** if you use it to control the drone. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
|
||||
* **If QGroundControl doesn't connect**, you might need to disable the firewall and/or VPN on your computer.
|
||||
* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
|
||||
* **Check the IMU is working**. Perform `imu` command and check its output:
|
||||
* The `status` field should be `OK`.
|
||||
* The `rate` field should be about 1000 (Hz).
|
||||
* The `accel` and `gyro` fields should change as you move the drone.
|
||||
* **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).
|
||||
* **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**. Perform the following commands using Serial Monitor:
|
||||
* `mfr` — should rotate front right motor (counter-clockwise).
|
||||
@@ -33,7 +38,10 @@ Do the following:
|
||||
* `mrl` — should rotate rear left motor (counter-clockwise).
|
||||
* `mrr` — should rotate rear right motor (clockwise).
|
||||
* **Check the propeller directions are correct**. Make sure your propeller types (A or B) are installed as on the picture:
|
||||
|
||||
<img src="img/user/peter_ukhov-2/1.jpg" width="200">
|
||||
* **Check the remote control**. Using `rc` command, check the control values reflect your sticks movement. All the controls should change between -1 and 1, and throttle between 0 and 1.
|
||||
* If using SBUS receiver, **calibrate the RC**. Type `cr` command in Serial Monitor and follow the instructions.
|
||||
* **Check the IMU output using QGroundControl**. Connect to the drone using QGroundControl on your computer. Go to the *Analyze* tab, *MAVLINK Inspector*. Plot the data from the `SCALED_IMU` message. The gyroscope and accelerometer data should change according to the drone movement.
|
||||
|
||||
* **If using an SBUS receiver**:
|
||||
* **Define the used GPIO pin** in `RC_RX_PIN` parameter.
|
||||
* **Calibrate the RC** using `cr` command in the console.
|
||||
* **Check the controls** using `rc` command. All the controls should change between -1 and 1, and the throttle between 0 and 1.
|
||||
|
||||
@@ -112,9 +112,9 @@ You can also work with parameters using `p` command in the console. Parameter na
|
||||
|
||||
### 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">
|
||||
|
||||
@@ -122,10 +122,10 @@ Use the following table to set the parameters for common IMU orientations:
|
||||
|
||||
|Orientation|Parameters|Orientation|Parameters|
|
||||
|:-:|-|-|-|
|
||||
|<img src="img/imu-rot-1.png" width="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-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-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-3.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0 |<img src="img/imu-rot-7.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0|
|
||||
|<img src="img/imu-rot-2.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|<img src="img/imu-rot-6.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|
|
||||
|<img src="img/imu-rot-1.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|<img src="img/imu-rot-5.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|
|
||||
|<img src="img/imu-rot-4.png" width="180"><br>☑️ **Default**|<br>`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|<img src="img/imu-rot-8.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|
|
||||
|
||||
### Calibrate accelerometer
|
||||
|
||||
@@ -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).
|
||||
|
||||
Certain ESP32 models (such as ESP32-S3 and ESP32-C3) support a lower maximum PWM frequency; on these boards the parameter `MOT_PWM_FREQ` should be set to 38000 Hz.
|
||||
|
||||
If using brushless motors and ESCs:
|
||||
|
||||
1. Set the appropriate PWM using the parameters: `MOT_PWM_STOP`, `MOT_PWM_MIN`, and `MOT_PWM_MAX` (1000, 1000, and 2000 is typical).
|
||||
2. Decrease the PWM frequency using the `MOT_PWM_FREQ` parameter (400 is typical).
|
||||
|
||||
Reboot the drone to apply the changes.
|
||||
|
||||
> [!CAUTION]
|
||||
> **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 `rate` field should be about 1000 (Hz).
|
||||
* The `accel` and `gyro` fields should change as you move the drone.
|
||||
* The `accel bias` and `accel scale` fields should contain calibration parameters (not zeros and ones).
|
||||
* The `gyro bias` field should contain estimated gyro bias (not zeros).
|
||||
* The `landed` field should be `1` when the drone is still on the ground and `0` when you lift it up.
|
||||
|
||||
2. Check the attitude estimation: connect to the drone using QGroundControl, rotate the drone in different orientations and check if the attitude estimation shown in QGroundControl is correct. 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>
|
||||
|
||||
3. Perform motor tests in the console. Use the following commands **— remove the propellers before running the tests!**
|
||||
3. Perform motor tests. Use the following commands **— remove the propellers before running the tests!**
|
||||
|
||||
* `mfr` — should rotate front right motor (counter-clockwise).
|
||||
* `mfl` — should rotate front left motor (clockwise).
|
||||
* `mrl` — should rotate rear left motor (counter-clockwise).
|
||||
* `mrr` — should rotate rear right motor (clockwise).
|
||||
* `mfr` — rotate front right motor (counter-clockwise).
|
||||
* `mfl` — rotate front left motor (clockwise).
|
||||
* `mrl` — rotate rear left motor (counter-clockwise).
|
||||
* `mrr` — rotate rear right motor (clockwise).
|
||||
|
||||
Rotation diagram:
|
||||
Make sure rotation directions and propeller types match the following diagram:
|
||||
|
||||
<img src="img/motors.svg" width=200>
|
||||
|
||||
@@ -181,6 +192,18 @@ There are several ways to control the drone's flight: using **smartphone** (Wi-F
|
||||
|
||||
### Control with a smartphone
|
||||
|
||||
#### Using Mavlink Joystick app (Android)
|
||||
|
||||
<img src="https://github.com/goldarte/mavlink-joystick/blob/master/app_screen.png?raw=true" width="400">
|
||||
|
||||
1. Download and install [Mavlink Joystick app](https://github.com/goldarte/mavlink-joystick/releases/latest).
|
||||
2. Power the drone using the battery.
|
||||
3. Connect your smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
|
||||
4. Open Mavlink Joystick app. It should connect and begin showing the drone's telemetry automatically.
|
||||
5. Use the virtual joystick to fly the drone!
|
||||
|
||||
#### Using QGroundControl app
|
||||
|
||||
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone.
|
||||
2. Power the drone using the battery.
|
||||
3. Connect your smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
|
||||
@@ -193,11 +216,13 @@ There are several ways to control the drone's flight: using **smartphone** (Wi-F
|
||||
|
||||
### Control with a remote control
|
||||
|
||||
Before using remote SBUS-connected remote control, you need to calibrate it:
|
||||
If using SBUS-connected remote control you need to enable SBUS and calibrate it:
|
||||
|
||||
1. Access the console using QGroundControl (recommended) or Serial Monitor.
|
||||
2. Type `cr` command and follow the instructions.
|
||||
3. Use the remote control to fly the drone!
|
||||
1. Connect to the drone using QGroundControl.
|
||||
2. In parameters, set the `RC_RX_PIN` parameter to the GPIO pin number where the SBUS signal is connected, for example: 4. Negative value disables SBUS.
|
||||
3. Check if the receiver is working using `rc` command in the console.
|
||||
4. Open the console, type `cr` command and follow the instructions to calibrate the remote control.
|
||||
5. Use the remote control to fly the drone!
|
||||
|
||||
### Control with a USB remote control
|
||||
|
||||
@@ -234,11 +259,11 @@ When finished flying, **disarm** the drone, moving the left stick to the bottom
|
||||
|
||||
### Flight modes
|
||||
|
||||
Flight mode is changed using mode switch on the remote control or using the command line.
|
||||
Flight mode is changed using mode switch on the remote control (if configured) or using the console commands. The main flight mode is *STAB*. In order to change modes using SBUS remote control, set the parameters: `CTL_FLT_MODE_0`, `CTL_FLT_MODE_1`, and `CTL_FLT_MODE_2` to required mode numbers (0 for *RAW*, 1 for *ACRO*, 2 for *STAB*, 3 for *AUTO*).
|
||||
|
||||
#### STAB
|
||||
|
||||
The default mode is *STAB*. In this mode, the drone stabilizes its attitude (orientation). The left stick controls throttle and yaw rate, the right stick controls pitch and roll angles.
|
||||
In this mode, the drone stabilizes its attitude (orientation). The left stick controls throttle and yaw rate, the right stick controls pitch and roll angles.
|
||||
|
||||
> [!IMPORTANT]
|
||||
> The drone doesn't stabilize its position, so slight drift is possible. The pilot should compensate it manually.
|
||||
@@ -253,9 +278,9 @@ In this mode, the pilot controls the angular rates. This control method is diffi
|
||||
|
||||
#### AUTO
|
||||
|
||||
In this mode, the pilot inputs are ignored (except the mode switch, if configured). The drone can be controlled using [pyflix](../tools/pyflix/) Python library, or by modifying the firmware to implement the needed autonomous behavior.
|
||||
In this mode, the pilot inputs are ignored (except the mode switch). The drone can be controlled using [pyflix](../tools/pyflix/) Python library, or by modifying the firmware to implement the needed behavior.
|
||||
|
||||
If the pilot moves the control sticks, the drone will switch back to *STAB* mode.
|
||||
If the pilot moves the control sticks and mode switch is not configured, the drone will switch back to *STAB* mode.
|
||||
|
||||
## Wi-Fi configuration
|
||||
|
||||
|
||||
@@ -4,6 +4,38 @@ 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: Oleg Kalachev.<br>
|
||||
Description: the first attempt on making an official PCB based Flix drone (Flix2 board). The IMU is not working on this version, so an external MPU-6050 board was used, therefore considered as **Flix version 1.5**.<br>
|
||||
[Flight video](https://drive.google.com/file/d/1R7tuUsFmPY0CGcOCFfMFaCp9kR49K3bl/view?usp=sharing).
|
||||
|
||||
<img src="img/flix1.5.jpg" width=300>
|
||||
|
||||
---
|
||||
|
||||
Author: [FanBy0ru](https://https://github.com/FanBy0ru).<br>
|
||||
Description: custom 3D-printed frame.<br>
|
||||
Frame STLs and flight validation: https://cults3d.com/en/3d-model/gadget/armature-pour-flix-drone.
|
||||
|
||||
<img src="img/user/fanby0ru/1.jpg" height=200> <img src="img/user/fanby0ru/2.jpg" height=200>
|
||||
|
||||
---
|
||||
|
||||
Author: Ivan44 Phalko.<br>
|
||||
Description: custom PCB, cusom test bench.<br>
|
||||
[Flight validation](https://drive.google.com/file/d/17DNDJ1gPmCmDRAwjedCbJ9RXAyqMqqcX/view?usp=sharing).
|
||||
|
||||
<img src="img/user/phalko/1.jpg" height=200> <img src="img/user/phalko/2.jpg" height=200> <img src="img/user/phalko/3.jpg" height=200>
|
||||
|
||||
---
|
||||
|
||||
Author: **Arkadiy "Arky" Matsekh**, Foucault Dynamics, Gold Coast, Australia.<br>
|
||||
The drone was built for the University of Queensland industry-led Master's capstone project.
|
||||
|
||||
|
||||
@@ -16,15 +16,17 @@ extern float controlTime;
|
||||
extern int mode;
|
||||
extern bool armed;
|
||||
extern LowPassFilter<Vector> gyroBiasFilter;
|
||||
extern float voltage;
|
||||
|
||||
const char* motd =
|
||||
"\nWelcome to\n"
|
||||
" _______ __ __ ___ ___\n"
|
||||
"| ____|| | | | \\ \\ / /\n"
|
||||
"| |__ | | | | \\ V /\n"
|
||||
"| __| | | | | > <\n"
|
||||
"| | | `----.| | / . \\\n"
|
||||
"|__| |_______||__| /__/ \\__\\\n\n"
|
||||
"(C) Oleg Kalachev\n"
|
||||
"https://github.com/okalachev/flix\n\n"
|
||||
"Commands:\n\n"
|
||||
"help - show help\n"
|
||||
"p - show all parameters\n"
|
||||
@@ -39,6 +41,7 @@ const char* motd =
|
||||
"disarm - disarm the drone\n"
|
||||
"raw/stab/acro/auto - set mode\n"
|
||||
"rc - show RC data\n"
|
||||
"pw - show power info\n"
|
||||
"wifi - show Wi-Fi info\n"
|
||||
"ap <ssid> <password> - setup Wi-Fi access point\n"
|
||||
"sta <ssid> <password> - setup Wi-Fi client mode\n"
|
||||
@@ -135,6 +138,8 @@ void doCommand(String str, bool echo = false) {
|
||||
print("time: %.1f\n", controlTime);
|
||||
print("mode: %s\n", getModeName());
|
||||
print("armed: %d\n", armed);
|
||||
} else if (command == "pw") {
|
||||
print("Voltage: %.1f V\n", voltage);
|
||||
} else if (command == "wifi") {
|
||||
printWiFiInfo();
|
||||
} else if (command == "ap") {
|
||||
@@ -164,6 +169,7 @@ void doCommand(String str, bool echo = false) {
|
||||
print("Chip: %s\n", ESP.getChipModel());
|
||||
print("Temperature: %.1f °C\n", temperatureRead());
|
||||
print("Free heap: %d\n", ESP.getFreeHeap());
|
||||
print("Firmware: " __DATE__ " " __TIME__ "\n");
|
||||
// Print tasks table
|
||||
print("Num Task Stack Prio Core CPU%%\n");
|
||||
int taskCount = uxTaskGetNumberOfTasks();
|
||||
@@ -174,7 +180,7 @@ void doCommand(String str, bool echo = false) {
|
||||
String core = systemState[i].xCoreID == tskNO_AFFINITY ? "*" : String(systemState[i].xCoreID);
|
||||
int cpuPercentage = systemState[i].ulRunTimeCounter / (totalRunTime / 100);
|
||||
print("%-5d%-20s%-7d%-6d%-6s%d\n",systemState[i].xTaskNumber, systemState[i].pcTaskName,
|
||||
systemState[i].usStackHighWaterMark, systemState[i].uxCurrentPriority, core, cpuPercentage);
|
||||
systemState[i].usStackHighWaterMark, systemState[i].uxCurrentPriority, core.c_str(), cpuPercentage);
|
||||
}
|
||||
delete[] systemState;
|
||||
#endif
|
||||
|
||||
@@ -67,7 +67,7 @@ void control() {
|
||||
|
||||
void interpretControls() {
|
||||
if (controlMode < 0.25) mode = flightModes[0];
|
||||
else if (controlMode < 0.75) mode = flightModes[1];
|
||||
else if (controlMode <= 0.75) mode = flightModes[1];
|
||||
else if (controlMode > 0.75) mode = flightModes[2];
|
||||
|
||||
if (mode == AUTO) return; // pilot is not effective in AUTO mode
|
||||
@@ -149,12 +149,25 @@ void controlTorque() {
|
||||
motors[MOTOR_REAR_LEFT] = 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[1] = constrain(motors[1], 0, 1);
|
||||
motors[2] = constrain(motors[2], 0, 1);
|
||||
motors[3] = constrain(motors[3], 0, 1);
|
||||
}
|
||||
|
||||
void desaturate(float& a, float& b, float& c, float& d) {
|
||||
float maxThrust = max(max(a, b), max(c, d));
|
||||
if (maxThrust > 1) {
|
||||
float diff = maxThrust - 1;
|
||||
a -= diff;
|
||||
b -= diff;
|
||||
c -= diff;
|
||||
d -= diff;
|
||||
}
|
||||
}
|
||||
|
||||
const char* getModeName() {
|
||||
switch (mode) {
|
||||
case RAW: return "RAW";
|
||||
|
||||
@@ -1,7 +1,7 @@
|
||||
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
|
||||
// Repository: https://github.com/okalachev/flix
|
||||
|
||||
// Attitude estimation from gyro and accelerometer
|
||||
// Attitude estimation using gyro and accelerometer
|
||||
|
||||
#include "quaternion.h"
|
||||
#include "vector.h"
|
||||
@@ -13,11 +13,13 @@ Quaternion attitude; // estimated attitude
|
||||
bool landed;
|
||||
|
||||
float accWeight = 0.003;
|
||||
float levelWeight = 0.0002;
|
||||
LowPassFilter<Vector> ratesFilter(0.2); // cutoff frequency ~ 40 Hz
|
||||
|
||||
void estimate() {
|
||||
applyGyro();
|
||||
applyAcc();
|
||||
applyLevel();
|
||||
}
|
||||
|
||||
void applyGyro() {
|
||||
@@ -42,3 +44,12 @@ void applyAcc() {
|
||||
// apply 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));
|
||||
}
|
||||
|
||||
@@ -18,11 +18,11 @@ extern float motors[4];
|
||||
void setup() {
|
||||
Serial.begin(115200);
|
||||
print("Initializing flix\n");
|
||||
disableBrownOut();
|
||||
setupParameters();
|
||||
setupPower();
|
||||
setupLED();
|
||||
setupMotors();
|
||||
setLED(true);
|
||||
setupMotors();
|
||||
setupWiFi();
|
||||
setupIMU();
|
||||
setupRC();
|
||||
@@ -39,6 +39,7 @@ void loop() {
|
||||
sendMotors();
|
||||
handleInput();
|
||||
processMavlink();
|
||||
readVoltage();
|
||||
logData();
|
||||
syncParameters();
|
||||
}
|
||||
|
||||
@@ -10,7 +10,7 @@
|
||||
#include "util.h"
|
||||
|
||||
MPU9250 imu(SPI);
|
||||
Vector imuRotation(0, 0, -PI / 2); // imu orientation as Euler angles
|
||||
Vector imuRotation(0, 0, PI / 2); // imu orientation as Euler angles
|
||||
|
||||
Vector gyro; // gyroscope output, rad/s
|
||||
Vector gyroBias;
|
||||
@@ -121,7 +121,7 @@ void printIMUInfo() {
|
||||
print("model: %s\n", imu.getModel());
|
||||
print("who am I: 0x%02X\n", imu.whoAmI());
|
||||
print("rate: %.0f\n", loopRate);
|
||||
print("gyro: %f %f %f\n", rates.x, rates.y, rates.z);
|
||||
print("gyro: %f %f %f\n", gyro.x, gyro.y, gyro.z);
|
||||
print("acc: %f %f %f\n", acc.x, acc.y, acc.z);
|
||||
imu.waitForData();
|
||||
Vector rawGyro, rawAcc;
|
||||
|
||||
@@ -14,6 +14,10 @@ public:
|
||||
LowPassFilter(float alpha): alpha(alpha) {};
|
||||
|
||||
T update(const T input) {
|
||||
if (!init) {
|
||||
init = true;
|
||||
return output = input;
|
||||
}
|
||||
return output += alpha * (input - output);
|
||||
}
|
||||
|
||||
@@ -22,6 +26,9 @@ public:
|
||||
}
|
||||
|
||||
void reset() {
|
||||
output = T(); // set to zero
|
||||
init = false;
|
||||
}
|
||||
|
||||
private:
|
||||
bool init = false;
|
||||
};
|
||||
|
||||
@@ -7,13 +7,15 @@
|
||||
#include "util.h"
|
||||
|
||||
extern float controlTime;
|
||||
extern float voltage;
|
||||
|
||||
bool mavlinkConnected = false;
|
||||
String mavlinkPrintBuffer;
|
||||
int mavlinkSysId = 1;
|
||||
Rate telemetryFast(10);
|
||||
Rate telemetrySlow(2);
|
||||
|
||||
bool mavlinkConnected = false;
|
||||
String mavlinkPrintBuffer;
|
||||
|
||||
void processMavlink() {
|
||||
sendMavlink();
|
||||
receiveMavlink();
|
||||
@@ -38,12 +40,19 @@ void sendMavlink() {
|
||||
mavlink_msg_extended_sys_state_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
|
||||
MAV_VTOL_STATE_UNDEFINED, landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR);
|
||||
sendMessage(&msg);
|
||||
|
||||
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) {
|
||||
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,
|
||||
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);
|
||||
|
||||
mavlink_msg_rc_channels_raw_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, controlTime * 1000, 0,
|
||||
@@ -56,7 +65,7 @@ void sendMavlink() {
|
||||
sendMessage(&msg);
|
||||
|
||||
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,
|
||||
0, 0, 0, 0);
|
||||
sendMessage(&msg);
|
||||
|
||||
@@ -24,6 +24,7 @@ void setupMotors() {
|
||||
// configure pins
|
||||
for (int i = 0; i < 4; i++) {
|
||||
ledcAttach(motorPins[i], pwmFrequency, pwmResolution);
|
||||
pwmFrequency = ledcChangeFrequency(motorPins[i], pwmFrequency, pwmResolution); // when reconfiguring
|
||||
}
|
||||
sendMotors();
|
||||
print("Motors initialized\n");
|
||||
@@ -53,7 +54,7 @@ bool motorsActive() {
|
||||
|
||||
void testMotor(int 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
|
||||
sendMotors();
|
||||
pause(3);
|
||||
|
||||
@@ -6,21 +6,26 @@
|
||||
#include <Preferences.h>
|
||||
#include "util.h"
|
||||
|
||||
extern float channelZero[16];
|
||||
extern float channelMax[16];
|
||||
extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
|
||||
extern int channelZero[16];
|
||||
extern int channelMax[16];
|
||||
extern int rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
|
||||
extern int rcRxPin;
|
||||
extern int wifiMode, udpLocalPort, udpRemotePort;
|
||||
extern float rcLossTimeout, descendTime;
|
||||
extern int voltagePin;
|
||||
extern float voltageScale;
|
||||
extern LowPassFilter<float> voltageFilter;
|
||||
|
||||
Preferences storage;
|
||||
|
||||
struct Parameter {
|
||||
const char *name; // max length is 15 (Preferences key limit)
|
||||
const char *name; // max length is 15
|
||||
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
|
||||
Parameter(const char *name, float *variable) : name(name), integer(false), f(variable) {};
|
||||
Parameter(const char *name, int *variable) : name(name), integer(true), i(variable) {};
|
||||
void (*callback)(); // called after parameter change
|
||||
Parameter(const char *name, float *variable, void (*callback)() = nullptr) : name(name), integer(false), f(variable), callback(callback) {};
|
||||
Parameter(const char *name, int *variable, void (*callback)() = nullptr) : name(name), integer(true), i(variable), callback(callback) {};
|
||||
float getValue() const { return integer ? *i : *f; };
|
||||
void setValue(const float value) { if (integer) *i = value; else *f = value; };
|
||||
};
|
||||
@@ -31,13 +36,16 @@ Parameter parameters[] = {
|
||||
{"CTL_R_RATE_I", &rollRatePID.i},
|
||||
{"CTL_R_RATE_D", &rollRatePID.d},
|
||||
{"CTL_R_RATE_WU", &rollRatePID.windup},
|
||||
{"CTL_R_RATE_D_A", &rollRatePID.lpf.alpha},
|
||||
{"CTL_P_RATE_P", &pitchRatePID.p},
|
||||
{"CTL_P_RATE_I", &pitchRatePID.i},
|
||||
{"CTL_P_RATE_D", &pitchRatePID.d},
|
||||
{"CTL_P_RATE_WU", &pitchRatePID.windup},
|
||||
{"CTL_P_RATE_D_A", &pitchRatePID.lpf.alpha},
|
||||
{"CTL_Y_RATE_P", &yawRatePID.p},
|
||||
{"CTL_Y_RATE_I", &yawRatePID.i},
|
||||
{"CTL_Y_RATE_D", &yawRatePID.d},
|
||||
{"CTL_Y_RATE_D_A", &yawRatePID.lpf.alpha},
|
||||
{"CTL_R_P", &rollPID.p},
|
||||
{"CTL_R_I", &rollPID.i},
|
||||
{"CTL_R_D", &rollPID.d},
|
||||
@@ -65,18 +73,20 @@ Parameter parameters[] = {
|
||||
{"IMU_GYRO_BIAS_A", &gyroBiasFilter.alpha},
|
||||
// estimate
|
||||
{"EST_ACC_WEIGHT", &accWeight},
|
||||
{"EST_LVL_WEIGHT", &levelWeight},
|
||||
{"EST_RATES_LPF_A", &ratesFilter.alpha},
|
||||
// motors
|
||||
{"MOT_PIN_FL", &motorPins[MOTOR_FRONT_LEFT]},
|
||||
{"MOT_PIN_FR", &motorPins[MOTOR_FRONT_RIGHT]},
|
||||
{"MOT_PIN_RL", &motorPins[MOTOR_REAR_LEFT]},
|
||||
{"MOT_PIN_RR", &motorPins[MOTOR_REAR_RIGHT]},
|
||||
{"MOT_PWM_FREQ", &pwmFrequency},
|
||||
{"MOT_PWM_RES", &pwmResolution},
|
||||
{"MOT_PIN_FL", &motorPins[MOTOR_FRONT_LEFT], setupMotors},
|
||||
{"MOT_PIN_FR", &motorPins[MOTOR_FRONT_RIGHT], setupMotors},
|
||||
{"MOT_PIN_RL", &motorPins[MOTOR_REAR_LEFT], setupMotors},
|
||||
{"MOT_PIN_RR", &motorPins[MOTOR_REAR_RIGHT], setupMotors},
|
||||
{"MOT_PWM_FREQ", &pwmFrequency, setupMotors},
|
||||
{"MOT_PWM_RES", &pwmResolution, setupMotors},
|
||||
{"MOT_PWM_STOP", &pwmStop},
|
||||
{"MOT_PWM_MIN", &pwmMin},
|
||||
{"MOT_PWM_MAX", &pwmMax},
|
||||
// rc
|
||||
{"RC_RX_PIN", &rcRxPin, setupRC},
|
||||
{"RC_ZERO_0", &channelZero[0]},
|
||||
{"RC_ZERO_1", &channelZero[1]},
|
||||
{"RC_ZERO_2", &channelZero[2]},
|
||||
@@ -100,19 +110,24 @@ Parameter parameters[] = {
|
||||
{"RC_MODE", &modeChannel},
|
||||
// wifi
|
||||
{"WIFI_MODE", &wifiMode},
|
||||
{"WIFI_LOC_PORT", &udpLocalPort},
|
||||
{"WIFI_REM_PORT", &udpRemotePort},
|
||||
{"WIFI_PORT_LOC", &udpLocalPort},
|
||||
{"WIFI_PORT_REM", &udpRemotePort},
|
||||
// mavlink
|
||||
{"MAV_SYS_ID", &mavlinkSysId},
|
||||
{"MAV_RATE_SLOW", &telemetrySlow.rate},
|
||||
{"MAV_RATE_FAST", &telemetryFast.rate},
|
||||
// power
|
||||
{"PWR_VOLT_PIN", &voltagePin},
|
||||
{"PWR_VOLT_SCALE", &voltageScale},
|
||||
{"PWR_VOLT_LPF_A", &voltageFilter.alpha},
|
||||
// safety
|
||||
{"SF_RC_LOSS_TIME", &rcLossTimeout},
|
||||
{"SF_DESCEND_TIME", &descendTime},
|
||||
};
|
||||
|
||||
void setupParameters() {
|
||||
storage.begin("flix", false);
|
||||
print("Setup parameters\n");
|
||||
storage.begin("flix");
|
||||
// Read parameters from storage
|
||||
for (auto ¶meter : parameters) {
|
||||
if (!storage.isKey(parameter.name)) {
|
||||
@@ -151,6 +166,7 @@ bool setParameter(const char *name, const float value) {
|
||||
if (strcasecmp(parameter.name, name) == 0) {
|
||||
if (parameter.integer && !isfinite(value)) return false; // can't set integer to NaN or Inf
|
||||
parameter.setValue(value);
|
||||
if (parameter.callback) parameter.callback();
|
||||
return true;
|
||||
}
|
||||
}
|
||||
@@ -164,8 +180,7 @@ void syncParameters() {
|
||||
|
||||
for (auto ¶meter : parameters) {
|
||||
if (parameter.getValue() == parameter.cache) continue; // no change
|
||||
if (isnan(parameter.getValue()) && isnan(parameter.cache)) continue; // both are NaN
|
||||
if (isinf(parameter.getValue()) && isinf(parameter.cache)) continue; // both are Inf
|
||||
if (isnan(parameter.getValue()) && isnan(parameter.cache)) continue; // both are NAN
|
||||
|
||||
storage.putFloat(parameter.name, parameter.getValue());
|
||||
parameter.cache = parameter.getValue(); // update cache
|
||||
|
||||
@@ -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);
|
||||
}
|
||||
@@ -6,25 +6,27 @@
|
||||
#include <SBUS.h>
|
||||
#include "util.h"
|
||||
|
||||
SBUS rc(Serial2);
|
||||
SBUS rc(Serial1);
|
||||
int rcRxPin = -1; // -1 means disabled
|
||||
|
||||
uint16_t channels[16]; // raw rc channels
|
||||
float channelZero[16]; // calibration zero values
|
||||
float channelMax[16]; // calibration max values
|
||||
int channelZero[16]; // calibration zero values
|
||||
int channelMax[16]; // calibration max values
|
||||
|
||||
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
|
||||
float controlMode = NAN;
|
||||
float controlTime = NAN; // time of the last controls update
|
||||
|
||||
// Channels mapping (nan means not assigned):
|
||||
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
|
||||
int rollChannel = -1, pitchChannel = -1, throttleChannel = -1, yawChannel = -1, modeChannel = -1; // channel mapping
|
||||
|
||||
void setupRC() {
|
||||
if (rcRxPin < 0) return;
|
||||
print("Setup RC\n");
|
||||
rc.begin();
|
||||
rc.begin(rcRxPin);
|
||||
}
|
||||
|
||||
bool readRC() {
|
||||
if (rcRxPin < 0) return false;
|
||||
if (rc.read()) {
|
||||
SBUSData data = rc.data();
|
||||
for (int i = 0; i < 16; i++) channels[i] = data.ch[i]; // copy channels data
|
||||
@@ -41,30 +43,34 @@ void normalizeRC() {
|
||||
controls[i] = mapf(channels[i], channelZero[i], channelMax[i], 0, 1);
|
||||
}
|
||||
// Update control values
|
||||
controlRoll = rollChannel >= 0 ? controls[(int)rollChannel] : 0;
|
||||
controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : 0;
|
||||
controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : 0;
|
||||
controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : 0;
|
||||
controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN; // mode switch should not have affect if not set
|
||||
controlRoll = rollChannel < 0 ? 0 : controls[rollChannel];
|
||||
controlPitch = pitchChannel < 0 ? 0 : controls[pitchChannel];
|
||||
controlYaw = yawChannel < 0 ? 0 : controls[yawChannel];
|
||||
controlThrottle = throttleChannel < 0 ? 0 : controls[throttleChannel];
|
||||
controlMode = modeChannel < 0 ? NAN : controls[modeChannel]; // mode control is ineffective if not mapped
|
||||
}
|
||||
|
||||
void calibrateRC() {
|
||||
uint16_t zero[16];
|
||||
uint16_t center[16];
|
||||
uint16_t max[16];
|
||||
if (rcRxPin < 0) {
|
||||
print("RC_RX_PIN = %d, set the RC pin!\n", rcRxPin);
|
||||
return;
|
||||
}
|
||||
uint16_t zero[16]; // for zero positions
|
||||
uint16_t center[16]; // for center positions
|
||||
uint16_t _[16]; // for unused data
|
||||
print("1/8 Calibrating RC: put all switches to default positions [3 sec]\n");
|
||||
pause(3);
|
||||
calibrateRCChannel(NULL, zero, zero, "2/8 Move sticks [3 sec]\n... ...\n... .o.\n.o. ...\n");
|
||||
calibrateRCChannel(NULL, center, center, "3/8 Move sticks [3 sec]\n... ...\n.o. .o.\n... ...\n");
|
||||
calibrateRCChannel(&throttleChannel, zero, max, "4/8 Move sticks [3 sec]\n.o. ...\n... .o.\n... ...\n");
|
||||
calibrateRCChannel(&yawChannel, center, max, "5/8 Move sticks [3 sec]\n... ...\n..o .o.\n... ...\n");
|
||||
calibrateRCChannel(&pitchChannel, zero, max, "6/8 Move sticks [3 sec]\n... .o.\n... ...\n.o. ...\n");
|
||||
calibrateRCChannel(&rollChannel, zero, max, "7/8 Move sticks [3 sec]\n... ...\n... ..o\n.o. ...\n");
|
||||
calibrateRCChannel(&modeChannel, zero, max, "8/8 Put mode switch to max [3 sec]\n");
|
||||
calibrateRCChannel(NULL, _, zero, "2/8 Move sticks [3 sec]\n... ...\n... .o.\n.o. ...\n");
|
||||
calibrateRCChannel(&throttleChannel, zero, _, "3/8 Move sticks [3 sec]\n.o. ...\n... .o.\n... ...\n");
|
||||
calibrateRCChannel(NULL, _, center, "4/8 Move sticks [3 sec]\n... ...\n.o. .o.\n... ...\n");
|
||||
calibrateRCChannel(&yawChannel, center, _, "5/8 Move sticks [3 sec]\n... ...\n..o .o.\n... ...\n");
|
||||
calibrateRCChannel(&pitchChannel, zero, _, "6/8 Move sticks [3 sec]\n... .o.\n... ...\n.o. ...\n");
|
||||
calibrateRCChannel(&rollChannel, zero, _, "7/8 Move sticks [3 sec]\n... ...\n... ..o\n.o. ...\n");
|
||||
calibrateRCChannel(&modeChannel, zero, _, "8/8 Put mode switch to max [3 sec]\n");
|
||||
printRCCalibration();
|
||||
}
|
||||
|
||||
void calibrateRCChannel(float *channel, uint16_t in[16], uint16_t out[16], const char *str) {
|
||||
void calibrateRCChannel(int *channel, uint16_t in[16], uint16_t out[16], const char *str) {
|
||||
print("%s", str);
|
||||
pause(3);
|
||||
for (int i = 0; i < 30; i++) readRC(); // try update 30 times max
|
||||
@@ -85,15 +91,15 @@ void calibrateRCChannel(float *channel, uint16_t in[16], uint16_t out[16], const
|
||||
channelZero[ch] = in[ch];
|
||||
channelMax[ch] = out[ch];
|
||||
} else {
|
||||
*channel = NAN;
|
||||
*channel = -1;
|
||||
}
|
||||
}
|
||||
|
||||
void printRCCalibration() {
|
||||
print("Control Ch Zero Max\n");
|
||||
print("Roll %-7g%-7g%-7g\n", rollChannel, rollChannel >= 0 ? channelZero[(int)rollChannel] : NAN, rollChannel >= 0 ? channelMax[(int)rollChannel] : NAN);
|
||||
print("Pitch %-7g%-7g%-7g\n", pitchChannel, pitchChannel >= 0 ? channelZero[(int)pitchChannel] : NAN, pitchChannel >= 0 ? channelMax[(int)pitchChannel] : NAN);
|
||||
print("Yaw %-7g%-7g%-7g\n", yawChannel, yawChannel >= 0 ? channelZero[(int)yawChannel] : NAN, yawChannel >= 0 ? channelMax[(int)yawChannel] : NAN);
|
||||
print("Throttle %-7g%-7g%-7g\n", throttleChannel, throttleChannel >= 0 ? channelZero[(int)throttleChannel] : NAN, throttleChannel >= 0 ? channelMax[(int)throttleChannel] : NAN);
|
||||
print("Mode %-7g%-7g%-7g\n", modeChannel, modeChannel >= 0 ? channelZero[(int)modeChannel] : NAN, modeChannel >= 0 ? channelMax[(int)modeChannel] : NAN);
|
||||
print("Roll %-7d%-7d%-7d\n", rollChannel, rollChannel < 0 ? 0 : channelZero[rollChannel], rollChannel < 0 ? 0 : channelMax[rollChannel]);
|
||||
print("Pitch %-7d%-7d%-7d\n", pitchChannel, pitchChannel < 0 ? 0 : channelZero[pitchChannel], pitchChannel < 0 ? 0 : channelMax[pitchChannel]);
|
||||
print("Yaw %-7d%-7d%-7d\n", yawChannel, yawChannel < 0 ? 0 : channelZero[yawChannel], yawChannel < 0 ? 0 : channelMax[yawChannel]);
|
||||
print("Throttle %-7d%-7d%-7d\n", throttleChannel, throttleChannel < 0 ? 0 : channelZero[throttleChannel], throttleChannel < 0 ? 0 : channelMax[throttleChannel]);
|
||||
print("Mode %-7d%-7d%-7d\n", modeChannel, modeChannel < 0 ? 0 : channelZero[modeChannel], modeChannel < 0 ? 0 : channelMax[modeChannel]);
|
||||
}
|
||||
|
||||
@@ -37,8 +37,8 @@ void descend() {
|
||||
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
|
||||
// controls changed and mode switch is not configured
|
||||
if (mode == AUTO && invalid(controlMode)) mode = STAB; // regain control by the pilot
|
||||
}
|
||||
roll = controlRoll;
|
||||
pitch = controlPitch;
|
||||
|
||||
@@ -6,8 +6,6 @@
|
||||
#pragma once
|
||||
|
||||
#include <math.h>
|
||||
#include <soc/soc.h>
|
||||
#include <soc/rtc_cntl_reg.h>
|
||||
|
||||
const float ONE_G = 9.80665;
|
||||
extern float t;
|
||||
@@ -35,19 +33,17 @@ float wrapAngle(float angle) {
|
||||
return angle;
|
||||
}
|
||||
|
||||
// Disable reset on low voltage
|
||||
void disableBrownOut() {
|
||||
REG_CLR_BIT(RTC_CNTL_BROWN_OUT_REG, RTC_CNTL_BROWN_OUT_ENA);
|
||||
}
|
||||
|
||||
// Trim and split string by spaces
|
||||
void splitString(String& str, String& token0, String& token1, String& token2) {
|
||||
str.trim();
|
||||
if (str.isEmpty()) return;
|
||||
char chars[str.length() + 1];
|
||||
str.toCharArray(chars, str.length() + 1);
|
||||
token0 = strtok(chars, " ");
|
||||
token1 = strtok(NULL, " "); // String(NULL) creates empty string
|
||||
token1 = strtok(NULL, " ");
|
||||
token2 = strtok(NULL, "");
|
||||
if (token1.c_str() == NULL) token1 = "";
|
||||
if (token2.c_str() == NULL) token2 = "";
|
||||
}
|
||||
|
||||
// Rate limiter
|
||||
|
||||
@@ -105,10 +105,23 @@ public:
|
||||
}
|
||||
|
||||
static Vector rotationVectorBetween(const Vector& a, const Vector& b) {
|
||||
float an = a.norm();
|
||||
float bn = b.norm();
|
||||
if (an < 1e-6 || bn < 1e-6) {
|
||||
return Vector(0, 0, 0);
|
||||
}
|
||||
Vector direction = cross(a, b);
|
||||
if (direction.zero()) {
|
||||
// vectors are opposite, return any perpendicular vector
|
||||
return cross(a, Vector(1, 0, 0));
|
||||
if (direction.norm() < 1e-6) { // vectors are parallel
|
||||
if (dot(a, b) > 0) { // same direction
|
||||
return Vector(0, 0, 0);
|
||||
}
|
||||
// opposite direction
|
||||
Vector perp = cross(a, Vector(1, 0, 0));
|
||||
if (perp.norm() < 1e-6) {
|
||||
perp = cross(a, Vector(0, 1, 0));
|
||||
}
|
||||
perp.normalize();
|
||||
return perp * PI;
|
||||
}
|
||||
direction.normalize();
|
||||
float angle = angleBetween(a, b);
|
||||
|
||||
@@ -24,7 +24,10 @@ void setupWiFi() {
|
||||
WiFi.softAP(storage.getString("WIFI_AP_SSID", "flix").c_str(), storage.getString("WIFI_AP_PASS", "flixwifi").c_str());
|
||||
} else if (wifiMode == W_STA) {
|
||||
WiFi.begin(storage.getString("WIFI_STA_SSID", "").c_str(), storage.getString("WIFI_STA_PASS", "").c_str());
|
||||
} else {
|
||||
return;
|
||||
}
|
||||
WiFi.setSleep(false); // disable power save
|
||||
udp.begin(udpLocalPort);
|
||||
}
|
||||
|
||||
@@ -36,6 +39,7 @@ void sendWiFi(const uint8_t *buf, int len) {
|
||||
}
|
||||
|
||||
int receiveWiFi(uint8_t *buf, int len) {
|
||||
if (WiFi.softAPgetStationNum() == 0 && !WiFi.isConnected()) return 0;
|
||||
udp.parsePacket();
|
||||
if (udp.remoteIP()) udpRemoteIP = udp.remoteIP();
|
||||
return udp.read(buf, len);
|
||||
@@ -56,10 +60,12 @@ void printWiFiInfo() {
|
||||
print("SSID: %s\n", WiFi.SSID().c_str());
|
||||
print("Password: ***\n");
|
||||
print("IP: %s\n", WiFi.localIP().toString().c_str());
|
||||
print("RSSI: %d dBm\n", WiFi.RSSI());
|
||||
} else {
|
||||
print("Mode: Disabled\n");
|
||||
return;
|
||||
}
|
||||
print("Channel: %d\n", WiFi.channel());
|
||||
print("Remote IP: %s\n", udpRemoteIP.toString().c_str());
|
||||
print("MAVLink connected: %d\n", mavlinkConnected);
|
||||
}
|
||||
|
||||
@@ -21,6 +21,8 @@
|
||||
#define degrees(rad) ((rad)*RAD_TO_DEG)
|
||||
|
||||
#define constrain(amt,low,high) ((amt)<(low)?(low):((amt)>(high)?(high):(amt)))
|
||||
template<typename T> T max(T a, T b) { return a > b ? a : b; }
|
||||
template<typename T> T min(T a, T b) { return a < b ? a : b; }
|
||||
|
||||
long map(long x, long in_min, long in_max, long out_min, long out_max) {
|
||||
const long run = in_max - in_min;
|
||||
@@ -149,7 +151,7 @@ public:
|
||||
void setRxInvert(bool invert) {};
|
||||
};
|
||||
|
||||
HardwareSerial Serial, Serial2;
|
||||
HardwareSerial Serial, Serial1, Serial2;
|
||||
|
||||
class EspClass {
|
||||
public:
|
||||
@@ -165,6 +167,8 @@ void delay(uint32_t ms) {
|
||||
|
||||
bool ledcAttach(uint8_t pin, uint32_t freq, uint8_t resolution) { return true; }
|
||||
bool ledcWrite(uint8_t pin, uint32_t duty) { return true; }
|
||||
uint32_t ledcChangeFrequency(uint8_t pin, uint32_t freq, uint8_t resolution) { return freq; }
|
||||
uint32_t analogReadMilliVolts(uint8_t pin) { return 0; }
|
||||
|
||||
unsigned long __micros;
|
||||
unsigned long __resetTime = 0;
|
||||
|
||||
@@ -13,7 +13,7 @@ class SBUS {
|
||||
public:
|
||||
SBUS(HardwareSerial& bus, const bool inv = true) {};
|
||||
SBUS(HardwareSerial& bus, const int8_t rxpin, const int8_t txpin, const bool inv = true) {};
|
||||
void begin() {};
|
||||
void begin(int rxpin = -1, int txpin = -1, bool inv = true, bool fast = false) {};
|
||||
bool read() { return joystickInit(); };
|
||||
SBUSData data() {
|
||||
SBUSData data;
|
||||
|
||||
@@ -27,11 +27,13 @@ void step();
|
||||
void computeLoopRate();
|
||||
void applyGyro();
|
||||
void applyAcc();
|
||||
void applyLevel();
|
||||
void control();
|
||||
void interpretControls();
|
||||
void controlAttitude();
|
||||
void controlRates();
|
||||
void controlTorque();
|
||||
void desaturate(float& a, float& b, float& c, float& d);
|
||||
const char* getModeName();
|
||||
void sendMotors();
|
||||
int getDutyCycle(float value);
|
||||
@@ -41,9 +43,10 @@ void print(const char* format, ...);
|
||||
void pause(float duration);
|
||||
void doCommand(String str, bool echo);
|
||||
void handleInput();
|
||||
void setupRC();
|
||||
void normalizeRC();
|
||||
void calibrateRC();
|
||||
void calibrateRCChannel(float *channel, uint16_t zero[16], uint16_t max[16], const char *str);
|
||||
void calibrateRCChannel(int*, uint16_t[16], uint16_t[16], const char*);
|
||||
void printRCCalibration();
|
||||
void printLogHeader();
|
||||
void printLogData();
|
||||
|
||||
@@ -27,6 +27,7 @@
|
||||
#include "mavlink.ino"
|
||||
#include "motors.ino"
|
||||
#include "parameters.ino"
|
||||
#include "power.ino"
|
||||
#include "rc.ino"
|
||||
#include "time.ino"
|
||||
|
||||
|
||||
@@ -1,4 +1,3 @@
|
||||
// Dummy file to make it possible to compile simulator with Flix' util.h
|
||||
|
||||
#define WRITE_PERI_REG(addr, val) {}
|
||||
#define REG_CLR_BIT(_r, _b) {}
|
||||
|
||||
@@ -10,6 +10,7 @@ print('Connected:', flix.connected)
|
||||
print('Mode:', flix.mode)
|
||||
print('Armed:', flix.armed)
|
||||
print('Landed:', flix.landed)
|
||||
print('Voltage:', flix.voltage, 'V')
|
||||
print('Rates:', *[f'{math.degrees(r):.0f}°/s' for r in flix.rates])
|
||||
print('Attitude:', *[f'{math.degrees(a):.0f}°' for a in flix.attitude_euler])
|
||||
print('Motors:', flix.motors)
|
||||
@@ -23,11 +24,11 @@ print('> imu')
|
||||
print(flix.cli('imu'))
|
||||
|
||||
print('=== Get parameter...')
|
||||
pitch_p = flix.get_param('PITCH_P')
|
||||
print('PITCH_P = ', pitch_p)
|
||||
pitch_p = flix.get_param('CTL_P_P')
|
||||
print('CTL_P_P = ', pitch_p)
|
||||
|
||||
print('=== Set parameter...')
|
||||
flix.set_param('PITCH_P', pitch_p)
|
||||
flix.set_param('CTL_P_P', pitch_p)
|
||||
|
||||
print('=== Wait for gyro update...')
|
||||
print('Gyro: ', flix.wait('gyro'))
|
||||
|
||||
@@ -24,19 +24,20 @@ pip install pyflix
|
||||
The API is accessed through the `Flix` class:
|
||||
|
||||
```python
|
||||
from flix import Flix
|
||||
from pyflix import Flix
|
||||
flix = Flix() # create a Flix object and wait for connection
|
||||
```
|
||||
|
||||
### Telemetry
|
||||
|
||||
Basic telemetry is available through object properties. The property names generally match the corresponding variables in the firmware itself:
|
||||
Basic telemetry is available through object properties. The property names generally match the corresponding variables in the firmware code:
|
||||
|
||||
```python
|
||||
print(flix.connected) # True if connected to the drone
|
||||
print(flix.mode) # current flight mode (str)
|
||||
print(flix.armed) # True if the drone is armed
|
||||
print(flix.landed) # True if the drone is landed
|
||||
print(flix.voltage) # battery voltage
|
||||
print(flix.attitude) # attitude quaternion [w, x, y, z]
|
||||
print(flix.attitude_euler) # attitude as Euler angles [roll, pitch, yaw]
|
||||
print(flix.rates) # angular rates [roll_rate, pitch_rate, yaw_rate]
|
||||
@@ -95,6 +96,7 @@ Full list of events:
|
||||
|`armed`|Armed state update|Armed state *(bool)*|
|
||||
|`mode`|Flight mode update|Flight mode *(str)*|
|
||||
|`landed`|Landed state update|Landed state *(bool)*|
|
||||
|`voltage`|Battery voltage update|Voltage *(float)*|
|
||||
|`print`|The drone prints text to the console|Text|
|
||||
|`attitude`|Attitude update|Attitude quaternion *(list)*|
|
||||
|`attitude_euler`|Attitude update|Euler angles *(list)*|
|
||||
@@ -117,8 +119,8 @@ Full list of events:
|
||||
Get and set firmware parameters using `get_param` and `set_param` methods:
|
||||
|
||||
```python
|
||||
pitch_p = flix.get_param('PITCH_P') # get parameter value
|
||||
flix.set_param('PITCH_P', 5) # set parameter value
|
||||
pitch_p = flix.get_param('CTL_P_P') # get parameter value
|
||||
flix.set_param('CTL_P_P', 5) # set parameter value
|
||||
```
|
||||
|
||||
Execute console commands using `cli` method. This method returns the command response:
|
||||
|
||||
@@ -26,6 +26,7 @@ class Flix:
|
||||
mode: str = ''
|
||||
armed: bool = False
|
||||
landed: bool = False
|
||||
voltage: float = 0
|
||||
attitude: List[float]
|
||||
attitude_euler: List[float] # roll, pitch, yaw
|
||||
rates: List[float]
|
||||
@@ -68,7 +69,7 @@ class Flix:
|
||||
self._heartbeat_thread.start()
|
||||
if wait_connection:
|
||||
self.wait('mavlink.HEARTBEAT')
|
||||
time.sleep(0.2) # give some time to receive initial state
|
||||
time.sleep(0.6) # give some time to receive initial state
|
||||
|
||||
def _init_state(self):
|
||||
self.attitude = [1, 0, 0, 0]
|
||||
@@ -138,7 +139,7 @@ class Flix:
|
||||
while True:
|
||||
try:
|
||||
msg: Optional[mavlink.MAVLink_message] = self.connection.recv_match(blocking=True)
|
||||
if msg is None:
|
||||
if msg is None or msg.get_srcSystem() != self.system_id:
|
||||
continue
|
||||
self._connected()
|
||||
msg_dict = msg.to_dict()
|
||||
@@ -185,11 +186,16 @@ class Flix:
|
||||
self._trigger('motors', self.motors)
|
||||
|
||||
if isinstance(msg, mavlink.MAVLink_scaled_imu_message):
|
||||
self.acc = self._mavlink_to_flu([msg.xacc / 1000, msg.yacc / 1000, msg.zacc / 1000])
|
||||
ONE_G = 9.80665
|
||||
self.acc = self._mavlink_to_flu([msg.xacc * ONE_G / 1000, msg.yacc * ONE_G / 1000, msg.zacc * ONE_G / 1000])
|
||||
self.gyro = self._mavlink_to_flu([msg.xgyro / 1000, msg.ygyro / 1000, msg.zgyro / 1000])
|
||||
self._trigger('acc', self.acc)
|
||||
self._trigger('gyro', self.gyro)
|
||||
|
||||
if isinstance(msg, mavlink.MAVLink_battery_status_message):
|
||||
self.voltage = msg.voltages[0] / 1000
|
||||
self._trigger('voltage', self.voltage)
|
||||
|
||||
if isinstance(msg, mavlink.MAVLink_serial_control_message):
|
||||
# new chunk of data
|
||||
text = bytes(msg.data)[:msg.count].decode('utf-8', errors='ignore')
|
||||
|
||||
@@ -1,6 +1,6 @@
|
||||
[project]
|
||||
name = "pyflix"
|
||||
version = "0.11"
|
||||
version = "0.14"
|
||||
description = "Python API for Flix drone"
|
||||
authors = [{ name="Oleg Kalachev", email="okalachev@gmail.com" }]
|
||||
license = "MIT"
|
||||
|
||||