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https://github.com/okalachev/flix.git
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1 Commits
| Author | SHA1 | Date | |
|---|---|---|---|
| b235825f3d |
@@ -25,8 +25,6 @@ jobs:
|
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path: flix/build
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- name: Build firmware for ESP32-S3
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run: make BOARD=esp32:esp32:esp32s3
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- name: Build firmware for ESP32-C3
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run: make BOARD=esp32:esp32:esp32c3
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- name: Check c_cpp_properties.json
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run: tools/check_c_cpp_properties.py
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@@ -1,5 +1,6 @@
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BOARD = esp32:esp32:d1_mini32
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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*))
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PORT := $(wildcard /dev/serial/by-id/usb-Silicon_Labs_CP21* /dev/serial/by-id/usb-1a86_USB_Single_Serial_* /dev/cu.usbserial-*)
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PORT := $(strip $(PORT))
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build: .dependencies
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arduino-cli compile --fqbn $(BOARD) flix
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@@ -53,7 +53,7 @@ The simulator is implemented using Gazebo and runs the original Arduino code:
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<img src="docs/img/simulator1.png" width=500 alt="Flix simulator">
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## Documentation articles
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## Documentation
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1. [Assembly instructions](docs/assembly.md).
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2. [Usage: build, setup and flight](docs/usage.md).
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@@ -75,10 +75,10 @@ Additional articles:
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|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|
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|Boost converter (optional, for more stable power supply)|5V output|<img src="docs/img/buck-boost.jpg" width=100>|1|
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|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|
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|Propeller|55 mm or 65 mm|<img src="docs/img/prop.jpg" width=100>|4|
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|Propeller|55 mm (alternatively 65 mm)|<img src="docs/img/prop.jpg" width=100>|4|
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|MOSFET (transistor)|100N03A or [analog](https://t.me/opensourcequadcopter/33)|<img src="docs/img/100n03a.jpg" width=100>|4|
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|Pull-down resistor<br>Voltage measurement resistor|10 kΩ|<img src="docs/img/resistor10k.jpg" width=100>|6|
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|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|
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|Pull-down resistor|10 kΩ|<img src="docs/img/resistor10k.jpg" width=100>|4|
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|3.7V Li-Po battery|LW 952540 (or any compatible by the size)|<img src="docs/img/battery.jpg" width=100>|1|
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|Battery connector cable|MX2.0 2P female|<img src="docs/img/mx.png" width=100>|1|
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|Li-Po Battery charger|Any|<img src="docs/img/charger.jpg" width=100>|1|
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|Screws for IMU board mounting|M3x5|<img src="docs/img/screw-m3.jpg" width=100>|2|
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@@ -154,12 +154,10 @@ You can see a user-contributed [variant of complete circuit diagram](https://mir
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|VIN|VCC (or 3.3V depending on the receiver)|
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|Signal (TX)|GPIO4¹|
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*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.*
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*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.*
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* Optionally connect the battery voltage divider for voltage monitoring to any ADC1 pin (e. g. *GPIO32* on ESP32, *GPIO3* on ESP32S3).
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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.
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## Resources
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* Telegram channel on developing the drone and the flight controller (in Russian): https://t.me/opensourcequadcopter.
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@@ -28,8 +28,6 @@ Soldered components ([schematics variant](https://miro.com/app/board/uXjVN-dTjoo
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<img src="img/assembly/7.jpg" width=600>
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See an alternative assembly process photos here: https://drive.google.com/drive/folders/1FG5BH9RCzdf1XmJcC70PymiRMXcz6Fx7?usp=sharing.
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## Motor directions
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> [!WARNING]
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+7
-13
@@ -12,25 +12,20 @@ Do the following:
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Do the following:
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* **Check the battery voltage**. Use a multimeter to measure the battery voltage. The fully charged battery should have about 4.2V.
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* **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).
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* **Check the battery voltage**. Use a multimeter to measure the battery voltage. It should be in range of 3.7-4.2 V.
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* **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.
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* **Check the baudrate is correct**. If you see garbage characters in the Serial Monitor, make sure the baudrate is set to 115200.
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* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
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* **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)*.
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* **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**.
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* **If QGroundControl doesn't connect**, you might need to disable the firewall and/or VPN on your computer.
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* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
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* **Check the IMU is working**. Perform `imu` command and check its output:
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* The `status` field should be `OK`.
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* The `rate` field should be about 1000 (Hz).
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* The `accel` and `gyro` fields should change as you move the drone.
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* **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).
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* **Calibrate the accelerometer.** if is wasn't done before. Type `ca` command in Serial Monitor and follow the instructions.
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* **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:
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<a href="https://youtu.be/yVRN23-GISU"><img width=200 src="https://i3.ytimg.com/vi/yVRN23-GISU/maxresdefault.jpg"></a>
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* **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.
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* **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.
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* **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).
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* **Check the motors type**. Motors with exact 3.7V voltage are needed, not ranged working voltage (3.7V — 6V).
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* **Check the motors**. Perform the following commands using Serial Monitor:
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* `mfr` — should rotate front right motor (counter-clockwise).
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@@ -38,10 +33,9 @@ Do the following:
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* `mrl` — should rotate rear left motor (counter-clockwise).
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* `mrr` — should rotate rear right motor (clockwise).
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* **Check the propeller directions are correct**. Make sure your propeller types (A or B) are installed as on the picture:
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<img src="img/user/peter_ukhov-2/1.jpg" width="200">
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* **If using an SBUS receiver**:
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* **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.
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* **If using SBUS receiver**:
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* **Define the used GPIO pin** in `RC_RX_PIN` parameter.
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* **Calibrate the RC** using `cr` command in the console.
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* **Check the controls** using `rc` command. All the controls should change between -1 and 1, and the throttle between 0 and 1.
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* **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.
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+8
-10
@@ -112,9 +112,9 @@ You can also work with parameters using `p` command in the console. Parameter na
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### Define IMU orientation
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The IMU orientation (relative to the drone's axes) is defined using the parameters: `IMU_ROT_ROLL`, `IMU_ROT_PITCH`, and `IMU_ROT_YAW`.
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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`.
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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:
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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:
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<img src="img/imu-axes.png" width="200">
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@@ -122,10 +122,10 @@ Use the following table to set the parameters for common IMU orientations:
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|Orientation|Parameters|Orientation|Parameters|
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|:-:|-|-|-|
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|<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|
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|<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|
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|<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|
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|<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|
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|<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|
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|<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|
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|<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|
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|<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|
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### Calibrate accelerometer
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@@ -138,8 +138,6 @@ Before flight you need to calibrate the accelerometer:
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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).
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|
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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.
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If using brushless motors and ESCs:
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1. Set the appropriate PWM using the parameters: `MOT_PWM_STOP`, `MOT_PWM_MIN`, and `MOT_PWM_MAX` (1000, 1000, and 2000 is typical).
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@@ -247,7 +245,7 @@ When finished flying, **disarm** the drone, moving the left stick to the bottom
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### Flight modes
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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*).
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Flight mode is changed using mode switch on the remote control (if configured) or using the console commands. The main flight mode is *STAB*.
|
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|
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#### STAB
|
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|
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@@ -268,7 +266,7 @@ In this mode, the pilot controls the angular rates. This control method is diffi
|
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|
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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.
|
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|
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If the pilot moves the control sticks and mode switch is not configured, the drone will switch back to *STAB* mode.
|
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If the pilot moves the control sticks, the drone will switch back to *STAB* mode.
|
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|
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## Wi-Fi configuration
|
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|
||||
|
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@@ -4,14 +4,6 @@ This page contains user-built drones based on the Flix project. Publish your pro
|
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|
||||
---
|
||||
|
||||
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>
|
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[Flight validation](https://drive.google.com/file/d/1yqkKNuz4R_yxGqUNQxVpixJbXqEEcUSj/view?usp=share_link).
|
||||
|
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<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>
|
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|
||||
---
|
||||
|
||||
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.
|
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|
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+1
-2
@@ -168,7 +168,6 @@ void doCommand(String str, bool echo = false) {
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print("Chip: %s\n", ESP.getChipModel());
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print("Temperature: %.1f °C\n", temperatureRead());
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print("Free heap: %d\n", ESP.getFreeHeap());
|
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print("Firmware: " __DATE__ " " __TIME__ "\n");
|
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// Print tasks table
|
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print("Num Task Stack Prio Core CPU%%\n");
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int taskCount = uxTaskGetNumberOfTasks();
|
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@@ -179,7 +178,7 @@ void doCommand(String str, bool echo = false) {
|
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String core = systemState[i].xCoreID == tskNO_AFFINITY ? "*" : String(systemState[i].xCoreID);
|
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int cpuPercentage = systemState[i].ulRunTimeCounter / (totalRunTime / 100);
|
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print("%-5d%-20s%-7d%-6d%-6s%d\n",systemState[i].xTaskNumber, systemState[i].pcTaskName,
|
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systemState[i].usStackHighWaterMark, systemState[i].uxCurrentPriority, core.c_str(), cpuPercentage);
|
||||
systemState[i].usStackHighWaterMark, systemState[i].uxCurrentPriority, core, cpuPercentage);
|
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}
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delete[] systemState;
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#endif
|
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||||
+1
-14
@@ -67,7 +67,7 @@ void control() {
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|
||||
void interpretControls() {
|
||||
if (controlMode < 0.25) mode = flightModes[0];
|
||||
else if (controlMode <= 0.75) mode = flightModes[1];
|
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else if (controlMode < 0.75) mode = flightModes[1];
|
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else if (controlMode > 0.75) mode = flightModes[2];
|
||||
|
||||
if (mode == AUTO) return; // pilot is not effective in AUTO mode
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@@ -149,25 +149,12 @@ void controlTorque() {
|
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motors[MOTOR_REAR_LEFT] = thrustTarget + torqueTarget.x + torqueTarget.y - torqueTarget.z;
|
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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);
|
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motors[1] = constrain(motors[1], 0, 1);
|
||||
motors[2] = constrain(motors[2], 0, 1);
|
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motors[3] = constrain(motors[3], 0, 1);
|
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}
|
||||
|
||||
void desaturate(float& a, float& b, float& c, float& d) {
|
||||
float maxThrust = max(max(a, b), max(c, d));
|
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if (maxThrust > 1) {
|
||||
float diff = maxThrust - 1;
|
||||
a -= diff;
|
||||
b -= diff;
|
||||
c -= diff;
|
||||
d -= diff;
|
||||
}
|
||||
}
|
||||
|
||||
const char* getModeName() {
|
||||
switch (mode) {
|
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case RAW: return "RAW";
|
||||
|
||||
@@ -13,13 +13,11 @@ 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() {
|
||||
@@ -44,12 +42,3 @@ 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));
|
||||
}
|
||||
|
||||
+1
-1
@@ -18,8 +18,8 @@ extern float motors[4];
|
||||
void setup() {
|
||||
Serial.begin(115200);
|
||||
print("Initializing flix\n");
|
||||
disableBrownOut();
|
||||
setupParameters();
|
||||
setupPower();
|
||||
setupLED();
|
||||
setLED(true);
|
||||
setupMotors();
|
||||
|
||||
+2
-2
@@ -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", gyro.x, gyro.y, gyro.z);
|
||||
print("gyro: %f %f %f\n", rates.x, rates.y, rates.z);
|
||||
print("acc: %f %f %f\n", acc.x, acc.y, acc.z);
|
||||
imu.waitForData();
|
||||
Vector rawGyro, rawAcc;
|
||||
|
||||
+1
-1
@@ -65,7 +65,7 @@ void sendMavlink() {
|
||||
sendMessage(&msg);
|
||||
|
||||
mavlink_msg_scaled_imu_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, time,
|
||||
acc.x / ONE_G * 1000, -acc.y / ONE_G * 1000, -acc.z / ONE_G * 1000, // convert to frd
|
||||
acc.x * 1000, -acc.y * 1000, -acc.z * 1000, // convert to frd
|
||||
gyro.x * 1000, -gyro.y * 1000, -gyro.z * 1000,
|
||||
0, 0, 0, 0);
|
||||
sendMessage(&msg);
|
||||
|
||||
+1
-1
@@ -54,7 +54,7 @@ bool motorsActive() {
|
||||
|
||||
void testMotor(int n) {
|
||||
print("Testing motor %d\n", n);
|
||||
motors[n] = 0.2;
|
||||
motors[n] = 1;
|
||||
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);
|
||||
|
||||
+2
-6
@@ -36,16 +36,13 @@ 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},
|
||||
@@ -73,7 +70,6 @@ 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], setupMotors},
|
||||
@@ -110,8 +106,8 @@ Parameter parameters[] = {
|
||||
{"RC_MODE", &modeChannel},
|
||||
// wifi
|
||||
{"WIFI_MODE", &wifiMode},
|
||||
{"WIFI_PORT_LOC", &udpLocalPort},
|
||||
{"WIFI_PORT_REM", &udpRemotePort},
|
||||
{"WIFI_LOC_PORT", &udpLocalPort},
|
||||
{"WIFI_REM_PORT", &udpRemotePort},
|
||||
// mavlink
|
||||
{"MAV_SYS_ID", &mavlinkSysId},
|
||||
{"MAV_RATE_SLOW", &telemetrySlow.rate},
|
||||
|
||||
@@ -3,8 +3,6 @@
|
||||
|
||||
// Power management
|
||||
|
||||
#include <soc/soc.h>
|
||||
#include <soc/rtc_cntl_reg.h>
|
||||
#include "lpf.h"
|
||||
#include "util.h"
|
||||
|
||||
@@ -13,11 +11,6 @@ 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);
|
||||
|
||||
+1
-1
@@ -6,7 +6,7 @@
|
||||
#include <SBUS.h>
|
||||
#include "util.h"
|
||||
|
||||
SBUS rc(Serial1);
|
||||
SBUS rc(Serial2);
|
||||
int rcRxPin = -1; // -1 means disabled
|
||||
|
||||
uint16_t channels[16]; // raw rc channels
|
||||
|
||||
+2
-2
@@ -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 and mode switch is not configured
|
||||
if (mode == AUTO && invalid(controlMode)) mode = STAB; // regain control by the pilot
|
||||
// controls changed
|
||||
if (mode == AUTO) mode = STAB; // regain control by the pilot
|
||||
}
|
||||
roll = controlRoll;
|
||||
pitch = controlPitch;
|
||||
|
||||
@@ -6,6 +6,8 @@
|
||||
#pragma once
|
||||
|
||||
#include <math.h>
|
||||
#include <soc/soc.h>
|
||||
#include <soc/rtc_cntl_reg.h>
|
||||
|
||||
const float ONE_G = 9.80665;
|
||||
extern float t;
|
||||
@@ -33,6 +35,11 @@ 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();
|
||||
|
||||
+3
-16
@@ -105,23 +105,10 @@ 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.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;
|
||||
if (direction.zero()) {
|
||||
// vectors are opposite, return any perpendicular vector
|
||||
return cross(a, Vector(1, 0, 0));
|
||||
}
|
||||
direction.normalize();
|
||||
float angle = angleBetween(a, b);
|
||||
|
||||
@@ -25,7 +25,6 @@ void setupWiFi() {
|
||||
} else if (wifiMode == W_STA) {
|
||||
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);
|
||||
}
|
||||
|
||||
|
||||
+1
-3
@@ -21,8 +21,6 @@
|
||||
#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;
|
||||
@@ -151,7 +149,7 @@ public:
|
||||
void setRxInvert(bool invert) {};
|
||||
};
|
||||
|
||||
HardwareSerial Serial, Serial1, Serial2;
|
||||
HardwareSerial Serial, Serial2;
|
||||
|
||||
class EspClass {
|
||||
public:
|
||||
|
||||
@@ -27,13 +27,11 @@ 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);
|
||||
|
||||
@@ -1,3 +1,4 @@
|
||||
// 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) {}
|
||||
|
||||
@@ -24,13 +24,13 @@ pip install pyflix
|
||||
The API is accessed through the `Flix` class:
|
||||
|
||||
```python
|
||||
from pyflix import Flix
|
||||
from flix 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 code:
|
||||
Basic telemetry is available through object properties. The property names generally match the corresponding variables in the firmware itself:
|
||||
|
||||
```python
|
||||
print(flix.connected) # True if connected to the drone
|
||||
|
||||
@@ -186,8 +186,7 @@ class Flix:
|
||||
self._trigger('motors', self.motors)
|
||||
|
||||
if isinstance(msg, mavlink.MAVLink_scaled_imu_message):
|
||||
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.acc = self._mavlink_to_flu([msg.xacc / 1000, msg.yacc / 1000, msg.zacc / 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)
|
||||
|
||||
@@ -1,6 +1,6 @@
|
||||
[project]
|
||||
name = "pyflix"
|
||||
version = "0.14"
|
||||
version = "0.11"
|
||||
description = "Python API for Flix drone"
|
||||
authors = [{ name="Oleg Kalachev", email="okalachev@gmail.com" }]
|
||||
license = "MIT"
|
||||
|
||||
Reference in New Issue
Block a user