Compare commits
16 Commits
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cpp
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6725f1d3de |
@@ -65,5 +65,6 @@
|
||||
"PX4"
|
||||
]
|
||||
},
|
||||
"MD045": false
|
||||
"MD045": false,
|
||||
"MD060": false
|
||||
}
|
||||
|
||||
45
.vscode/c_cpp_properties.json
vendored
@@ -18,20 +18,7 @@
|
||||
"forcedInclude": [
|
||||
"${workspaceFolder}/.vscode/intellisense.h",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
|
||||
"${workspaceFolder}/flix/cli.ino",
|
||||
"${workspaceFolder}/flix/control.ino",
|
||||
"${workspaceFolder}/flix/estimate.ino",
|
||||
"${workspaceFolder}/flix/flix.ino",
|
||||
"${workspaceFolder}/flix/imu.ino",
|
||||
"${workspaceFolder}/flix/led.ino",
|
||||
"${workspaceFolder}/flix/log.ino",
|
||||
"${workspaceFolder}/flix/mavlink.ino",
|
||||
"${workspaceFolder}/flix/motors.ino",
|
||||
"${workspaceFolder}/flix/rc.ino",
|
||||
"${workspaceFolder}/flix/time.ino",
|
||||
"${workspaceFolder}/flix/wifi.ino",
|
||||
"${workspaceFolder}/flix/parameters.ino"
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h"
|
||||
],
|
||||
"compilerPath": "~/.arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++",
|
||||
"cStandard": "c11",
|
||||
@@ -65,20 +52,7 @@
|
||||
"forcedInclude": [
|
||||
"${workspaceFolder}/.vscode/intellisense.h",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
|
||||
"${workspaceFolder}/flix/flix.ino",
|
||||
"${workspaceFolder}/flix/cli.ino",
|
||||
"${workspaceFolder}/flix/control.ino",
|
||||
"${workspaceFolder}/flix/estimate.ino",
|
||||
"${workspaceFolder}/flix/imu.ino",
|
||||
"${workspaceFolder}/flix/led.ino",
|
||||
"${workspaceFolder}/flix/log.ino",
|
||||
"${workspaceFolder}/flix/mavlink.ino",
|
||||
"${workspaceFolder}/flix/motors.ino",
|
||||
"${workspaceFolder}/flix/rc.ino",
|
||||
"${workspaceFolder}/flix/time.ino",
|
||||
"${workspaceFolder}/flix/wifi.ino",
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||||
"${workspaceFolder}/flix/parameters.ino"
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h"
|
||||
],
|
||||
"compilerPath": "~/Library/Arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++",
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||||
"cStandard": "c11",
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@@ -113,20 +87,7 @@
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"forcedInclude": [
|
||||
"${workspaceFolder}/.vscode/intellisense.h",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
|
||||
"${workspaceFolder}/flix/cli.ino",
|
||||
"${workspaceFolder}/flix/control.ino",
|
||||
"${workspaceFolder}/flix/estimate.ino",
|
||||
"${workspaceFolder}/flix/flix.ino",
|
||||
"${workspaceFolder}/flix/imu.ino",
|
||||
"${workspaceFolder}/flix/led.ino",
|
||||
"${workspaceFolder}/flix/log.ino",
|
||||
"${workspaceFolder}/flix/mavlink.ino",
|
||||
"${workspaceFolder}/flix/motors.ino",
|
||||
"${workspaceFolder}/flix/rc.ino",
|
||||
"${workspaceFolder}/flix/time.ino",
|
||||
"${workspaceFolder}/flix/wifi.ino",
|
||||
"${workspaceFolder}/flix/parameters.ino"
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h"
|
||||
],
|
||||
"compilerPath": "~/AppData/Local/Arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++.exe",
|
||||
"cStandard": "c11",
|
||||
|
||||
@@ -1,6 +1,9 @@
|
||||
# Flix
|
||||
<!-- markdownlint-disable MD041 -->
|
||||
|
||||
**Flix** (*flight + X*) — open source ESP32-based quadcopter made from scratch.
|
||||
<p align="center">
|
||||
<img src="docs/img/flix.svg" width=180 alt="Flix logo"><br>
|
||||
<b>Flix</b> (<i>flight + X</i>) — open source ESP32-based quadcopter made from scratch.
|
||||
</p>
|
||||
|
||||
<table>
|
||||
<tr>
|
||||
|
||||
@@ -35,7 +35,7 @@
|
||||
|
||||
### Подсистема управления
|
||||
|
||||
Состояние органов управления обрабатывается в функции `interpretControls()` и преобразуется в *команду управления*, которая включает следующее:
|
||||
Состояние органов управления обрабатывается в функции `interpretControls()` и преобразуется в **команду управления**, которая включает следующее:
|
||||
|
||||
* `attitudeTarget` *(Quaternion)* — целевая ориентация дрона.
|
||||
* `ratesTarget` *(Vector)* — целевые угловые скорости, *рад/с*.
|
||||
|
||||
@@ -38,13 +38,13 @@ Utility files:
|
||||
|
||||
### Control subsystem
|
||||
|
||||
Pilot inputs are interpreted in `interpretControls()`, and then converted to the *control command*, which consists of the following:
|
||||
Pilot inputs are interpreted in `interpretControls()`, and then converted to the **control command**, which consists of the following:
|
||||
|
||||
* `attitudeTarget` *(Quaternion)* — target attitude of the drone.
|
||||
* `ratesTarget` *(Vector)* — target angular rates, *rad/s*.
|
||||
* `ratesExtra` *(Vector)* — additional (feed-forward) angular rates , used for yaw rate control in STAB mode, *rad/s*.
|
||||
* `torqueTarget` *(Vector)* — target torque, range [-1, 1].
|
||||
* `thrustTarget` *(float)* — collective thrust target, range [0, 1].
|
||||
* `thrustTarget` *(float)* — collective motor thrust target, range [0, 1].
|
||||
|
||||
Control command is handled in `controlAttitude()`, `controlRates()`, `controlTorque()` functions. Each function may be skipped if the corresponding control target is set to `NAN`.
|
||||
|
||||
@@ -62,6 +62,11 @@ print("Test value: %.2f\n", testValue);
|
||||
|
||||
In order to add a console command, modify the `doCommand()` function in `cli.ino` file.
|
||||
|
||||
> [!IMPORTANT]
|
||||
> Avoid using delays in in-flight commands, it will **crash** the drone! (The design is one-threaded.)
|
||||
>
|
||||
> For on-the-ground commands, use `pause()` function, instead of `delay()`. This function allows to pause in a way that MAVLink connection will continue working.
|
||||
|
||||
## Building the firmware
|
||||
|
||||
See build instructions in [usage.md](usage.md).
|
||||
|
||||
38
docs/img/flix.svg
Normal file
@@ -0,0 +1,38 @@
|
||||
<svg xmlns="http://www.w3.org/2000/svg" viewBox="0 0 734.86 378.46">
|
||||
<defs>
|
||||
<style>
|
||||
.a {
|
||||
fill: none;
|
||||
stroke: #d5d5d5;
|
||||
stroke-miterlimit: 10;
|
||||
stroke-width: 31px;
|
||||
}
|
||||
|
||||
.b {
|
||||
fill: #c1c1c1;
|
||||
}
|
||||
|
||||
.c {
|
||||
fill: #ff9400;
|
||||
}
|
||||
|
||||
.d {
|
||||
fill: #d5d5d5;
|
||||
}
|
||||
</style>
|
||||
</defs>
|
||||
<g>
|
||||
<g>
|
||||
<line class="a" x1="448.78" y1="294.23" x2="648.77" y2="93.24"/>
|
||||
<line class="a" x1="449.78" y1="94.24" x2="649.77" y2="295.23"/>
|
||||
<circle class="b" cx="549.27" cy="193.73" r="41.5"/>
|
||||
<circle class="c" cx="449.35" cy="93.74" r="77.95"/>
|
||||
<circle class="c" cx="648.89" cy="93.53" r="77.95"/>
|
||||
<circle class="c" cx="647.89" cy="294.51" r="77.95"/>
|
||||
<circle class="c" cx="448.9" cy="294.51" r="77.95"/>
|
||||
</g>
|
||||
<path class="d" d="M8,161.93q0-17.85,22.36-17.85h4.81V100.57Q35.17,8.49,131.23,8h1q36.87,0,47.31,7.48L181,17.41l1,2.41V50q0,12.32-5.82,12.31-2.43,0-7.4-4.64t-14.19-9a48.63,48.63,0,0,0-21.22-4.41q-12,0-19.17,3.5a18.85,18.85,0,0,0-9.82,10.62,67.35,67.35,0,0,0-3.52,12.06,82.52,82.52,0,0,0-.85,13.39v60.32h27.28q10.86,0,16.05,5.43a17.52,17.52,0,0,1,5.19,12.42,22.5,22.5,0,0,1-1.21,7.36q-1.22,3.51-6.64,7.24t-14.36,3.74H101.64V344.82a56,56,0,0,1-.61,9.65,37.8,37.8,0,0,1-2.56,7.6,11.83,11.83,0,0,1-6.94,6.4q-5,1.93-13.51,1.93H57.08q-10.47,0-15.7-4.71t-5.73-8.44a77.31,77.31,0,0,1-.48-9.53V180.27H29.4Q8,180.27,8,161.93Z"/>
|
||||
<path class="d" d="M201.21,348.2V37q0-23.16,20.86-23.4h22.81q22.8,0,22.8,22.44V346.27a68.92,68.92,0,0,1-.49,9.41,22.59,22.59,0,0,1-2.42,7.12,11.48,11.48,0,0,1-6.67,5.43,47.78,47.78,0,0,1-12.74,2.17H225q-11.4,0-17.58-4.47T201.21,348.2Z"/>
|
||||
<path class="d" d="M284.9,61.08V36.47a40.39,40.39,0,0,1,1.7-12.91,11.36,11.36,0,0,1,6.18-7,25.27,25.27,0,0,1,6.68-2.3c1.45-.15,4-.4,7.76-.72h25.23q10.43,0,16.73,4.7t6.31,18.22V62.05a27.94,27.94,0,0,1-.85,7.11,23,23,0,0,1-2.06,5.43,20,20,0,0,1-2.91,4,10,10,0,0,1-3.52,2.54c-1.21.48-2.54,1-4,1.44a11.53,11.53,0,0,1-3.4.73,13.71,13.71,0,0,0-3.15.48H307.7q-10.43,0-16.61-4.7T284.9,61.08Zm1.94,284.71V166.28q0-22.2,21.83-22.2h20.38q10.92,0,16.62,4t6.67,8.45a60.47,60.47,0,0,1,1,12.18V348.2q0,22.2-21.83,22.2H308.67q-10.43,0-15.64-4.95t-5.7-8.81A90.93,90.93,0,0,1,286.84,345.79Z"/>
|
||||
</g>
|
||||
</svg>
|
||||
|
After Width: | Height: | Size: 2.2 KiB |
BIN
docs/img/imu-axes.png
Normal file
|
After Width: | Height: | Size: 23 KiB |
BIN
docs/img/imu-rot-1.png
Normal file
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After Width: | Height: | Size: 18 KiB |
BIN
docs/img/imu-rot-2.png
Normal file
|
After Width: | Height: | Size: 18 KiB |
BIN
docs/img/imu-rot-3.png
Normal file
|
After Width: | Height: | Size: 17 KiB |
BIN
docs/img/imu-rot-4.png
Normal file
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After Width: | Height: | Size: 17 KiB |
BIN
docs/img/imu-rot-5.png
Normal file
|
After Width: | Height: | Size: 10 KiB |
BIN
docs/img/imu-rot-6.png
Normal file
|
After Width: | Height: | Size: 9.6 KiB |
BIN
docs/img/imu-rot-7.png
Normal file
|
After Width: | Height: | Size: 10 KiB |
BIN
docs/img/imu-rot-8.png
Normal file
|
After Width: | Height: | Size: 10 KiB |
@@ -4,7 +4,7 @@
|
||||
|
||||
Do the following:
|
||||
|
||||
* **Check ESP32 core is installed**. Check if the version matches the one used in the [tutorial](usage.md#firmware).
|
||||
* **Check ESP32 core is installed**. Check if the version matches the one used in the [tutorial](usage.md#building-the-firmware).
|
||||
* **Check libraries**. Install all the required libraries from the tutorial. Make sure there are no MPU9250 or other peripherals libraries that may conflict with the ones used in the tutorial.
|
||||
* **Check the chosen board**. The correct board to choose in Arduino IDE for ESP32 Mini is *WEMOS D1 MINI ESP32*.
|
||||
|
||||
@@ -25,7 +25,7 @@ Do the following:
|
||||
* 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, make sure `rotateIMU` function is defined correctly in `imu.ino` file.
|
||||
* **Check the IMU orientation is set correctly**. If the attitude estimation is rotated, set the correct IMU orientation as described in the [tutorial](usage.md#define-imu-orientation).
|
||||
* **Check the 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).
|
||||
|
||||
@@ -73,14 +73,6 @@ ICM20948 imu(SPI); // For ICM-20948
|
||||
MPU6050 imu(Wire); // For MPU-6050
|
||||
```
|
||||
|
||||
### Setup the IMU orientation
|
||||
|
||||
The IMU orientation is defined in `rotateIMU` function in the `imu.ino` file. Change it so it converts the IMU axes to the drone's axes correctly. **Drone axes are X forward, Y left, Z up**:
|
||||
|
||||
<img src="img/drone-axes.svg" width="200">
|
||||
|
||||
See various [IMU boards axes orientations table](https://github.com/okalachev/flixperiph/?tab=readme-ov-file#imu-axes-orientation) to help you set up the correct orientation.
|
||||
|
||||
### Connect using QGroundControl
|
||||
|
||||
QGroundControl is a ground control station software that can be used to monitor and control the drone.
|
||||
@@ -88,7 +80,7 @@ QGroundControl is a ground control station software that can be used to monitor
|
||||
1. Install mobile or desktop version of [QGroundControl](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html).
|
||||
2. Power up the drone.
|
||||
3. Connect your computer or smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
|
||||
4. Launch QGroundControl app. It should connect and begin showing the drone's telemetry automatically
|
||||
4. Launch QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
|
||||
|
||||
### Access console
|
||||
|
||||
@@ -104,11 +96,37 @@ To access the console using QGroundControl:
|
||||
|
||||
1. Connect to the drone using QGroundControl app.
|
||||
2. Go to the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Analyze Tools* ⇒ *MAVLink Console*.
|
||||
<img src="img/cli.png" width="400">
|
||||
|
||||
<img src="img/cli.png" width="400">
|
||||
|
||||
> [!TIP]
|
||||
> Use `help` command to see the list of available commands.
|
||||
|
||||
### Access parameters
|
||||
|
||||
The drone is configured using parameters. To access and modify them, go to the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Parameters*:
|
||||
|
||||
<img src="img/parameters.png" width="400">
|
||||
|
||||
You can also work with parameters using `p` command in the console.
|
||||
|
||||
### Define IMU orientation
|
||||
|
||||
Use parameters, to define the IMU board axes orientation relative to the drone's axes: `IMU_ROT_ROLL`, `IMU_ROT_PITCH`, and `IMU_ROT_YAW`.
|
||||
|
||||
The drone has *X* axis pointing forward, *Y* axis pointing left, and *Z* axis pointing up, and the supported IMU boards have *X* axis pointing to the pins side and *Z* axis pointing up from the component side:
|
||||
|
||||
<img src="img/imu-axes.png" width="200">
|
||||
|
||||
Use the following table to set the parameters for common IMU orientations:
|
||||
|
||||
|Orientation|Parameters|Orientation|Parameters|
|
||||
|:-:|-|-|-|
|
||||
|<img src="img/imu-rot-1.png" width="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|
|
||||
|
||||
### Calibrate accelerometer
|
||||
|
||||
Before flight you need to calibrate the accelerometer:
|
||||
@@ -136,6 +154,10 @@ Before flight you need to calibrate the accelerometer:
|
||||
* `mrl` — should rotate rear left motor (counter-clockwise).
|
||||
* `mrr` — should rotate rear right motor (clockwise).
|
||||
|
||||
Rotation diagram:
|
||||
|
||||
<img src="img/motors.svg" width=200>
|
||||
|
||||
> [!WARNING]
|
||||
> Never run the motors when powering the drone from USB, always use the battery for that.
|
||||
|
||||
@@ -143,7 +165,7 @@ Before flight you need to calibrate the accelerometer:
|
||||
|
||||
There are several ways to control the drone's flight: using **smartphone** (Wi-Fi), using **SBUS remote control**, or using **USB remote control** (Wi-Fi).
|
||||
|
||||
### Control with smartphone
|
||||
### Control with a smartphone
|
||||
|
||||
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone.
|
||||
2. Power the drone using the battery.
|
||||
@@ -155,7 +177,7 @@ There are several ways to control the drone's flight: using **smartphone** (Wi-F
|
||||
> [!TIP]
|
||||
> Decrease `CTL_TILT_MAX` parameter when flying using the smartphone to make the controls less sensitive.
|
||||
|
||||
### Control with remote control
|
||||
### Control with a remote control
|
||||
|
||||
Before using remote SBUS-connected remote control, you need to calibrate it:
|
||||
|
||||
@@ -163,7 +185,7 @@ Before using remote SBUS-connected remote control, you need to calibrate it:
|
||||
2. Type `cr` command and follow the instructions.
|
||||
3. Use the remote control to fly the drone!
|
||||
|
||||
### Control with USB remote control
|
||||
### Control with a USB remote control
|
||||
|
||||
If your drone doesn't have RC receiver installed, you can use USB remote control and QGroundControl app to fly it.
|
||||
|
||||
@@ -221,12 +243,6 @@ In this mode, the pilot inputs are ignored (except the mode switch, if configure
|
||||
|
||||
If the pilot moves the control sticks, the drone will switch back to *STAB* mode.
|
||||
|
||||
## Adjusting parameters
|
||||
|
||||
You can adjust some of the drone's parameters (include PID coefficients) in QGroundControl. In order to do that, go to the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Parameters*.
|
||||
|
||||
<img src="img/parameters.png" width="400">
|
||||
|
||||
## Flight log
|
||||
|
||||
After the flight, you can download the flight log for analysis wirelessly. Use the following for that:
|
||||
|
||||
@@ -16,7 +16,7 @@ Author: [goldarte](https://t.me/goldarte).<br>
|
||||
|
||||
## School 548 course
|
||||
|
||||
Special quadcopter design and engineering course took place in october-november 2025 in School 548, Moscow. Course included UAV control theory, electronics, and practical drone assembly and setup using the Flix project.
|
||||
Special course on quadcopter design and engineering took place in october-november 2025 in School 548, Moscow. The course included UAV control theory, electronics, drone assembly and setup practice, using the Flix project.
|
||||
|
||||
<img height=200 src="img/user/school548/1.jpg"> <img height=200 src="img/user/school548/2.jpg"> <img height=200 src="img/user/school548/3.jpg">
|
||||
|
||||
@@ -25,7 +25,7 @@ STL files and other materials: see [here](https://drive.google.com/drive/folders
|
||||
### Selected works
|
||||
|
||||
Author: [KiraFlux](https://t.me/@kiraflux_0XC0000005).<br>
|
||||
Description: **custom ESPNOW remote control** is implemented, firmware modified to support ESPNOW protocol.<br>
|
||||
Description: **custom ESPNOW remote control** was implemented, modified firmware to support ESPNOW protocol.<br>
|
||||
Telegram posts: [1](https://t.me/opensourcequadcopter/106), [2](https://t.me/opensourcequadcopter/114).<br>
|
||||
Modified Flix firmware: https://github.com/KiraFlux/flix/tree/klyax.<br>
|
||||
Remote control project: https://github.com/KiraFlux/ESP32-DJC.<br>
|
||||
|
||||
@@ -3,6 +3,8 @@
|
||||
|
||||
// Implementation of command line interface
|
||||
|
||||
#include <Arduino.h>
|
||||
#include "flix.h"
|
||||
#include "pid.h"
|
||||
#include "vector.h"
|
||||
#include "util.h"
|
||||
@@ -11,7 +13,7 @@ extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRO
|
||||
extern const int RAW, ACRO, STAB, AUTO;
|
||||
extern float t, dt, loopRate;
|
||||
extern uint16_t channels[16];
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
|
||||
extern float controlTime;
|
||||
extern int mode;
|
||||
extern bool armed;
|
||||
|
||||
@@ -71,7 +73,7 @@ void pause(float duration) {
|
||||
}
|
||||
}
|
||||
|
||||
void doCommand(String str, bool echo = false) {
|
||||
void doCommand(String str, bool echo) {
|
||||
// parse command
|
||||
String command, arg0, arg1;
|
||||
splitString(str, command, arg0, arg1);
|
||||
@@ -132,6 +134,7 @@ void doCommand(String str, bool echo = false) {
|
||||
}
|
||||
print("\nroll: %g pitch: %g yaw: %g throttle: %g mode: %g\n",
|
||||
controlRoll, controlPitch, controlYaw, controlThrottle, controlMode);
|
||||
print("time: %.1f\n", controlTime);
|
||||
print("mode: %s\n", getModeName());
|
||||
print("armed: %d\n", armed);
|
||||
} else if (command == "wifi") {
|
||||
55
flix/config.h
Normal file
@@ -0,0 +1,55 @@
|
||||
// Wi-Fi
|
||||
#define WIFI_ENABLED 1
|
||||
#define WIFI_SSID "flix"
|
||||
#define WIFI_PASSWORD "flixwifi"
|
||||
#define WIFI_UDP_PORT 14550
|
||||
#define WIFI_UDP_REMOTE_PORT 14550
|
||||
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
|
||||
|
||||
// Motors
|
||||
#define MOTOR_0_PIN 12 // rear left
|
||||
#define MOTOR_1_PIN 13 // rear right
|
||||
#define MOTOR_2_PIN 14 // front right
|
||||
#define MOTOR_3_PIN 15 // front left
|
||||
#define PWM_FREQUENCY 78000
|
||||
#define PWM_RESOLUTION 10
|
||||
#define PWM_STOP 0
|
||||
#define PWM_MIN 0
|
||||
#define PWM_MAX 1000000 / PWM_FREQUENCY
|
||||
|
||||
// Control
|
||||
#define PITCHRATE_P 0.05
|
||||
#define PITCHRATE_I 0.2
|
||||
#define PITCHRATE_D 0.001
|
||||
#define PITCHRATE_I_LIM 0.3
|
||||
#define ROLLRATE_P PITCHRATE_P
|
||||
#define ROLLRATE_I PITCHRATE_I
|
||||
#define ROLLRATE_D PITCHRATE_D
|
||||
#define ROLLRATE_I_LIM PITCHRATE_I_LIM
|
||||
#define YAWRATE_P 0.3
|
||||
#define YAWRATE_I 0.0
|
||||
#define YAWRATE_D 0.0
|
||||
#define YAWRATE_I_LIM 0.3
|
||||
#define ROLL_P 6
|
||||
#define ROLL_I 0
|
||||
#define ROLL_D 0
|
||||
#define PITCH_P ROLL_P
|
||||
#define PITCH_I ROLL_I
|
||||
#define PITCH_D ROLL_D
|
||||
#define YAW_P 3
|
||||
#define PITCHRATE_MAX radians(360)
|
||||
#define ROLLRATE_MAX radians(360)
|
||||
#define YAWRATE_MAX radians(300)
|
||||
#define TILT_MAX radians(30)
|
||||
#define RATES_D_LPF_ALPHA 0.2 // cutoff frequency ~ 40 Hz
|
||||
|
||||
// Estimation
|
||||
#define WEIGHT_ACC 0.003
|
||||
#define RATES_LFP_ALPHA 0.2 // cutoff frequency ~ 40 Hz
|
||||
|
||||
// MAVLink
|
||||
#define SYSTEM_ID 1
|
||||
|
||||
// Safety
|
||||
#define RC_LOSS_TIMEOUT 1
|
||||
#define DESCEND_TIME 10
|
||||
@@ -3,41 +3,25 @@
|
||||
|
||||
// Flight control
|
||||
|
||||
#include "config.h"
|
||||
#include "flix.h"
|
||||
#include "vector.h"
|
||||
#include "quaternion.h"
|
||||
#include "pid.h"
|
||||
#include "lpf.h"
|
||||
#include "util.h"
|
||||
|
||||
#define PITCHRATE_P 0.05
|
||||
#define PITCHRATE_I 0.2
|
||||
#define PITCHRATE_D 0.001
|
||||
#define PITCHRATE_I_LIM 0.3
|
||||
#define ROLLRATE_P PITCHRATE_P
|
||||
#define ROLLRATE_I PITCHRATE_I
|
||||
#define ROLLRATE_D PITCHRATE_D
|
||||
#define ROLLRATE_I_LIM PITCHRATE_I_LIM
|
||||
#define YAWRATE_P 0.3
|
||||
#define YAWRATE_I 0.0
|
||||
#define YAWRATE_D 0.0
|
||||
#define YAWRATE_I_LIM 0.3
|
||||
#define ROLL_P 6
|
||||
#define ROLL_I 0
|
||||
#define ROLL_D 0
|
||||
#define PITCH_P ROLL_P
|
||||
#define PITCH_I ROLL_I
|
||||
#define PITCH_D ROLL_D
|
||||
#define YAW_P 3
|
||||
#define PITCHRATE_MAX radians(360)
|
||||
#define ROLLRATE_MAX radians(360)
|
||||
#define YAWRATE_MAX radians(300)
|
||||
#define TILT_MAX radians(30)
|
||||
#define RATES_D_LPF_ALPHA 0.2 // cutoff frequency ~ 40 Hz
|
||||
extern const int RAW = 0, ACRO = 1, STAB = 2, AUTO = 3; // flight modes
|
||||
|
||||
const int RAW = 0, ACRO = 1, STAB = 2, AUTO = 3; // flight modes
|
||||
int mode = STAB;
|
||||
bool armed = false;
|
||||
|
||||
Quaternion attitudeTarget;
|
||||
Vector ratesTarget;
|
||||
Vector ratesExtra; // feedforward rates
|
||||
Vector torqueTarget;
|
||||
float thrustTarget;
|
||||
|
||||
PID rollRatePID(ROLLRATE_P, ROLLRATE_I, ROLLRATE_D, ROLLRATE_I_LIM, RATES_D_LPF_ALPHA);
|
||||
PID pitchRatePID(PITCHRATE_P, PITCHRATE_I, PITCHRATE_D, PITCHRATE_I_LIM, RATES_D_LPF_ALPHA);
|
||||
PID yawRatePID(YAWRATE_P, YAWRATE_I, YAWRATE_D);
|
||||
@@ -47,12 +31,6 @@ PID yawPID(YAW_P, 0, 0);
|
||||
Vector maxRate(ROLLRATE_MAX, PITCHRATE_MAX, YAWRATE_MAX);
|
||||
float tiltMax = TILT_MAX;
|
||||
|
||||
Quaternion attitudeTarget;
|
||||
Vector ratesTarget;
|
||||
Vector ratesExtra; // feedforward rates
|
||||
Vector torqueTarget;
|
||||
float thrustTarget;
|
||||
|
||||
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
|
||||
|
||||
@@ -3,13 +3,19 @@
|
||||
|
||||
// Attitude estimation from gyro and accelerometer
|
||||
|
||||
#include "config.h"
|
||||
#include "flix.h"
|
||||
#include "quaternion.h"
|
||||
#include "vector.h"
|
||||
#include "lpf.h"
|
||||
#include "util.h"
|
||||
|
||||
#define WEIGHT_ACC 0.003
|
||||
#define RATES_LFP_ALPHA 0.2 // cutoff frequency ~ 40 Hz
|
||||
Vector rates; // estimated angular rates, rad/s
|
||||
Quaternion attitude; // estimated attitude
|
||||
bool landed;
|
||||
|
||||
float accWeight = 0.003;
|
||||
LowPassFilter<Vector> ratesFilter(0.2); // cutoff frequency ~ 40 Hz
|
||||
|
||||
void estimate() {
|
||||
applyGyro();
|
||||
@@ -18,7 +24,6 @@ void estimate() {
|
||||
|
||||
void applyGyro() {
|
||||
// filter gyro to get angular rates
|
||||
static LowPassFilter<Vector> ratesFilter(RATES_LFP_ALPHA);
|
||||
rates = ratesFilter.update(gyro);
|
||||
|
||||
// apply rates to attitude
|
||||
@@ -34,7 +39,7 @@ void applyAcc() {
|
||||
|
||||
// calculate accelerometer correction
|
||||
Vector up = Quaternion::rotateVector(Vector(0, 0, 1), attitude);
|
||||
Vector correction = Vector::rotationVectorBetween(acc, up) * WEIGHT_ACC;
|
||||
Vector correction = Vector::rotationVectorBetween(acc, up) * accWeight;
|
||||
|
||||
// apply correction
|
||||
attitude = Quaternion::rotate(attitude, Quaternion::fromRotationVector(correction));
|
||||
90
flix/flix.h
Normal file
@@ -0,0 +1,90 @@
|
||||
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
|
||||
// Repository: https://github.com/okalachev/flix
|
||||
|
||||
// All-in-one header file
|
||||
|
||||
#pragma once
|
||||
|
||||
#include <Arduino.h>
|
||||
#include "vector.h"
|
||||
#include "quaternion.h"
|
||||
|
||||
extern float t, dt;
|
||||
extern float loopRate;
|
||||
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
|
||||
extern Vector gyro, acc;
|
||||
extern Vector rates;
|
||||
extern Quaternion attitude;
|
||||
extern bool landed;
|
||||
extern int mode;
|
||||
extern bool armed;
|
||||
extern Quaternion attitudeTarget;
|
||||
extern Vector ratesTarget, ratesExtra, torqueTarget;
|
||||
extern float thrustTarget;
|
||||
extern float motors[4];
|
||||
|
||||
void print(const char* format, ...);
|
||||
void pause(float duration);
|
||||
void doCommand(String str, bool echo = false);
|
||||
void handleInput();
|
||||
void control();
|
||||
void interpretControls();
|
||||
void controlAttitude();
|
||||
void controlRates();
|
||||
void controlTorque();
|
||||
const char *getModeName();
|
||||
void estimate();
|
||||
void applyGyro();
|
||||
void applyAcc();
|
||||
void setupIMU();
|
||||
void configureIMU();
|
||||
void readIMU();
|
||||
void rotateIMU(Vector& data);
|
||||
void calibrateGyroOnce();
|
||||
void calibrateAccel();
|
||||
void calibrateAccelOnce();
|
||||
void printIMUCalibration();
|
||||
void printIMUInfo();
|
||||
void setupLED();
|
||||
void setLED(bool on);
|
||||
void blinkLED();
|
||||
void prepareLogData();
|
||||
void logData();
|
||||
void printLogHeader();
|
||||
void printLogData();
|
||||
void processMavlink();
|
||||
void sendMavlink();
|
||||
void sendMessage(const void *msg);
|
||||
void receiveMavlink();
|
||||
void handleMavlink(const void *_msg);
|
||||
void mavlinkPrint(const char* str);
|
||||
void sendMavlinkPrint();
|
||||
void setupMotors();
|
||||
int getDutyCycle(float value);
|
||||
void sendMotors();
|
||||
bool motorsActive();
|
||||
void testMotor(int n);
|
||||
void setupParameters();
|
||||
int parametersCount();
|
||||
const char *getParameterName(int index);
|
||||
float getParameter(int index);
|
||||
float getParameter(const char *name);
|
||||
bool setParameter(const char *name, const float value);
|
||||
void syncParameters();
|
||||
void printParameters();
|
||||
void resetParameters();
|
||||
void setupRC();
|
||||
bool readRC();
|
||||
void normalizeRC();
|
||||
void calibrateRC();
|
||||
void calibrateRCChannel(float *channel, uint16_t in[16], uint16_t out[16], const char *str);
|
||||
void printRCCalibration();
|
||||
void failsafe();
|
||||
void rcLossFailsafe();
|
||||
void descend();
|
||||
void autoFailsafe();
|
||||
void step();
|
||||
void computeLoopRate();
|
||||
void setupWiFi();
|
||||
void sendWiFi(const uint8_t *buf, int len);
|
||||
int receiveWiFi(uint8_t *buf, int len);
|
||||
@@ -3,22 +3,11 @@
|
||||
|
||||
// Main firmware file
|
||||
|
||||
#include "config.h"
|
||||
#include "vector.h"
|
||||
#include "quaternion.h"
|
||||
#include "util.h"
|
||||
|
||||
#define WIFI_ENABLED 1
|
||||
|
||||
float t = NAN; // current step time, s
|
||||
float dt; // time delta from previous step, s
|
||||
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
|
||||
float controlMode = NAN;
|
||||
Vector gyro; // gyroscope data
|
||||
Vector acc; // accelerometer data, m/s/s
|
||||
Vector rates; // filtered angular rates, rad/s
|
||||
Quaternion attitude; // estimated attitude
|
||||
bool landed; // are we landed and stationary
|
||||
float motors[4]; // normalized motors thrust in range [0..1]
|
||||
#include "flix.h"
|
||||
|
||||
void setup() {
|
||||
Serial.begin(115200);
|
||||
|
||||
@@ -10,10 +10,14 @@
|
||||
#include "util.h"
|
||||
|
||||
MPU9250 imu(SPI);
|
||||
Vector imuRotation(0, 0, -PI / 2); // imu orientation as Euler angles
|
||||
|
||||
Vector gyro; // gyroscope output, rad/s
|
||||
Vector gyroBias;
|
||||
|
||||
Vector acc; // accelerometer output, m/s/s
|
||||
Vector accBias;
|
||||
Vector accScale(1, 1, 1);
|
||||
Vector gyroBias;
|
||||
|
||||
void setupIMU() {
|
||||
print("Setup IMU\n");
|
||||
@@ -37,24 +41,18 @@ void readIMU() {
|
||||
// apply scale and bias
|
||||
acc = (acc - accBias) / accScale;
|
||||
gyro = gyro - gyroBias;
|
||||
// rotate
|
||||
rotateIMU(acc);
|
||||
rotateIMU(gyro);
|
||||
}
|
||||
|
||||
void rotateIMU(Vector& data) {
|
||||
// Rotate from LFD to FLU
|
||||
// NOTE: In case of using other IMU orientation, change this line:
|
||||
data = Vector(data.y, data.x, -data.z);
|
||||
// Axes orientation for various boards: https://github.com/okalachev/flixperiph#imu-axes-orientation
|
||||
// rotate to body frame
|
||||
Quaternion rotation = Quaternion::fromEuler(imuRotation);
|
||||
acc = Quaternion::rotateVector(acc, rotation.inversed());
|
||||
gyro = Quaternion::rotateVector(gyro, rotation.inversed());
|
||||
}
|
||||
|
||||
void calibrateGyroOnce() {
|
||||
static Delay landedDelay(2);
|
||||
if (!landedDelay.update(landed)) return; // calibrate only if definitely stationary
|
||||
|
||||
static LowPassFilter<Vector> gyroCalibrationFilter(0.001);
|
||||
gyroBias = gyroCalibrationFilter.update(gyro);
|
||||
static LowPassFilter<Vector> gyroBiasFilter(0.001);
|
||||
gyroBias = gyroBiasFilter.update(gyro);
|
||||
}
|
||||
|
||||
void calibrateAccel() {
|
||||
@@ -3,6 +3,8 @@
|
||||
|
||||
// Board's LED control
|
||||
|
||||
#include <Arduino.h>
|
||||
|
||||
#define BLINK_PERIOD 500000
|
||||
|
||||
#ifndef LED_BUILTIN
|
||||
@@ -3,6 +3,7 @@
|
||||
|
||||
// In-RAM logging
|
||||
|
||||
#include "flix.h"
|
||||
#include "vector.h"
|
||||
#include "util.h"
|
||||
|
||||
@@ -5,6 +5,8 @@
|
||||
|
||||
#pragma once
|
||||
|
||||
#include <Arduino.h>
|
||||
|
||||
template <typename T> // Using template to make the filter usable for scalar and vector values
|
||||
class LowPassFilter {
|
||||
public:
|
||||
|
||||
@@ -3,6 +3,10 @@
|
||||
|
||||
// MAVLink communication
|
||||
|
||||
#include <Arduino.h>
|
||||
#include "config.h"
|
||||
#include "flix.h"
|
||||
|
||||
#if WIFI_ENABLED
|
||||
|
||||
#include <MAVLink.h>
|
||||
@@ -12,12 +16,13 @@
|
||||
#define MAVLINK_RATE_SLOW 1
|
||||
#define MAVLINK_RATE_FAST 10
|
||||
|
||||
extern const int AUTO, STAB;
|
||||
extern uint16_t channels[16];
|
||||
extern float controlTime;
|
||||
|
||||
bool mavlinkConnected = false;
|
||||
String mavlinkPrintBuffer;
|
||||
|
||||
extern float controlTime;
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
|
||||
|
||||
void processMavlink() {
|
||||
sendMavlink();
|
||||
receiveMavlink();
|
||||
@@ -207,6 +212,7 @@ void handleMavlink(const void *_msg) {
|
||||
armed = motors[0] > 0 || motors[1] > 0 || motors[2] > 0 || motors[3] > 0;
|
||||
}
|
||||
|
||||
/* TODO:
|
||||
if (msg.msgid == MAVLINK_MSG_ID_LOG_REQUEST_DATA) {
|
||||
mavlink_log_request_data_t m;
|
||||
mavlink_msg_log_request_data_decode(&msg, &m);
|
||||
@@ -220,6 +226,7 @@ void handleMavlink(const void *_msg) {
|
||||
sendMessage(&msg);
|
||||
}
|
||||
}
|
||||
*/
|
||||
|
||||
// Handle commands
|
||||
if (msg.msgid == MAVLINK_MSG_ID_COMMAND_LONG) {
|
||||
@@ -4,24 +4,17 @@
|
||||
// Motors output control using MOSFETs
|
||||
// In case of using ESCs, change PWM_STOP, PWM_MIN and PWM_MAX to appropriate values in μs, decrease PWM_FREQUENCY (to 400)
|
||||
|
||||
#include <Arduino.h>
|
||||
#include "config.h"
|
||||
#include "flix.h"
|
||||
#include "util.h"
|
||||
|
||||
#define MOTOR_0_PIN 12 // rear left
|
||||
#define MOTOR_1_PIN 13 // rear right
|
||||
#define MOTOR_2_PIN 14 // front right
|
||||
#define MOTOR_3_PIN 15 // front left
|
||||
float motors[4]; // normalized motor thrusts in range [0..1]
|
||||
|
||||
#define PWM_FREQUENCY 78000
|
||||
#define PWM_RESOLUTION 10
|
||||
#define PWM_STOP 0
|
||||
#define PWM_MIN 0
|
||||
#define PWM_MAX 1000000 / PWM_FREQUENCY
|
||||
|
||||
// Motors array indexes:
|
||||
const int MOTOR_REAR_LEFT = 0;
|
||||
const int MOTOR_REAR_RIGHT = 1;
|
||||
const int MOTOR_FRONT_RIGHT = 2;
|
||||
const int MOTOR_FRONT_LEFT = 3;
|
||||
extern const int MOTOR_REAR_LEFT = 0;
|
||||
extern const int MOTOR_REAR_RIGHT = 1;
|
||||
extern const int MOTOR_FRONT_RIGHT = 2;
|
||||
extern const int MOTOR_FRONT_LEFT = 3;
|
||||
|
||||
void setupMotors() {
|
||||
print("Setup Motors\n");
|
||||
@@ -4,11 +4,22 @@
|
||||
// Parameters storage in flash memory
|
||||
|
||||
#include <Preferences.h>
|
||||
#include "flix.h"
|
||||
#include "pid.h"
|
||||
#include "lpf.h"
|
||||
#include "util.h"
|
||||
|
||||
extern float channelZero[16];
|
||||
extern float channelMax[16];
|
||||
extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
|
||||
extern float tiltMax;
|
||||
extern PID rollPID, pitchPID, yawPID;
|
||||
extern PID rollRatePID, pitchRatePID, yawRatePID;
|
||||
extern Vector maxRate;
|
||||
extern Vector imuRotation;
|
||||
extern Vector accBias, accScale;
|
||||
extern float accWeight;
|
||||
extern LowPassFilter<Vector> ratesFilter;
|
||||
|
||||
Preferences storage;
|
||||
|
||||
@@ -43,12 +54,18 @@ Parameter parameters[] = {
|
||||
{"CTL_Y_RATE_MAX", &maxRate.z},
|
||||
{"CTL_TILT_MAX", &tiltMax},
|
||||
// imu
|
||||
{"IMU_ROT_ROLL", &imuRotation.x},
|
||||
{"IMU_ROT_PITCH", &imuRotation.y},
|
||||
{"IMU_ROT_YAW", &imuRotation.z},
|
||||
{"IMU_ACC_BIAS_X", &accBias.x},
|
||||
{"IMU_ACC_BIAS_Y", &accBias.y},
|
||||
{"IMU_ACC_BIAS_Z", &accBias.z},
|
||||
{"IMU_ACC_SCALE_X", &accScale.x},
|
||||
{"IMU_ACC_SCALE_Y", &accScale.y},
|
||||
{"IMU_ACC_SCALE_Z", &accScale.z},
|
||||
// estimate
|
||||
{"EST_ACC_WEIGHT", &accWeight},
|
||||
{"EST_RATES_LPF_A", &ratesFilter.alpha},
|
||||
// rc
|
||||
{"RC_ZERO_0", &channelZero[0]},
|
||||
{"RC_ZERO_1", &channelZero[1]},
|
||||
@@ -5,6 +5,8 @@
|
||||
|
||||
#pragma once
|
||||
|
||||
#include "Arduino.h"
|
||||
#include "flix.h"
|
||||
#include "lpf.h"
|
||||
|
||||
class PID {
|
||||
|
||||
@@ -5,6 +5,7 @@
|
||||
|
||||
#pragma once
|
||||
|
||||
#include <Arduino.h>
|
||||
#include "vector.h"
|
||||
|
||||
class Quaternion : public Printable {
|
||||
|
||||
@@ -6,13 +6,16 @@
|
||||
#include <SBUS.h>
|
||||
#include "util.h"
|
||||
|
||||
SBUS rc(Serial2); // NOTE: Use RC(Serial2, 16, 17) if you use the old UART2 pins
|
||||
SBUS rc(Serial2);
|
||||
|
||||
uint16_t channels[16]; // raw rc channels
|
||||
float controlTime; // time of the last controls update
|
||||
float channelZero[16]; // calibration zero values
|
||||
float channelMax[16]; // calibration max values
|
||||
|
||||
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
|
||||
float controlMode = NAN; //
|
||||
float controlTime; // time of the last controls update (0 when no RC)
|
||||
|
||||
// Channels mapping (using float to store in parameters):
|
||||
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
|
||||
|
||||
@@ -38,11 +41,11 @@ void normalizeRC() {
|
||||
controls[i] = mapf(channels[i], channelZero[i], channelMax[i], 0, 1);
|
||||
}
|
||||
// Update control values
|
||||
controlRoll = rollChannel >= 0 ? controls[(int)rollChannel] : NAN;
|
||||
controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : NAN;
|
||||
controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : NAN;
|
||||
controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : NAN;
|
||||
controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN;
|
||||
controlRoll = rollChannel >= 0 ? 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
|
||||
}
|
||||
|
||||
void calibrateRC() {
|
||||
@@ -3,11 +3,11 @@
|
||||
|
||||
// Fail-safe functions
|
||||
|
||||
#define RC_LOSS_TIMEOUT 1
|
||||
#define DESCEND_TIME 10
|
||||
#include "config.h"
|
||||
#include "flix.h"
|
||||
|
||||
extern float controlTime;
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw;
|
||||
extern const int AUTO, STAB;
|
||||
|
||||
void failsafe() {
|
||||
rcLossFailsafe();
|
||||
@@ -3,6 +3,11 @@
|
||||
|
||||
// Time related functions
|
||||
|
||||
#include "Arduino.h"
|
||||
#include "flix.h"
|
||||
|
||||
float t = NAN; // current time, s
|
||||
float dt; // time delta with the previous step, s
|
||||
float loopRate; // Hz
|
||||
|
||||
void step() {
|
||||
14
flix/util.h
@@ -8,24 +8,24 @@
|
||||
#include <math.h>
|
||||
#include <soc/soc.h>
|
||||
#include <soc/rtc_cntl_reg.h>
|
||||
#include "flix.h"
|
||||
|
||||
const float ONE_G = 9.80665;
|
||||
extern float t;
|
||||
|
||||
float mapf(float x, float in_min, float in_max, float out_min, float out_max) {
|
||||
inline float mapf(float x, float in_min, float in_max, float out_min, float out_max) {
|
||||
return (x - in_min) * (out_max - out_min) / (in_max - in_min) + out_min;
|
||||
}
|
||||
|
||||
bool invalid(float x) {
|
||||
inline bool invalid(float x) {
|
||||
return !isfinite(x);
|
||||
}
|
||||
|
||||
bool valid(float x) {
|
||||
inline bool valid(float x) {
|
||||
return isfinite(x);
|
||||
}
|
||||
|
||||
// Wrap angle to [-PI, PI)
|
||||
float wrapAngle(float angle) {
|
||||
inline float wrapAngle(float angle) {
|
||||
angle = fmodf(angle, 2 * PI);
|
||||
if (angle > PI) {
|
||||
angle -= 2 * PI;
|
||||
@@ -36,12 +36,12 @@ float wrapAngle(float angle) {
|
||||
}
|
||||
|
||||
// Disable reset on low voltage
|
||||
void disableBrownOut() {
|
||||
inline 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) {
|
||||
inline void splitString(String& str, String& token0, String& token1, String& token2) {
|
||||
str.trim();
|
||||
char chars[str.length() + 1];
|
||||
str.toCharArray(chars, str.length() + 1);
|
||||
|
||||
@@ -5,6 +5,8 @@
|
||||
|
||||
#pragma once
|
||||
|
||||
#include <Arduino.h>
|
||||
|
||||
class Vector : public Printable {
|
||||
public:
|
||||
float x, y, z;
|
||||
@@ -35,7 +37,6 @@ public:
|
||||
z = NAN;
|
||||
}
|
||||
|
||||
|
||||
float norm() const {
|
||||
return sqrt(x * x + y * y + z * z);
|
||||
}
|
||||
@@ -124,5 +125,5 @@ public:
|
||||
}
|
||||
};
|
||||
|
||||
Vector operator * (const float a, const Vector& b) { return b * a; }
|
||||
Vector operator + (const float a, const Vector& b) { return b + a; }
|
||||
inline Vector operator * (const float a, const Vector& b) { return b * a; }
|
||||
inline Vector operator + (const float a, const Vector& b) { return b + a; }
|
||||
|
||||
@@ -3,20 +3,19 @@
|
||||
|
||||
// Wi-Fi support
|
||||
|
||||
#include "config.h"
|
||||
#include "flix.h"
|
||||
|
||||
#if WIFI_ENABLED
|
||||
|
||||
#include <WiFi.h>
|
||||
#include <WiFiAP.h>
|
||||
#include <WiFiUdp.h>
|
||||
|
||||
#define WIFI_SSID "flix"
|
||||
#define WIFI_PASSWORD "flixwifi"
|
||||
#define WIFI_UDP_PORT 14550
|
||||
#define WIFI_UDP_REMOTE_PORT 14550
|
||||
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
|
||||
|
||||
WiFiUDP udp;
|
||||
|
||||
extern bool mavlinkConnected;
|
||||
|
||||
void setupWiFi() {
|
||||
print("Setup Wi-Fi\n");
|
||||
WiFi.softAP(WIFI_SSID, WIFI_PASSWORD);
|
||||
@@ -12,16 +12,15 @@
|
||||
|
||||
#define WIFI_ENABLED 1
|
||||
|
||||
float t = NAN;
|
||||
float dt;
|
||||
float motors[4];
|
||||
float controlRoll, controlPitch, controlYaw, controlThrottle = NAN;
|
||||
float controlMode = NAN;
|
||||
Vector acc;
|
||||
Vector gyro;
|
||||
Vector rates;
|
||||
Quaternion attitude;
|
||||
bool landed;
|
||||
extern float t, dt;
|
||||
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
|
||||
extern Vector rates;
|
||||
extern Quaternion attitude;
|
||||
extern bool landed;
|
||||
extern float motors[4];
|
||||
|
||||
Vector gyro, acc, imuRotation;
|
||||
Vector accBias, gyroBias, accScale(1, 1, 1);
|
||||
|
||||
// declarations
|
||||
void step();
|
||||
@@ -74,4 +73,3 @@ void calibrateAccel() { print("Skip accel calibrating\n"); };
|
||||
void printIMUCalibration() { print("cal: N/A\n"); };
|
||||
void printIMUInfo() {};
|
||||
void printWiFiInfo() {};
|
||||
Vector accBias, gyroBias, accScale(1, 1, 1);
|
||||
|
||||
@@ -95,7 +95,7 @@ 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*)|
|
||||
|`print`|The drone sends text to the console|Text|
|
||||
|`print`|The drone prints text to the console|Text|
|
||||
|`attitude`|Attitude update|Attitude quaternion (*list*)|
|
||||
|`attitude_euler`|Attitude update|Euler angles (*list*)|
|
||||
|`rates`|Angular rates update|Angular rates (*list*)|
|
||||
@@ -112,7 +112,7 @@ Full list of events:
|
||||
> [!NOTE]
|
||||
> Update events trigger on every new piece of data from the drone, and do not mean the value has changed.
|
||||
|
||||
### Common methods
|
||||
### Basic methods
|
||||
|
||||
Get and set firmware parameters using `get_param` and `set_param` methods:
|
||||
|
||||
|
||||