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27
.github/workflows/build.yml
vendored
@@ -23,10 +23,19 @@ jobs:
|
||||
with:
|
||||
name: firmware-binary
|
||||
path: flix/build
|
||||
- name: Build firmware without Wi-Fi
|
||||
- name: Build firmware for ESP32-S3
|
||||
run: make BOARD=esp32:esp32:esp32s3
|
||||
- name: Build firmware with WiFi disabled
|
||||
run: sed -i 's/^#define WIFI_ENABLED 1$/#define WIFI_ENABLED 0/' flix/flix.ino && make
|
||||
- name: Check c_cpp_properties.json
|
||||
run: tools/check_c_cpp_properties.py
|
||||
- name: Build for Black Pill F411CE (STM32)
|
||||
run: |
|
||||
arduino-cli config set board_manager.additional_urls https://github.com/stm32duino/BoardManagerFiles/raw/main/package_stmicroelectronics_index.json
|
||||
arduino-cli core install STMicroelectronics:stm32
|
||||
arduino-cli board listall STMicroelectronics:stm32
|
||||
arduino-cli lib install "Preferences"
|
||||
make BOARD=STMicroelectronics:stm32:GenF4:pnum=BLACKPILL_F411CE
|
||||
|
||||
build_macos:
|
||||
runs-on: macos-latest
|
||||
@@ -53,15 +62,25 @@ jobs:
|
||||
run: python3 tools/check_c_cpp_properties.py
|
||||
|
||||
build_simulator:
|
||||
runs-on: ubuntu-22.04
|
||||
runs-on: ubuntu-latest
|
||||
container:
|
||||
image: ubuntu:20.04
|
||||
steps:
|
||||
- name: Install dependencies
|
||||
run: |
|
||||
apt-get update
|
||||
DEBIAN_FRONTEND=noninteractive apt-get install -y curl wget build-essential cmake g++ pkg-config gnupg2 lsb-release sudo
|
||||
- name: Install Arduino CLI
|
||||
uses: arduino/setup-arduino-cli@v1.1.1
|
||||
- uses: actions/checkout@v4
|
||||
- name: Install Gazebo
|
||||
run: curl -sSL http://get.gazebosim.org | sh
|
||||
run: |
|
||||
sudo sh -c 'echo "deb http://packages.osrfoundation.org/gazebo/ubuntu-stable `lsb_release -cs` main" > /etc/apt/sources.list.d/gazebo-stable.list'
|
||||
wget https://packages.osrfoundation.org/gazebo.key -O - | sudo apt-key add -
|
||||
sudo apt-get update
|
||||
sudo apt-get install -y gazebo11 libgazebo11-dev
|
||||
- name: Install SDL2
|
||||
run: sudo apt-get install libsdl2-dev
|
||||
run: sudo apt-get install -y libsdl2-dev
|
||||
- name: Build simulator
|
||||
run: make build_simulator
|
||||
- uses: actions/upload-artifact@v4
|
||||
|
||||
9
.vscode/c_cpp_properties.json
vendored
@@ -5,13 +5,15 @@
|
||||
"includePath": [
|
||||
"${workspaceFolder}/flix",
|
||||
"${workspaceFolder}/gazebo",
|
||||
"${workspaceFolder}/tools/**",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
|
||||
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/**",
|
||||
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
|
||||
"~/Arduino/libraries/**",
|
||||
"/usr/include/**"
|
||||
"/usr/include/gazebo-11/",
|
||||
"/usr/include/ignition/math6/"
|
||||
],
|
||||
"forcedInclude": [
|
||||
"${workspaceFolder}/.vscode/intellisense.h",
|
||||
@@ -51,14 +53,14 @@
|
||||
"name": "Mac",
|
||||
"includePath": [
|
||||
"${workspaceFolder}/flix",
|
||||
// "${workspaceFolder}/gazebo",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
|
||||
"~/Library/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/include/**",
|
||||
"~/Library/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
|
||||
"~/Documents/Arduino/libraries/**",
|
||||
"/opt/homebrew/include/**"
|
||||
"/opt/homebrew/include/gazebo-11/",
|
||||
"/opt/homebrew/include/ignition/math6/"
|
||||
],
|
||||
"forcedInclude": [
|
||||
"${workspaceFolder}/.vscode/intellisense.h",
|
||||
@@ -100,6 +102,7 @@
|
||||
"includePath": [
|
||||
"${workspaceFolder}/flix",
|
||||
"${workspaceFolder}/gazebo",
|
||||
"${workspaceFolder}/tools/**",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
|
||||
|
||||
1
.vscode/settings.json
vendored
@@ -1,5 +1,6 @@
|
||||
{
|
||||
"C_Cpp.intelliSenseEngineFallback": "enabled",
|
||||
"C_Cpp.errorSquiggles": "disabled",
|
||||
"files.associations": {
|
||||
"*.sdf": "xml",
|
||||
"*.ino": "cpp",
|
||||
|
||||
28
README.md
@@ -17,11 +17,11 @@
|
||||
|
||||
* Dedicated for education and research.
|
||||
* Made from general-purpose components.
|
||||
* Simple and clean source code in Arduino.
|
||||
* Control using remote control or smartphone.
|
||||
* Precise simulation with Gazebo.
|
||||
* Simple and clean source code in Arduino (<2k lines firmware).
|
||||
* Control using USB gamepad, remote control or smartphone.
|
||||
* Wi-Fi and MAVLink support.
|
||||
* Wireless command line interface and analyzing.
|
||||
* Precise simulation with Gazebo.
|
||||
* Python library.
|
||||
* Textbook on flight control theory and practice ([in development](https://quadcopter.dev)).
|
||||
* *Position control (using external camera) and autonomous flights¹*.
|
||||
@@ -38,7 +38,11 @@ Version 0 demo video: https://youtu.be/8GzzIQ3C6DQ.
|
||||
|
||||
<a href="https://youtu.be/8GzzIQ3C6DQ"><img width=500 src="https://i3.ytimg.com/vi/8GzzIQ3C6DQ/maxresdefault.jpg"></a>
|
||||
|
||||
See the [user builds gallery](docs/user.md).
|
||||
Usage in education (RoboCamp): https://youtu.be/Wd3yaorjTx0.
|
||||
|
||||
<a href="https://youtu.be/Wd3yaorjTx0"><img width=500 src="https://i3.ytimg.com/vi/Wd3yaorjTx0/sddefault.jpg"></a>
|
||||
|
||||
See the [user builds gallery](docs/user.md):
|
||||
|
||||
<a href="docs/user.md"><img src="docs/img/user/user.jpg" width=500></a>
|
||||
|
||||
@@ -51,7 +55,7 @@ The simulator is implemented using Gazebo and runs the original Arduino code:
|
||||
## Articles
|
||||
|
||||
* [Assembly instructions](docs/assembly.md).
|
||||
* [Building and running the code](docs/build.md).
|
||||
* [Usage: build, setup and flight](docs/usage.md).
|
||||
* [Troubleshooting](docs/troubleshooting.md).
|
||||
* [Firmware architecture overview](docs/firmware.md).
|
||||
* [Python library tutorial](tools/pyflix/README.md).
|
||||
@@ -63,8 +67,8 @@ The simulator is implemented using Gazebo and runs the original Arduino code:
|
||||
|Type|Part|Image|Quantity|
|
||||
|-|-|:-:|:-:|
|
||||
|Microcontroller board|ESP32 Mini|<img src="docs/img/esp32.jpg" width=100>|1|
|
||||
|IMU (and barometer²) board|GY‑91, MPU-9265 (or other MPU‑9250/MPU‑6500 board)<br>ICM‑20948³<br>GY-521 (MPU-6050)³⁻¹|<img src="docs/img/gy-91.jpg" width=90 align=center><br><img src="docs/img/icm-20948.jpg" width=100><br><img src="docs/img/gy-521.jpg" width=100>|1|
|
||||
|<span style="background:yellow">(Recommended) Buck-boost converter</span>|To be determined, output 5V or 3.3V, see [user-contributed schematics](https://miro.com/app/board/uXjVN-dTjoo=/?moveToWidget=3458764612179508274&cot=14)|<img src="docs/img/buck-boost.jpg" width=100>|1|
|
||||
|IMU (and barometer²) 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|
|
||||
|<span style="background:yellow">Buck-boost converter</span> (recommended)|To be determined, output 5V or 3.3V, see [user-contributed schematics](https://miro.com/app/board/uXjVN-dTjoo=/?moveToWidget=3458764612179508274&cot=14)|<img src="docs/img/buck-boost.jpg" width=100>|1|
|
||||
|Motor|8520 3.7V brushed motor (shaft 0.8mm).<br>Motor with exact 3.7V voltage is needed, not ranged working voltage (3.7V — 6V).|<img src="docs/img/motor.jpeg" width=100>|4|
|
||||
|Propeller|Hubsan 55 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|
|
||||
@@ -77,16 +81,16 @@ The simulator is implemented using Gazebo and runs the original Arduino code:
|
||||
|Frame main part|3D printed⁴:<br>[`flix-frame-1.1.stl`](docs/assets/flix-frame-1.1.stl) [`flix-frame-1.1.step`](docs/assets/flix-frame-1.1.step)<br>Recommended settings: layer 0.2 mm, line 0.4 mm, infill 100%.|<img src="docs/img/frame1.jpg" width=100>|1|
|
||||
|Frame top part|3D printed:<br>[`esp32-holder.stl`](docs/assets/esp32-holder.stl) [`esp32-holder.step`](docs/assets/esp32-holder.step)|<img src="docs/img/esp32-holder.jpg" width=100>|1|
|
||||
|Washer for IMU board mounting|3D printed:<br>[`washer-m3.stl`](docs/assets/washer-m3.stl) [`washer-m3.step`](docs/assets/washer-m3.step)|<img src="docs/img/washer-m3.jpg" width=100>|2|
|
||||
|*RC transmitter (optional)*|*KINGKONG TINY X8 (warning: lacks USB support) or other⁵*|<img src="docs/img/tx.jpg" width=100>|1|
|
||||
|Controller (recommended)|CC2500 transmitter, like BetaFPV LiteRadio CC2500 (RC receiver/Wi-Fi).<br>Two-sticks gamepad (Wi-Fi only) — see [recommended gamepads](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/setup_view/joystick.html#supported-joysticks).<br>Other⁵|<img src="docs/img/betafpv.jpg" width=100><img src="docs/img/logitech.jpg" width=80>|1|
|
||||
|*RC receiver (optional)*|*DF500 or other⁵*|<img src="docs/img/rx.jpg" width=100>|1|
|
||||
|Wires|28 AWG recommended|<img src="docs/img/wire-28awg.jpg" width=100>||
|
||||
|Tape, double-sided tape||||
|
||||
|
||||
*² — barometer is not used for now.*<br>
|
||||
*³ — change `MPU9250` to `ICM20948` in `imu.ino` file if using ICM-20948 board.*<br>
|
||||
*³ — change `MPU9250` to `ICM20948` or `MPU6050` in `imu.ino` file for using the appropriate boards.*<br>
|
||||
*³⁻¹ — MPU-6050 supports I²C interface only (not recommended). To use it change IMU declaration to `MPU6050 IMU(Wire)`.*<br>
|
||||
*⁴ — this frame is optimized for GY-91 board, if using other, the board mount holes positions should be modified.*<br>
|
||||
*⁵ — you may use any transmitter-receiver pair with SBUS interface.*
|
||||
*⁵ — you also may use any transmitter-receiver pair with SBUS interface.*
|
||||
|
||||
Tools required for assembly:
|
||||
|
||||
@@ -102,7 +106,9 @@ Feel free to modify the design and or code, and create your own improved version
|
||||
|
||||
### Simplified connection diagram
|
||||
|
||||
<img src="docs/img/schematics1.svg" width=800 alt="Flix version 1 schematics">
|
||||
<img src="docs/img/schematics1.svg" width=700 alt="Flix version 1 schematics">
|
||||
|
||||
*(Dashed is optional).*
|
||||
|
||||
Motor connection scheme:
|
||||
|
||||
|
||||
@@ -1,8 +1,10 @@
|
||||
# Архитектура прошивки
|
||||
|
||||
<img src="img/dataflow.svg" width=800 alt="Firmware dataflow diagram">
|
||||
Прошивка Flix это обычный скетч Arduino, реализованный в однопоточном стиле. Код инициализации находится в функции `setup()`, а главный цикл — в функции `loop()`. Скетч состоит из нескольких файлов, каждый из которых отвечает за определенную подсистему.
|
||||
|
||||
Главный цикл работает на частоте 1000 Гц. Передача данных между подсистемами происходит через глобальные переменные:
|
||||
<img src="img/dataflow.svg" width=600 alt="Firmware dataflow diagram">
|
||||
|
||||
Главный цикл `loop()` работает на частоте 1000 Гц. Передача данных между подсистемами происходит через глобальные переменные:
|
||||
|
||||
* `t` *(float)* — текущее время шага, *с*.
|
||||
* `dt` *(float)* — дельта времени между текущим и предыдущим шагами, *с*.
|
||||
@@ -15,18 +17,34 @@
|
||||
|
||||
## Исходные файлы
|
||||
|
||||
Исходные файлы прошивки находятся в директории `flix`. Ключевые файлы:
|
||||
Исходные файлы прошивки находятся в директории `flix`. Основные файлы:
|
||||
|
||||
* [`flix.ino`](https://github.com/okalachev/flix/blob/canonical/flix/flix.ino) — основной входной файл, скетч Arduino. Включает определение глобальных переменных и главный цикл.
|
||||
* [`imu.ino`](https://github.com/okalachev/flix/blob/canonical/flix/imu.ino) — чтение данных с датчика IMU (гироскоп и акселерометр), калибровка IMU.
|
||||
* [`rc.ino`](https://github.com/okalachev/flix/blob/canonical/flix/rc.ino) — чтение данных с RC-приемника, калибровка RC.
|
||||
* [`mavlink.ino`](https://github.com/okalachev/flix/blob/canonical/flix/mavlink.ino) — взаимодействие с QGroundControl через MAVLink.
|
||||
* [`estimate.ino`](https://github.com/okalachev/flix/blob/canonical/flix/estimate.ino) — оценка ориентации дрона, комплементарный фильтр.
|
||||
* [`control.ino`](https://github.com/okalachev/flix/blob/canonical/flix/control.ino) — управление ориентацией и угловыми скоростями дрона, трехмерный двухуровневый каскадный PID-регулятор.
|
||||
* [`motors.ino`](https://github.com/okalachev/flix/blob/canonical/flix/motors.ino) — управление выходными сигналами на моторы через ШИМ.
|
||||
* [`flix.ino`](https://github.com/okalachev/flix/blob/master/flix/flix.ino) — основной файл Arduino-скетча. Определяет некоторые глобальные переменные и главный цикл.
|
||||
* [`imu.ino`](https://github.com/okalachev/flix/blob/master/flix/imu.ino) — чтение данных с датчика IMU (гироскоп и акселерометр), калибровка IMU.
|
||||
* [`rc.ino`](https://github.com/okalachev/flix/blob/master/flix/rc.ino) — чтение данных с RC-приемника, калибровка RC.
|
||||
* [`estimate.ino`](https://github.com/okalachev/flix/blob/master/flix/estimate.ino) — оценка ориентации дрона, комплементарный фильтр.
|
||||
* [`control.ino`](https://github.com/okalachev/flix/blob/master/flix/control.ino) — подсистема управления, трехмерный двухуровневый каскадный ПИД-регулятор.
|
||||
* [`motors.ino`](https://github.com/okalachev/flix/blob/master/flix/motors.ino) — выход PWM на моторы.
|
||||
* [`mavlink.ino`](https://github.com/okalachev/flix/blob/master/flix/mavlink.ino) — взаимодействие с QGroundControl или [pyflix](https://github.com/okalachev/flix/tree/master/tools/pyflix) через протокол MAVLink.
|
||||
|
||||
Вспомогательные файлы включают:
|
||||
Вспомогательные файлы:
|
||||
|
||||
* [`vector.h`](https://github.com/okalachev/flix/blob/canonical/flix/vector.h), [`quaternion.h`](https://github.com/okalachev/flix/blob/canonical/flix/quaternion.h) — реализация библиотек векторов и кватернионов проекта.
|
||||
* [`pid.h`](https://github.com/okalachev/flix/blob/canonical/flix/pid.h) — реализация общего ПИД-регулятора.
|
||||
* [`lpf.h`](https://github.com/okalachev/flix/blob/canonical/flix/lpf.h) — реализация общего фильтра нижних частот.
|
||||
* [`vector.h`](https://github.com/okalachev/flix/blob/master/flix/vector.h), [`quaternion.h`](https://github.com/okalachev/flix/blob/master/flix/quaternion.h) — библиотеки векторов и кватернионов.
|
||||
* [`pid.h`](https://github.com/okalachev/flix/blob/master/flix/pid.h) — ПИД-регулятор.
|
||||
* [`lpf.h`](https://github.com/okalachev/flix/blob/master/flix/lpf.h) — фильтр нижних частот.
|
||||
|
||||
### Подсистема управления
|
||||
|
||||
Состояние органов управления обрабатывается в функции `interpretControls()` и преобразуется в *команду управления*, которая включает следующее:
|
||||
|
||||
* `attitudeTarget` *(Quaternion)* — целевая ориентация дрона.
|
||||
* `ratesTarget` *(Vector)* — целевые угловые скорости, *рад/с*.
|
||||
* `ratesExtra` *(Vector)* — дополнительные (feed-forward) угловые скорости, для управления рысканием в режиме STAB, *рад/с*.
|
||||
* `torqueTarget` *(Vector)* — целевой крутящий момент, диапазон [-1, 1].
|
||||
* `thrustTarget` *(float)* — целевая общая тяга, диапазон [0, 1].
|
||||
|
||||
Команда управления обрабатывается в функциях `controlAttitude()`, `controlRates()`, `controlTorque()`. Если значение одной из переменных установлено в `NAN`, то соответствующая функция пропускается.
|
||||
|
||||
<img src="img/control.svg" width=300 alt="Control subsystem diagram">
|
||||
|
||||
Состояние *armed* хранится в переменной `armed`, а текущий режим — в переменной `mode`.
|
||||
|
||||
205
docs/build.md
@@ -1,205 +0,0 @@
|
||||
# Building and running
|
||||
|
||||
To build the firmware or the simulator, you need to clone the repository using git:
|
||||
|
||||
```bash
|
||||
git clone https://github.com/okalachev/flix.git
|
||||
cd flix
|
||||
```
|
||||
|
||||
## Simulation
|
||||
|
||||
### Ubuntu
|
||||
|
||||
The latest version of Ubuntu supported by Gazebo 11 simulator is 22.04. If you have a newer version, consider using a virtual machine.
|
||||
|
||||
1. Install Arduino CLI:
|
||||
|
||||
```bash
|
||||
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
|
||||
```
|
||||
|
||||
2. Install Gazebo 11:
|
||||
|
||||
```bash
|
||||
curl -sSL http://get.gazebosim.org | sh
|
||||
```
|
||||
|
||||
Set up your Gazebo environment variables:
|
||||
|
||||
```bash
|
||||
echo "source /usr/share/gazebo/setup.sh" >> ~/.bashrc
|
||||
source ~/.bashrc
|
||||
```
|
||||
|
||||
3. Install SDL2 and other dependencies:
|
||||
|
||||
```bash
|
||||
sudo apt-get update && sudo apt-get install build-essential libsdl2-dev
|
||||
```
|
||||
|
||||
4. Add your user to the `input` group to enable joystick support (you need to re-login after this command):
|
||||
|
||||
```bash
|
||||
sudo usermod -a -G input $USER
|
||||
```
|
||||
|
||||
5. Run the simulation:
|
||||
|
||||
```bash
|
||||
make simulator
|
||||
```
|
||||
|
||||
### macOS
|
||||
|
||||
1. Install Homebrew package manager, if you don't have it installed:
|
||||
|
||||
```bash
|
||||
/bin/bash -c "$(curl -fsSL https://raw.githubusercontent.com/Homebrew/install/HEAD/install.sh)"
|
||||
```
|
||||
|
||||
2. Install Arduino CLI, Gazebo 11 and SDL2:
|
||||
|
||||
```bash
|
||||
brew tap osrf/simulation
|
||||
brew install arduino-cli
|
||||
brew install gazebo11
|
||||
brew install sdl2
|
||||
```
|
||||
|
||||
Set up your Gazebo environment variables:
|
||||
|
||||
```bash
|
||||
echo "source /opt/homebrew/share/gazebo/setup.sh" >> ~/.zshrc
|
||||
source ~/.zshrc
|
||||
```
|
||||
|
||||
3. Run the simulation:
|
||||
|
||||
```bash
|
||||
make simulator
|
||||
```
|
||||
|
||||
### Setup and flight
|
||||
|
||||
#### Control with smartphone
|
||||
|
||||
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone. For **iOS**, use [QGroundControl build from TAJISOFT](https://apps.apple.com/ru/app/qgc-from-tajisoft/id1618653051).
|
||||
2. Connect your smartphone to the same Wi-Fi network as the machine running the simulator.
|
||||
3. If you're using a virtual machine, make sure that its network is set to the **bridged** mode with Wi-Fi adapter selected.
|
||||
4. Run the simulation.
|
||||
5. Open QGroundControl app. It should connect and begin showing the virtual drone's telemetry automatically.
|
||||
6. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
|
||||
7. Use the virtual joystick to fly the drone!
|
||||
|
||||
#### Control with USB remote control
|
||||
|
||||
1. Connect your USB remote control to the machine running the simulator.
|
||||
2. Run the simulation.
|
||||
3. Calibrate the RC using `cr` command in the command line interface.
|
||||
4. Run the simulation again.
|
||||
5. Use the USB remote control to fly the drone!
|
||||
|
||||
## Firmware
|
||||
|
||||
### Arduino IDE (Windows, Linux, macOS)
|
||||
|
||||
1. Install [Arduino IDE](https://www.arduino.cc/en/software) (version 2 is recommended).
|
||||
2. Windows users might need to install [USB to UART bridge driver from Silicon Labs](https://www.silabs.com/developers/usb-to-uart-bridge-vcp-drivers).
|
||||
3. Install ESP32 core, version 3.2.0. See the [official Espressif's instructions](https://docs.espressif.com/projects/arduino-esp32/en/latest/installing.html#installing-using-arduino-ide) on installing ESP32 Core in Arduino IDE.
|
||||
4. Install the following libraries using [Library Manager](https://docs.arduino.cc/software/ide-v2/tutorials/ide-v2-installing-a-library):
|
||||
* `FlixPeriph`, the latest version.
|
||||
* `MAVLink`, version 2.0.16.
|
||||
5. Clone the project using git or [download the source code as a ZIP archive](https://codeload.github.com/okalachev/flix/zip/refs/heads/master).
|
||||
6. Open the downloaded Arduino sketch `flix/flix.ino` in Arduino IDE.
|
||||
7. Connect your ESP32 board to the computer and choose correct board type in Arduino IDE (*WEMOS D1 MINI ESP32* for ESP32 Mini) and the port.
|
||||
8. [Build and upload](https://docs.arduino.cc/software/ide-v2/tutorials/getting-started/ide-v2-uploading-a-sketch) the firmware using Arduino IDE.
|
||||
|
||||
### Command line (Windows, Linux, macOS)
|
||||
|
||||
1. [Install Arduino CLI](https://arduino.github.io/arduino-cli/installation/).
|
||||
|
||||
On Linux, use:
|
||||
|
||||
```bash
|
||||
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
|
||||
```
|
||||
|
||||
2. Windows users might need to install [USB to UART bridge driver from Silicon Labs](https://www.silabs.com/developers/usb-to-uart-bridge-vcp-drivers).
|
||||
3. Compile the firmware using `make`. Arduino dependencies will be installed automatically:
|
||||
|
||||
```bash
|
||||
make
|
||||
```
|
||||
|
||||
You can flash the firmware to the board using command:
|
||||
|
||||
```bash
|
||||
make upload
|
||||
```
|
||||
|
||||
You can also compile the firmware, upload it and start serial port monitoring using command:
|
||||
|
||||
```bash
|
||||
make upload monitor
|
||||
```
|
||||
|
||||
See other available Make commands in the [Makefile](../Makefile).
|
||||
|
||||
> [!TIP]
|
||||
> You can test the firmware on a bare ESP32 board without connecting IMU and other peripherals. The Wi-Fi network `flix` should appear and all the basic functionality including CLI and QGroundControl connection should work.
|
||||
|
||||
### Setup and flight
|
||||
|
||||
Before flight you need to calibrate the accelerometer:
|
||||
|
||||
1. Open Serial Monitor in Arduino IDE (or use `make monitor` command in the command line).
|
||||
2. Type `ca` command there and follow the instructions.
|
||||
|
||||
#### Control with smartphone
|
||||
|
||||
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone.
|
||||
2. Power the drone using the battery.
|
||||
3. Connect your smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
|
||||
4. Open QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
|
||||
5. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
|
||||
6. Use the virtual joystick to fly the drone!
|
||||
|
||||
#### Control with remote control
|
||||
|
||||
Before flight using remote control, you need to calibrate it:
|
||||
|
||||
1. Open Serial Monitor in Arduino IDE (or use `make monitor` command in the command line).
|
||||
2. Type `cr` command there and follow the instructions.
|
||||
3. Use the remote control to fly the drone!
|
||||
|
||||
#### Control with USB remote control
|
||||
|
||||
If your drone doesn't have RC receiver installed, you can use USB remote control and QGroundControl app to fly it.
|
||||
|
||||
1. Install [QGroundControl](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html) app on your computer.
|
||||
2. Connect your USB remote control to the computer.
|
||||
3. Power up the drone.
|
||||
4. Connect your computer to the appeared `flix` Wi-Fi network (password: `flixwifi`).
|
||||
5. Launch QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
|
||||
6. Go the the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Joystick*. Calibrate you USB remote control there.
|
||||
7. Use the USB remote control to fly the drone!
|
||||
|
||||
#### Adjusting parameters
|
||||
|
||||
You can adjust some of the drone's parameters (include PID coefficients) in QGroundControl app. In order to do that, go to the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Parameters*.
|
||||
|
||||
<img src="img/parameters.png" width="400">
|
||||
|
||||
#### CLI access
|
||||
|
||||
In addition to accessing the drone's command line interface (CLI) using the serial port, you can also access it with QGroundControl using Wi-Fi connection. To do that, go to the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Analyze Tools* ⇒ *MAVLink Console*.
|
||||
|
||||
<img src="img/cli.png" width="400">
|
||||
|
||||
> [!NOTE]
|
||||
> If something goes wrong, go to the [Troubleshooting](troubleshooting.md) article.
|
||||
|
||||
### Firmware code structure
|
||||
|
||||
See [firmware overview](firmware.md) for more details.
|
||||
1
docs/build.md
Symbolic link
@@ -0,0 +1 @@
|
||||
usage.md
|
||||
@@ -1,39 +1,56 @@
|
||||
# Firmware overview
|
||||
|
||||
The firmware is a regular Arduino sketch, and follows the classic Arduino one-threaded design. The initialization code is in the `setup()` function, and the main loop is in the `loop()` function. The sketch includes multiple files, each responsible for a specific part of the system.
|
||||
The firmware is a regular Arduino sketch, and it follows the classic Arduino one-threaded design. The initialization code is in the `setup()` function, and the main loop is in the `loop()` function. The sketch includes several files, each responsible for a specific subsystem.
|
||||
|
||||
## Dataflow
|
||||
|
||||
<img src="img/dataflow.svg" width=800 alt="Firmware dataflow diagram">
|
||||
<img src="img/dataflow.svg" width=600 alt="Firmware dataflow diagram">
|
||||
|
||||
The main loop is running at 1000 Hz. All the dataflow is happening through global variables (for simplicity):
|
||||
The main loop is running at 1000 Hz. All the dataflow goes through global variables (for simplicity):
|
||||
|
||||
* `t` *(double)* — current step time, *s*.
|
||||
* `t` *(float)* — current step time, *s*.
|
||||
* `dt` *(float)* — time delta between the current and previous steps, *s*.
|
||||
* `gyro` *(Vector)* — data from the gyroscope, *rad/s*.
|
||||
* `acc` *(Vector)* — acceleration data from the accelerometer, *m/s<sup>2</sup>*.
|
||||
* `rates` *(Vector)* — filtered angular rates, *rad/s*.
|
||||
* `attitude` *(Quaternion)* — estimated attitude (orientation) of drone.
|
||||
* `controlRoll`, `controlPitch`, ... *(float[])* — pilot's control inputs, range [-1, 1].
|
||||
* `motors` *(float[])* — motor outputs, range [0, 1].
|
||||
* `controlRoll`, `controlPitch`, ... *(float[])* — pilot control inputs, range [-1, 1].
|
||||
* `motors` *(float[])* — motor outputs, range [0, 1].
|
||||
|
||||
## Source files
|
||||
|
||||
Firmware source files are located in `flix` directory. The key files are:
|
||||
Firmware source files are located in `flix` directory. The core files are:
|
||||
|
||||
* [`flix.ino`](../flix/flix.ino) — main entry point, Arduino sketch. Includes global variables definition and the main loop.
|
||||
* [`flix.ino`](../flix/flix.ino) — Arduino sketch main file, entry point.Includes some global variable definitions and the main loop.
|
||||
* [`imu.ino`](../flix/imu.ino) — reading data from the IMU sensor (gyroscope and accelerometer), IMU calibration.
|
||||
* [`rc.ino`](../flix/rc.ino) — reading data from the RC receiver, RC calibration.
|
||||
* [`estimate.ino`](../flix/estimate.ino) — drone's attitude estimation, complementary filter.
|
||||
* [`control.ino`](../flix/control.ino) — drone's attitude and rates control, three-dimensional two-level cascade PID controller.
|
||||
* [`motors.ino`](../flix/motors.ino) — PWM motor outputs control.
|
||||
* [`estimate.ino`](../flix/estimate.ino) — attitude estimation, complementary filter.
|
||||
* [`control.ino`](../flix/control.ino) — control subsystem, three-dimensional two-level cascade PID controller.
|
||||
* [`motors.ino`](../flix/motors.ino) — PWM motor output control.
|
||||
* [`mavlink.ino`](../flix/mavlink.ino) — interaction with QGroundControl or [pyflix](../tools/pyflix) via MAVLink protocol.
|
||||
|
||||
Utility files include:
|
||||
Utility files:
|
||||
|
||||
* [`vector.h`](../flix/vector.h), [`quaternion.h`](../flix/quaternion.h) — project's vector and quaternion libraries implementation.
|
||||
* [`pid.h`](../flix/pid.h) — generic PID controller implementation.
|
||||
* [`lpf.h`](../flix/lpf.h) — generic low-pass filter implementation.
|
||||
* [`vector.h`](../flix/vector.h), [`quaternion.h`](../flix/quaternion.h) — vector and quaternion libraries.
|
||||
* [`pid.h`](../flix/pid.h) — generic PID controller.
|
||||
* [`lpf.h`](../flix/lpf.h) — generic low-pass filter.
|
||||
|
||||
### Control subsystem
|
||||
|
||||
Pilot inputs are interpreted in `interpretControls()`, and then converted to the *control command*, which consists of the following:
|
||||
|
||||
* `attitudeTarget` *(Quaternion)* — target attitude of the drone.
|
||||
* `ratesTarget` *(Vector)* — target angular rates, *rad/s*.
|
||||
* `ratesExtra` *(Vector)* — additional (feed-forward) angular rates , used for yaw rate control in STAB mode, *rad/s*.
|
||||
* `torqueTarget` *(Vector)* — target torque, range [-1, 1].
|
||||
* `thrustTarget` *(float)* — collective thrust target, range [0, 1].
|
||||
|
||||
Control command is processed in `controlAttitude()`, `controlRates()`, `controlTorque()` functions. Each function may be skipped if the corresponding target is set to `NAN`.
|
||||
|
||||
<img src="img/control.svg" width=300 alt="Control subsystem diagram">
|
||||
|
||||
Armed state is stored in `armed` variable, and current mode is stored in `mode` variable.
|
||||
|
||||
## Building
|
||||
|
||||
See build instructions in [build.md](build.md).
|
||||
See build instructions in [usage.md](usage.md).
|
||||
|
||||
22
docs/img/arming.svg
Normal file
@@ -0,0 +1,22 @@
|
||||
<svg xmlns="http://www.w3.org/2000/svg" viewBox="0 0 340.21 211.28">
|
||||
<defs>
|
||||
<style>
|
||||
.a {
|
||||
fill: #d5d5d5;
|
||||
}
|
||||
|
||||
.b {
|
||||
fill: #fff;
|
||||
}
|
||||
|
||||
.c {
|
||||
fill: #636363;
|
||||
}
|
||||
</style>
|
||||
</defs>
|
||||
<path class="a" d="M340,159.31c-4.74-86-35.9-128.7-35.9-128.7C288.3,9.53,269.17,2.91,251.87.39s-22.31,7.87-22.31,7.87C201.7,4,170.11,4.19,170.11,4.19S138.51,4,110.65,8.26c0,0-5-10.38-22.3-7.87S51.91,9.53,36.14,30.61c0,0-31.16,42.67-35.9,128.7-2.82,51.08,19.68,55.36,38.43,50.4a60.08,60.08,0,0,0,30.55-19.66c7.51-9,19.64-25.32,34-28,17.28-3.26,33.14-4.77,45.09-4.78l21.82,0,21.81,0c12,0,27.82,1.52,45.09,4.78,14.34,2.71,26.47,19,34,28a60.06,60.06,0,0,0,30.56,19.66C320.29,214.67,342.79,210.39,340,159.31Z"/>
|
||||
<circle class="b" cx="88.54" cy="85.75" r="45.22"/>
|
||||
<circle class="b" cx="251.67" cy="85.75" r="45.22"/>
|
||||
<circle class="c" cx="251.67" cy="85.75" r="13.8"/>
|
||||
<circle class="c" cx="103.8" cy="112.12" r="13.8"/>
|
||||
</svg>
|
||||
|
After Width: | Height: | Size: 971 B |
BIN
docs/img/betafpv.jpg
Normal file
|
After Width: | Height: | Size: 26 KiB |
4
docs/img/control.svg
Normal file
|
After Width: | Height: | Size: 140 KiB |
123
docs/img/controls.svg
Normal file
@@ -0,0 +1,123 @@
|
||||
<svg xmlns="http://www.w3.org/2000/svg" viewBox="0 0 464.2 249.05">
|
||||
<defs>
|
||||
<style>
|
||||
.a {
|
||||
fill: #d5d5d5;
|
||||
}
|
||||
|
||||
.b {
|
||||
fill: #fff;
|
||||
}
|
||||
|
||||
.c {
|
||||
fill: #636363;
|
||||
}
|
||||
|
||||
.d {
|
||||
opacity: 0.7;
|
||||
}
|
||||
|
||||
.e {
|
||||
fill: none;
|
||||
stroke: #0076ba;
|
||||
stroke-linecap: round;
|
||||
stroke-miterlimit: 10;
|
||||
stroke-width: 13px;
|
||||
}
|
||||
|
||||
.f {
|
||||
fill: #0076ba;
|
||||
}
|
||||
|
||||
.g {
|
||||
font-size: 30px;
|
||||
font-family: Tahoma;
|
||||
}
|
||||
|
||||
.h {
|
||||
letter-spacing: 0em;
|
||||
}
|
||||
|
||||
.i {
|
||||
letter-spacing: -0.01em;
|
||||
}
|
||||
|
||||
.j {
|
||||
letter-spacing: -0.06em;
|
||||
}
|
||||
|
||||
.k {
|
||||
letter-spacing: 0em;
|
||||
}
|
||||
|
||||
.l {
|
||||
letter-spacing: -0.02em;
|
||||
}
|
||||
|
||||
.m {
|
||||
letter-spacing: 0em;
|
||||
}
|
||||
|
||||
.n {
|
||||
opacity: 0.6;
|
||||
}
|
||||
</style>
|
||||
</defs>
|
||||
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||||
|
After Width: | Height: | Size: 3.9 KiB |
|
Before Width: | Height: | Size: 22 KiB After Width: | Height: | Size: 101 KiB |
22
docs/img/disarming.svg
Normal file
@@ -0,0 +1,22 @@
|
||||
<svg xmlns="http://www.w3.org/2000/svg" viewBox="0 0 340.21 211.28">
|
||||
<defs>
|
||||
<style>
|
||||
.a {
|
||||
fill: #d5d5d5;
|
||||
}
|
||||
|
||||
.b {
|
||||
fill: #fff;
|
||||
}
|
||||
|
||||
.c {
|
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fill: #636363;
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}
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</style>
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</defs>
|
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<path class="a" d="M340,159.31c-4.74-86-35.9-128.7-35.9-128.7C288.3,9.53,269.17,2.91,251.87.39s-22.31,7.87-22.31,7.87C201.7,4,170.11,4.19,170.11,4.19S138.51,4,110.65,8.26c0,0-5-10.38-22.3-7.87S51.91,9.53,36.14,30.61c0,0-31.16,42.67-35.9,128.7-2.82,51.08,19.68,55.36,38.43,50.4a60.08,60.08,0,0,0,30.55-19.66c7.51-9,19.64-25.32,34-28,17.28-3.26,33.14-4.77,45.09-4.78l21.82,0,21.81,0c12,0,27.82,1.52,45.09,4.78,14.34,2.71,26.47,19,34,28a60.06,60.06,0,0,0,30.56,19.66C320.29,214.67,342.79,210.39,340,159.31Z"/>
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<circle class="b" cx="251.67" cy="85.75" r="45.22"/>
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<circle class="c" cx="251.67" cy="85.75" r="13.8"/>
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<circle class="c" cx="73.28" cy="112.12" r="13.8"/>
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</svg>
|
||||
|
After Width: | Height: | Size: 971 B |
|
Before Width: | Height: | Size: 36 KiB After Width: | Height: | Size: 36 KiB |
BIN
docs/img/logitech.jpg
Normal file
|
After Width: | Height: | Size: 26 KiB |
BIN
docs/img/qgc-proxy.png
Normal file
|
After Width: | Height: | Size: 24 KiB |
|
Before Width: | Height: | Size: 17 KiB After Width: | Height: | Size: 18 KiB |
BIN
docs/img/user/robocamp/1.jpg
Normal file
|
After Width: | Height: | Size: 148 KiB |
@@ -4,8 +4,9 @@
|
||||
|
||||
Do the following:
|
||||
|
||||
* **Check ESP32 core is installed**. Check if the version matches the one used in the [tutorial](build.md#firmware).
|
||||
* **Check ESP32 core is installed**. Check if the version matches the one used in the [tutorial](usage.md#firmware).
|
||||
* **Check libraries**. Install all the required libraries from the tutorial. Make sure there are no MPU9250 or other peripherals libraries that may conflict with the ones used in the tutorial.
|
||||
* **Check the chosen board**. The correct board to choose in Arduino IDE for ESP32 Mini is *WEMOS D1 MINI ESP32*.
|
||||
|
||||
## The drone doesn't fly
|
||||
|
||||
@@ -14,7 +15,7 @@ Do the following:
|
||||
* **Check the battery voltage**. Use a multimeter to measure the battery voltage. It should be in range of 3.7-4.2 V.
|
||||
* **Check if there are some startup errors**. Connect the ESP32 to the computer and check the Serial Monitor output. Use the Reset button to make sure you see the whole ESP32 output.
|
||||
* **Check the baudrate is correct**. If you see garbage characters in the Serial Monitor, make sure the baudrate is set to 115200.
|
||||
* **Make sure correct IMU model is chosen**. If using ICM-20948 board, change `MPU9250` to `ICM20948` everywhere in the `imu.ino` file.
|
||||
* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
|
||||
* **Check if the CLI is working**. Perform `help` command in Serial Monitor. You should see the list of available commands. You can also access the CLI using QGroundControl (*Vehicle Setup* ⇒ *Analyze Tools* ⇒ *MAVLink Console*).
|
||||
* **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.
|
||||
@@ -31,7 +32,6 @@ Do the following:
|
||||
* `mfl` — should rotate front left motor (clockwise).
|
||||
* `mrl` — should rotate rear left motor (counter-clockwise).
|
||||
* `mrr` — should rotate rear right motor (clockwise).
|
||||
* **Calibrate the RC** if you use it. Type `cr` command in Serial Monitor and follow the instructions.
|
||||
* **Check the RC data** if you use it. Use `rc` command, `Control` should show correct values between -1 and 1, and between 0 and 1 for the throttle.
|
||||
* **Check the remote control**. Using `rc` command, check the control values reflect your sticks movement. All the controls should change between -1 and 1, and throttle between 0 and 1.
|
||||
* If using SBUS receiver, **calibrate the RC**. Type `cr` command in Serial Monitor and follow the instructions.
|
||||
* **Check the IMU output using QGroundControl**. Connect to the drone using QGroundControl on your computer. Go to the *Analyze* tab, *MAVLINK Inspector*. Plot the data from the `SCALED_IMU` message. The gyroscope and accelerometer data should change according to the drone movement.
|
||||
* **Check the gyroscope only attitude estimation**. Comment out `applyAcc();` line in `estimate.ino` and check if the attitude estimation in QGroundControl. It should be stable, but only drift very slowly.
|
||||
|
||||
252
docs/usage.md
Normal file
@@ -0,0 +1,252 @@
|
||||
# Usage: build, setup and flight
|
||||
|
||||
To use Flix, you need to build the firmware and upload it to the ESP32 board. For simulation, you need to build and run the simulator.
|
||||
|
||||
For the start, clone the repository using git:
|
||||
|
||||
```bash
|
||||
git clone https://github.com/okalachev/flix.git
|
||||
cd flix
|
||||
```
|
||||
|
||||
## Simulation
|
||||
|
||||
### Ubuntu
|
||||
|
||||
The latest version of Ubuntu supported by Gazebo 11 simulator is 20.04. If you have a newer version, consider using a virtual machine.
|
||||
|
||||
1. Install Arduino CLI:
|
||||
|
||||
```bash
|
||||
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
|
||||
```
|
||||
|
||||
2. Install Gazebo 11:
|
||||
|
||||
```bash
|
||||
sudo sh -c 'echo "deb http://packages.osrfoundation.org/gazebo/ubuntu-stable `lsb_release -cs` main" > /etc/apt/sources.list.d/gazebo-stable.list'
|
||||
wget https://packages.osrfoundation.org/gazebo.key -O - | sudo apt-key add -
|
||||
sudo apt-get update
|
||||
sudo apt-get install -y gazebo11 libgazebo11-dev
|
||||
```
|
||||
|
||||
Set up your Gazebo environment variables:
|
||||
|
||||
```bash
|
||||
echo "source /usr/share/gazebo/setup.sh" >> ~/.bashrc
|
||||
source ~/.bashrc
|
||||
```
|
||||
|
||||
3. Install SDL2 and other dependencies:
|
||||
|
||||
```bash
|
||||
sudo apt-get update && sudo apt-get install build-essential libsdl2-dev
|
||||
```
|
||||
|
||||
4. Add your user to the `input` group to enable joystick support (you need to re-login after this command):
|
||||
|
||||
```bash
|
||||
sudo usermod -a -G input $USER
|
||||
```
|
||||
|
||||
5. Run the simulation:
|
||||
|
||||
```bash
|
||||
make simulator
|
||||
```
|
||||
|
||||
### macOS
|
||||
|
||||
1. Install Homebrew package manager, if you don't have it installed:
|
||||
|
||||
```bash
|
||||
/bin/bash -c "$(curl -fsSL https://raw.githubusercontent.com/Homebrew/install/HEAD/install.sh)"
|
||||
```
|
||||
|
||||
2. Install Arduino CLI, Gazebo 11 and SDL2:
|
||||
|
||||
```bash
|
||||
brew tap osrf/simulation
|
||||
brew install arduino-cli
|
||||
brew install gazebo11
|
||||
brew install sdl2
|
||||
```
|
||||
|
||||
Set up your Gazebo environment variables:
|
||||
|
||||
```bash
|
||||
echo "source /opt/homebrew/share/gazebo/setup.sh" >> ~/.zshrc
|
||||
source ~/.zshrc
|
||||
```
|
||||
|
||||
3. Run the simulation:
|
||||
|
||||
```bash
|
||||
make simulator
|
||||
```
|
||||
|
||||
### Setup
|
||||
|
||||
#### Control with smartphone
|
||||
|
||||
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone. For **iOS**, use [QGroundControl build from TAJISOFT](https://apps.apple.com/ru/app/qgc-from-tajisoft/id1618653051).
|
||||
2. Connect your smartphone to the same Wi-Fi network as the machine running the simulator.
|
||||
3. If you're using a virtual machine, make sure that its network is set to the **bridged** mode with Wi-Fi adapter selected.
|
||||
4. Run the simulation.
|
||||
5. Open QGroundControl app. It should connect and begin showing the virtual drone's telemetry automatically.
|
||||
6. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
|
||||
7. Use the virtual joystick to fly the drone!
|
||||
|
||||
#### Control with USB remote control
|
||||
|
||||
1. Connect your USB remote control to the machine running the simulator.
|
||||
2. Run the simulation.
|
||||
3. Calibrate the RC using `cr` command in the command line interface.
|
||||
4. Run the simulation again.
|
||||
5. Use the USB remote control to fly the drone!
|
||||
|
||||
## Firmware
|
||||
|
||||
### Arduino IDE (Windows, Linux, macOS)
|
||||
|
||||
1. Install [Arduino IDE](https://www.arduino.cc/en/software) (version 2 is recommended).
|
||||
2. Windows users might need to install [USB to UART bridge driver from Silicon Labs](https://www.silabs.com/developers/usb-to-uart-bridge-vcp-drivers).
|
||||
3. Install ESP32 core, version 3.2.0. See the [official Espressif's instructions](https://docs.espressif.com/projects/arduino-esp32/en/latest/installing.html#installing-using-arduino-ide) on installing ESP32 Core in Arduino IDE.
|
||||
4. Install the following libraries using [Library Manager](https://docs.arduino.cc/software/ide-v2/tutorials/ide-v2-installing-a-library):
|
||||
* `FlixPeriph`, the latest version.
|
||||
* `MAVLink`, version 2.0.16.
|
||||
5. Clone the project using git or [download the source code as a ZIP archive](https://codeload.github.com/okalachev/flix/zip/refs/heads/master).
|
||||
6. Open the downloaded Arduino sketch `flix/flix.ino` in Arduino IDE.
|
||||
7. Connect your ESP32 board to the computer and choose correct board type in Arduino IDE (*WEMOS D1 MINI ESP32* for ESP32 Mini) and the port.
|
||||
8. [Build and upload](https://docs.arduino.cc/software/ide-v2/tutorials/getting-started/ide-v2-uploading-a-sketch) the firmware using Arduino IDE.
|
||||
|
||||
### Command line (Windows, Linux, macOS)
|
||||
|
||||
1. [Install Arduino CLI](https://arduino.github.io/arduino-cli/installation/).
|
||||
|
||||
On Linux, use:
|
||||
|
||||
```bash
|
||||
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
|
||||
```
|
||||
|
||||
2. Windows users might need to install [USB to UART bridge driver from Silicon Labs](https://www.silabs.com/developers/usb-to-uart-bridge-vcp-drivers).
|
||||
3. Compile the firmware using `make`. Arduino dependencies will be installed automatically:
|
||||
|
||||
```bash
|
||||
make
|
||||
```
|
||||
|
||||
You can flash the firmware to the board using command:
|
||||
|
||||
```bash
|
||||
make upload
|
||||
```
|
||||
|
||||
You can also compile the firmware, upload it and start serial port monitoring using command:
|
||||
|
||||
```bash
|
||||
make upload monitor
|
||||
```
|
||||
|
||||
See other available Make commands in the [Makefile](../Makefile).
|
||||
|
||||
> [!TIP]
|
||||
> You can test the firmware on a bare ESP32 board without connecting IMU and other peripherals. The Wi-Fi network `flix` should appear and all the basic functionality including CLI and QGroundControl connection should work.
|
||||
|
||||
### Setup
|
||||
|
||||
Before flight you need to calibrate the accelerometer:
|
||||
|
||||
1. Open Serial Monitor in Arduino IDE (or use `make monitor` command in the command line).
|
||||
2. Type `ca` command there and follow the instructions.
|
||||
|
||||
#### Control with smartphone
|
||||
|
||||
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone.
|
||||
2. Power the drone using the battery.
|
||||
3. Connect your smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
|
||||
4. Open QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
|
||||
5. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
|
||||
6. Use the virtual joystick to fly the drone!
|
||||
|
||||
> [!TIP]
|
||||
> Decrease `TILT_MAX` parameter when flying using the smartphone to make the controls less sensitive.
|
||||
|
||||
#### Control with remote control
|
||||
|
||||
Before flight using remote control, you need to calibrate it:
|
||||
|
||||
1. Open Serial Monitor in Arduino IDE (or use `make monitor` command in the command line).
|
||||
2. Type `cr` command there and follow the instructions.
|
||||
3. Use the remote control to fly the drone!
|
||||
|
||||
#### Control with USB remote control (Wi-Fi)
|
||||
|
||||
If your drone doesn't have RC receiver installed, you can use USB remote control and QGroundControl app to fly it.
|
||||
|
||||
1. Install [QGroundControl](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html) app on your computer.
|
||||
2. Connect your USB remote control to the computer.
|
||||
3. Power up the drone.
|
||||
4. Connect your computer to the appeared `flix` Wi-Fi network (password: `flixwifi`).
|
||||
5. Launch QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
|
||||
6. Go the the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Joystick*. Calibrate you USB remote control there.
|
||||
7. Use the USB remote control to fly the drone!
|
||||
|
||||
> [!NOTE]
|
||||
> If something goes wrong, go to the [Troubleshooting](troubleshooting.md) article.
|
||||
|
||||
## Flight
|
||||
|
||||
For both virtual sticks and a physical joystick, the default control scheme is left stick for throttle and yaw and right stick for pitch and roll:
|
||||
|
||||
<img src="img/controls.svg" width="300">
|
||||
|
||||
### Arming and disarming
|
||||
|
||||
To start the motors, you should **arm** the drone. To do that, move the left stick to the bottom right corner:
|
||||
|
||||
<img src="img/arming.svg" width="150">
|
||||
|
||||
After that, the motors **will start spinning** at low speed, indicating that the drone is armed and ready to fly.
|
||||
|
||||
When finished flying, **disarm** the drone, moving the left stick to the bottom left corner:
|
||||
|
||||
<img src="img/disarming.svg" width="150">
|
||||
|
||||
### Flight modes
|
||||
|
||||
Flight mode is changed using mode switch on the remote control or using the command line.
|
||||
|
||||
#### STAB
|
||||
|
||||
The default mode is *STAB*. In this mode, the drone stabilizes its attitude (orientation). The left stick controls throttle and yaw rate, the right stick controls pitch and roll angles.
|
||||
|
||||
> [!IMPORTANT]
|
||||
> The drone doesn't stabilize its position, so slight drift is possible. The pilot should compensate it manually.
|
||||
|
||||
#### ACRO
|
||||
|
||||
In this mode, the pilot controls the angular rates. This control method is difficult to fly and mostly used in FPV racing.
|
||||
|
||||
#### MANUAL
|
||||
|
||||
Manual mode disables all the stabilization, and the pilot inputs are passed directly to the motors. This mode is intended for testing and demonstration purposes only, and basically the drone **cannot fly in this mode**.
|
||||
|
||||
#### AUTO
|
||||
|
||||
In this mode, the pilot inputs are ignored (except the mode switch, if configured). The drone can be controlled using [pyflix](../tools/pyflix/) Python library, or by modifying the firmware to implement the needed autonomous behavior.
|
||||
|
||||
If the pilot moves the control sticks, the drone will switch back to *STAB* mode.
|
||||
|
||||
## Adjusting parameters
|
||||
|
||||
You can adjust some of the drone's parameters (include PID coefficients) in QGroundControl app. In order to do that, go to the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Parameters*.
|
||||
|
||||
<img src="img/parameters.png" width="400">
|
||||
|
||||
## CLI access
|
||||
|
||||
In addition to accessing the drone's command line interface (CLI) using the serial port, you can also access it with QGroundControl using Wi-Fi connection. To do that, go to the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Analyze Tools* ⇒ *MAVLink Console*.
|
||||
|
||||
<img src="img/cli.png" width="400">
|
||||
19
docs/user.md
@@ -4,6 +4,25 @@ This page contains user-built drones based on the Flix project. Publish your pro
|
||||
|
||||
---
|
||||
|
||||
## RoboCamp
|
||||
|
||||
Author: RoboCamp participants.<br>
|
||||
Description: 3D-printed and wooden frames, ESP32 Mini, DC-DC buck-boost converters. BetaFPV LiteRadio 3 to control the drones via Wi-Fi connection.<br>
|
||||
Features: altitude hold, obstacle avoidance, autonomous flight elements.<br>
|
||||
Some of the designed model files: https://drive.google.com/drive/folders/18YHWGquKeIevzrMH4-OUT-zKXMETTEUu?usp=share_link.
|
||||
|
||||
RoboCamp took place in July 2025, Saint Petersburg, where 9 participants designed and built their own drones using the Flix project, and then modified the firmware to complete specific flight tasks.
|
||||
|
||||
See the detailed video about the event:
|
||||
|
||||
<a href="https://youtu.be/Wd3yaorjTx0"><img width=500 src="https://img.youtube.com/vi/Wd3yaorjTx0/sddefault.jpg"></a>
|
||||
|
||||
Built drones:
|
||||
|
||||
<img src="img/user/robocamp/1.jpg" width=500>
|
||||
|
||||
---
|
||||
|
||||
Author: chkroko.<br>
|
||||
Description: the first Flix drone built with **brushless motors** (DShot interface).<br>
|
||||
Features: SpeedyBee BLS 35A Mini V2 ESC, ESP32-S3 board, EMAX ECO 2 2207 1700kv motors, ICM20948V2 IMU, INA226 power monitor and Bluetooth gamepad for control.<br>
|
||||
|
||||
38
flix/cli.ino
@@ -8,10 +8,12 @@
|
||||
#include "util.h"
|
||||
|
||||
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
|
||||
extern float loopRate, dt;
|
||||
extern double t;
|
||||
extern const int ACRO, STAB, AUTO;
|
||||
extern float t, dt, loopRate;
|
||||
extern uint16_t channels[16];
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlArmed, controlMode;
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
|
||||
extern int mode;
|
||||
extern bool armed;
|
||||
|
||||
const char* motd =
|
||||
"\nWelcome to\n"
|
||||
@@ -31,6 +33,9 @@ const char* motd =
|
||||
"ps - show pitch/roll/yaw\n"
|
||||
"psq - show attitude quaternion\n"
|
||||
"imu - show IMU data\n"
|
||||
"arm - arm the drone\n"
|
||||
"disarm - disarm the drone\n"
|
||||
"stab/acro/auto - set mode\n"
|
||||
"rc - show RC data\n"
|
||||
"mot - show motor output\n"
|
||||
"log - dump in-RAM log\n"
|
||||
@@ -54,7 +59,7 @@ void print(const char* format, ...) {
|
||||
}
|
||||
|
||||
void pause(float duration) {
|
||||
double start = t;
|
||||
float start = t;
|
||||
while (t - start < duration) {
|
||||
step();
|
||||
handleInput();
|
||||
@@ -69,9 +74,10 @@ void doCommand(String str, bool echo = false) {
|
||||
// parse command
|
||||
String command, arg0, arg1;
|
||||
splitString(str, command, arg0, arg1);
|
||||
if (command.isEmpty()) return;
|
||||
|
||||
// echo command
|
||||
if (echo && !command.isEmpty()) {
|
||||
if (echo) {
|
||||
print("> %s\n", str.c_str());
|
||||
}
|
||||
|
||||
@@ -101,22 +107,30 @@ void doCommand(String str, bool echo = false) {
|
||||
Vector a = attitude.toEuler();
|
||||
print("roll: %f pitch: %f yaw: %f\n", degrees(a.x), degrees(a.y), degrees(a.z));
|
||||
} else if (command == "psq") {
|
||||
print("qx: %f qy: %f qz: %f qw: %f\n", attitude.x, attitude.y, attitude.z, attitude.w);
|
||||
print("qw: %f qx: %f qy: %f qz: %f\n", attitude.w, attitude.x, attitude.y, attitude.z);
|
||||
} else if (command == "imu") {
|
||||
printIMUInfo();
|
||||
print("gyro: %f %f %f\n", rates.x, rates.y, rates.z);
|
||||
print("acc: %f %f %f\n", acc.x, acc.y, acc.z);
|
||||
printIMUCalibration();
|
||||
print("rate: %.0f\n", loopRate);
|
||||
print("landed: %d\n", landed);
|
||||
} else if (command == "arm") {
|
||||
armed = true;
|
||||
} else if (command == "disarm") {
|
||||
armed = false;
|
||||
} else if (command == "stab") {
|
||||
mode = STAB;
|
||||
} else if (command == "acro") {
|
||||
mode = ACRO;
|
||||
} else if (command == "auto") {
|
||||
mode = AUTO;
|
||||
} else if (command == "rc") {
|
||||
print("channels: ");
|
||||
for (int i = 0; i < 16; i++) {
|
||||
print("%u ", channels[i]);
|
||||
}
|
||||
print("\nroll: %g pitch: %g yaw: %g throttle: %g armed: %g mode: %g\n",
|
||||
controlRoll, controlPitch, controlYaw, controlThrottle, controlArmed, controlMode);
|
||||
print("\nroll: %g pitch: %g yaw: %g throttle: %g mode: %g\n",
|
||||
controlRoll, controlPitch, controlYaw, controlThrottle, controlMode);
|
||||
print("mode: %s\n", getModeName());
|
||||
print("armed: %d\n", armed);
|
||||
} else if (command == "mot") {
|
||||
print("front-right %g front-left %g rear-right %g rear-left %g\n",
|
||||
motors[MOTOR_FRONT_RIGHT], motors[MOTOR_FRONT_LEFT], motors[MOTOR_REAR_RIGHT], motors[MOTOR_REAR_LEFT]);
|
||||
@@ -157,8 +171,6 @@ void doCommand(String str, bool echo = false) {
|
||||
attitude = Quaternion();
|
||||
} else if (command == "reboot") {
|
||||
ESP.restart();
|
||||
} else if (command == "") {
|
||||
// do nothing
|
||||
} else {
|
||||
print("Invalid command: %s\n", command.c_str());
|
||||
}
|
||||
|
||||
126
flix/control.ino
@@ -34,8 +34,8 @@
|
||||
#define TILT_MAX radians(30)
|
||||
#define RATES_D_LPF_ALPHA 0.2 // cutoff frequency ~ 40 Hz
|
||||
|
||||
enum { MANUAL, ACRO, STAB, USER } mode = STAB;
|
||||
enum { YAW, YAW_RATE } yawMode = YAW;
|
||||
const int MANUAL = 0, ACRO = 1, STAB = 2, AUTO = 3; // flight modes
|
||||
int mode = STAB;
|
||||
bool armed = false;
|
||||
|
||||
PID rollRatePID(ROLLRATE_P, ROLLRATE_I, ROLLRATE_D, ROLLRATE_I_LIM, RATES_D_LPF_ALPHA);
|
||||
@@ -49,75 +49,57 @@ 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, controlArmed, controlMode;
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
|
||||
|
||||
void control() {
|
||||
interpretRC();
|
||||
interpretControls();
|
||||
failsafe();
|
||||
if (mode == STAB) {
|
||||
controlAttitude();
|
||||
controlRate();
|
||||
controlTorque();
|
||||
} else if (mode == ACRO) {
|
||||
controlRate();
|
||||
controlTorque();
|
||||
} else if (mode == MANUAL) {
|
||||
controlTorque();
|
||||
}
|
||||
controlAttitude();
|
||||
controlRates();
|
||||
controlTorque();
|
||||
}
|
||||
|
||||
void interpretRC() {
|
||||
armed = controlThrottle >= 0.05 && controlArmed >= 0.5;
|
||||
|
||||
void interpretControls() {
|
||||
// NOTE: put ACRO or MANUAL modes there if you want to use them
|
||||
if (controlMode < 0.25) {
|
||||
mode = STAB;
|
||||
} else if (controlMode < 0.75) {
|
||||
mode = STAB;
|
||||
} else {
|
||||
mode = STAB;
|
||||
}
|
||||
if (controlMode < 0.25) mode = STAB;
|
||||
if (controlMode < 0.75) mode = STAB;
|
||||
if (controlMode > 0.75) mode = STAB;
|
||||
|
||||
if (mode == AUTO) return; // pilot is not effective in AUTO mode
|
||||
|
||||
if (controlThrottle < 0.05 && controlYaw > 0.95) armed = true; // arm gesture
|
||||
if (controlThrottle < 0.05 && controlYaw < -0.95) armed = false; // disarm gesture
|
||||
|
||||
thrustTarget = controlThrottle;
|
||||
|
||||
if (mode == ACRO) {
|
||||
yawMode = YAW_RATE;
|
||||
ratesTarget.x = controlRoll * maxRate.x;
|
||||
ratesTarget.y = controlPitch* maxRate.y;
|
||||
ratesTarget.z = -controlYaw * maxRate.z; // positive yaw stick means clockwise rotation in FLU
|
||||
|
||||
} else if (mode == STAB) {
|
||||
yawMode = controlYaw == 0 ? YAW : YAW_RATE;
|
||||
|
||||
attitudeTarget = Quaternion::fromEuler(Vector(
|
||||
controlRoll * tiltMax,
|
||||
controlPitch * tiltMax,
|
||||
attitudeTarget.getYaw()));
|
||||
ratesTarget.z = -controlYaw * maxRate.z; // positive yaw stick means clockwise rotation in FLU
|
||||
|
||||
} else if (mode == MANUAL) {
|
||||
// passthrough mode
|
||||
yawMode = YAW_RATE;
|
||||
torqueTarget = Vector(controlRoll, controlPitch, -controlYaw) * 0.01;
|
||||
if (mode == STAB) {
|
||||
float yawTarget = attitudeTarget.getYaw();
|
||||
if (!armed || invalid(yawTarget) || controlYaw != 0) yawTarget = attitude.getYaw(); // reset yaw target
|
||||
attitudeTarget = Quaternion::fromEuler(Vector(controlRoll * tiltMax, controlPitch * tiltMax, yawTarget));
|
||||
ratesExtra = Vector(0, 0, -controlYaw * maxRate.z); // positive yaw stick means clockwise rotation in FLU
|
||||
}
|
||||
|
||||
if (yawMode == YAW_RATE || !motorsActive()) {
|
||||
// update yaw target as we don't have control over the yaw
|
||||
attitudeTarget.setYaw(attitude.getYaw());
|
||||
if (mode == ACRO) {
|
||||
attitudeTarget.invalidate(); // skip attitude control
|
||||
ratesTarget.x = controlRoll * maxRate.x;
|
||||
ratesTarget.y = controlPitch * maxRate.y;
|
||||
ratesTarget.z = -controlYaw * maxRate.z; // positive yaw stick means clockwise rotation in FLU
|
||||
}
|
||||
|
||||
if (mode == MANUAL) { // passthrough mode
|
||||
attitudeTarget.invalidate(); // skip attitude control
|
||||
ratesTarget.invalidate(); // skip rate control
|
||||
torqueTarget = Vector(controlRoll, controlPitch, -controlYaw) * 0.01;
|
||||
}
|
||||
}
|
||||
|
||||
void controlAttitude() {
|
||||
if (!armed) {
|
||||
rollPID.reset();
|
||||
pitchPID.reset();
|
||||
yawPID.reset();
|
||||
return;
|
||||
}
|
||||
if (!armed || attitudeTarget.invalid() || thrustTarget < 0.1) return; // skip attitude control
|
||||
|
||||
const Vector up(0, 0, 1);
|
||||
Vector upActual = Quaternion::rotateVector(up, attitude);
|
||||
@@ -125,34 +107,38 @@ void controlAttitude() {
|
||||
|
||||
Vector error = Vector::rotationVectorBetween(upTarget, upActual);
|
||||
|
||||
ratesTarget.x = rollPID.update(error.x, dt);
|
||||
ratesTarget.y = pitchPID.update(error.y, dt);
|
||||
ratesTarget.x = rollPID.update(error.x) + ratesExtra.x;
|
||||
ratesTarget.y = pitchPID.update(error.y) + ratesExtra.y;
|
||||
|
||||
if (yawMode == YAW) {
|
||||
float yawError = wrapAngle(attitudeTarget.getYaw() - attitude.getYaw());
|
||||
ratesTarget.z = yawPID.update(yawError, dt);
|
||||
}
|
||||
float yawError = wrapAngle(attitudeTarget.getYaw() - attitude.getYaw());
|
||||
ratesTarget.z = yawPID.update(yawError) + ratesExtra.z;
|
||||
}
|
||||
|
||||
void controlRate() {
|
||||
if (!armed) {
|
||||
rollRatePID.reset();
|
||||
pitchRatePID.reset();
|
||||
yawRatePID.reset();
|
||||
return;
|
||||
}
|
||||
|
||||
void controlRates() {
|
||||
if (!armed || ratesTarget.invalid() || thrustTarget < 0.1) return; // skip rates control
|
||||
|
||||
Vector error = ratesTarget - rates;
|
||||
|
||||
// Calculate desired torque, where 0 - no torque, 1 - maximum possible torque
|
||||
torqueTarget.x = rollRatePID.update(error.x, dt);
|
||||
torqueTarget.y = pitchRatePID.update(error.y, dt);
|
||||
torqueTarget.z = yawRatePID.update(error.z, dt);
|
||||
torqueTarget.x = rollRatePID.update(error.x);
|
||||
torqueTarget.y = pitchRatePID.update(error.y);
|
||||
torqueTarget.z = yawRatePID.update(error.z);
|
||||
}
|
||||
|
||||
void controlTorque() {
|
||||
if (!torqueTarget.valid()) return; // skip torque control
|
||||
|
||||
if (!armed) {
|
||||
memset(motors, 0, sizeof(motors));
|
||||
memset(motors, 0, sizeof(motors)); // stop motors if disarmed
|
||||
return;
|
||||
}
|
||||
|
||||
if (thrustTarget < 0.1) {
|
||||
motors[0] = 0.1; // idle thrust
|
||||
motors[1] = 0.1;
|
||||
motors[2] = 0.1;
|
||||
motors[3] = 0.1;
|
||||
return;
|
||||
}
|
||||
|
||||
@@ -172,7 +158,7 @@ const char* getModeName() {
|
||||
case MANUAL: return "MANUAL";
|
||||
case ACRO: return "ACRO";
|
||||
case STAB: return "STAB";
|
||||
case USER: return "USER";
|
||||
case AUTO: return "AUTO";
|
||||
default: return "UNKNOWN";
|
||||
}
|
||||
}
|
||||
|
||||
@@ -11,8 +11,6 @@
|
||||
#define WEIGHT_ACC 0.003
|
||||
#define RATES_LFP_ALPHA 0.2 // cutoff frequency ~ 40 Hz
|
||||
|
||||
LowPassFilter<Vector> ratesFilter(RATES_LFP_ALPHA);
|
||||
|
||||
void estimate() {
|
||||
applyGyro();
|
||||
applyAcc();
|
||||
@@ -20,6 +18,7 @@ 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
|
||||
|
||||
@@ -1,41 +0,0 @@
|
||||
// Copyright (c) 2024 Oleg Kalachev <okalachev@gmail.com>
|
||||
// Repository: https://github.com/okalachev/flix
|
||||
|
||||
// Fail-safe functions
|
||||
|
||||
#define RC_LOSS_TIMEOUT 0.2
|
||||
#define DESCEND_TIME 3.0 // time to descend from full throttle to zero
|
||||
|
||||
extern double controlTime;
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw;
|
||||
|
||||
void failsafe() {
|
||||
armingFailsafe();
|
||||
rcLossFailsafe();
|
||||
}
|
||||
|
||||
// Prevent arming without zero throttle input
|
||||
void armingFailsafe() {
|
||||
static double zeroThrottleTime;
|
||||
static double armingTime;
|
||||
if (!armed) armingTime = t; // stores the last time when the drone was disarmed, therefore contains arming time
|
||||
if (controlTime > 0 && controlThrottle < 0.05) zeroThrottleTime = controlTime;
|
||||
if (armingTime - zeroThrottleTime > 0.1) armed = false; // prevent arming if there was no zero throttle for 0.1 sec
|
||||
}
|
||||
|
||||
// RC loss failsafe
|
||||
void rcLossFailsafe() {
|
||||
if (t - controlTime > RC_LOSS_TIMEOUT) {
|
||||
descend();
|
||||
}
|
||||
}
|
||||
|
||||
// Smooth descend on RC lost
|
||||
void descend() {
|
||||
mode = STAB;
|
||||
controlRoll = 0;
|
||||
controlPitch = 0;
|
||||
controlYaw = 0;
|
||||
controlThrottle -= dt / DESCEND_TIME;
|
||||
if (controlThrottle < 0) controlThrottle = 0;
|
||||
}
|
||||
@@ -10,9 +10,10 @@
|
||||
#define SERIAL_BAUDRATE 115200
|
||||
#define WIFI_ENABLED 1
|
||||
|
||||
double t = NAN; // current step time, s
|
||||
float t = NAN; // current step time, s
|
||||
float dt; // time delta from previous step, s
|
||||
float controlRoll, controlPitch, controlYaw, controlThrottle, controlArmed, controlMode; // pilot's inputs, range [-1, 1]
|
||||
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
|
||||
float controlMode = NAN;
|
||||
Vector gyro; // gyroscope data
|
||||
Vector acc; // accelerometer data, m/s/s
|
||||
Vector rates; // filtered angular rates, rad/s
|
||||
|
||||
49
flix/imu.ino
@@ -4,11 +4,12 @@
|
||||
// Work with the IMU sensor
|
||||
|
||||
#include <SPI.h>
|
||||
#include <MPU9250.h>
|
||||
#include <FlixPeriph.h>
|
||||
#include "vector.h"
|
||||
#include "lpf.h"
|
||||
#include "util.h"
|
||||
|
||||
MPU9250 IMU(SPI);
|
||||
MPU9250 imu(SPI);
|
||||
|
||||
Vector accBias;
|
||||
Vector accScale(1, 1, 1);
|
||||
@@ -16,22 +17,22 @@ Vector gyroBias;
|
||||
|
||||
void setupIMU() {
|
||||
print("Setup IMU\n");
|
||||
IMU.begin();
|
||||
imu.begin();
|
||||
configureIMU();
|
||||
}
|
||||
|
||||
void configureIMU() {
|
||||
IMU.setAccelRange(IMU.ACCEL_RANGE_4G);
|
||||
IMU.setGyroRange(IMU.GYRO_RANGE_2000DPS);
|
||||
IMU.setDLPF(IMU.DLPF_MAX);
|
||||
IMU.setRate(IMU.RATE_1KHZ_APPROX);
|
||||
IMU.setupInterrupt();
|
||||
imu.setAccelRange(imu.ACCEL_RANGE_4G);
|
||||
imu.setGyroRange(imu.GYRO_RANGE_2000DPS);
|
||||
imu.setDLPF(imu.DLPF_MAX);
|
||||
imu.setRate(imu.RATE_1KHZ_APPROX);
|
||||
imu.setupInterrupt();
|
||||
}
|
||||
|
||||
void readIMU() {
|
||||
IMU.waitForData();
|
||||
IMU.getGyro(gyro.x, gyro.y, gyro.z);
|
||||
IMU.getAccel(acc.x, acc.y, acc.z);
|
||||
imu.waitForData();
|
||||
imu.getGyro(gyro.x, gyro.y, gyro.z);
|
||||
imu.getAccel(acc.x, acc.y, acc.z);
|
||||
calibrateGyroOnce();
|
||||
// apply scale and bias
|
||||
acc = (acc - accBias) / accScale;
|
||||
@@ -49,9 +50,8 @@ void rotateIMU(Vector& data) {
|
||||
}
|
||||
|
||||
void calibrateGyroOnce() {
|
||||
static float landedTime = 0;
|
||||
landedTime = landed ? landedTime + dt : 0;
|
||||
if (landedTime < 2) return; // calibrate only if definitely stationary
|
||||
static Delay landedDelay(2);
|
||||
if (!landedDelay.update(landed)) return; // calibrate only if definitely stationary
|
||||
|
||||
static LowPassFilter<Vector> gyroCalibrationFilter(0.001);
|
||||
gyroBias = gyroCalibrationFilter.update(gyro);
|
||||
@@ -59,7 +59,7 @@ void calibrateGyroOnce() {
|
||||
|
||||
void calibrateAccel() {
|
||||
print("Calibrating accelerometer\n");
|
||||
IMU.setAccelRange(IMU.ACCEL_RANGE_2G); // the most sensitive mode
|
||||
imu.setAccelRange(imu.ACCEL_RANGE_2G); // the most sensitive mode
|
||||
|
||||
print("1/6 Place level [8 sec]\n");
|
||||
pause(8);
|
||||
@@ -93,9 +93,9 @@ void calibrateAccelOnce() {
|
||||
// Compute the average of the accelerometer readings
|
||||
acc = Vector(0, 0, 0);
|
||||
for (int i = 0; i < samples; i++) {
|
||||
IMU.waitForData();
|
||||
imu.waitForData();
|
||||
Vector sample;
|
||||
IMU.getAccel(sample.x, sample.y, sample.z);
|
||||
imu.getAccel(sample.x, sample.y, sample.z);
|
||||
acc = acc + sample;
|
||||
}
|
||||
acc = acc / samples;
|
||||
@@ -119,7 +119,16 @@ void printIMUCalibration() {
|
||||
}
|
||||
|
||||
void printIMUInfo() {
|
||||
IMU.status() ? print("status: ERROR %d\n", IMU.status()) : print("status: OK\n");
|
||||
print("model: %s\n", IMU.getModel());
|
||||
print("who am I: 0x%02X\n", IMU.whoAmI());
|
||||
imu.status() ? print("status: ERROR %d\n", imu.status()) : print("status: OK\n");
|
||||
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("acc: %f %f %f\n", acc.x, acc.y, acc.z);
|
||||
imu.waitForData();
|
||||
Vector rawGyro, rawAcc;
|
||||
imu.getGyro(rawGyro.x, rawGyro.y, rawGyro.z);
|
||||
imu.getAccel(rawAcc.x, rawAcc.y, rawAcc.z);
|
||||
print("raw gyro: %f %f %f\n", rawGyro.x, rawGyro.y, rawGyro.z);
|
||||
print("raw acc: %f %f %f\n", rawAcc.x, rawAcc.y, rawAcc.z);
|
||||
}
|
||||
|
||||
@@ -10,7 +10,6 @@
|
||||
#define LOG_PERIOD 1.0 / LOG_RATE
|
||||
#define LOG_SIZE LOG_DURATION * LOG_RATE
|
||||
|
||||
float tFloat;
|
||||
Vector attitudeEuler;
|
||||
Vector attitudeTargetEuler;
|
||||
|
||||
@@ -20,7 +19,7 @@ struct LogEntry {
|
||||
};
|
||||
|
||||
LogEntry logEntries[] = {
|
||||
{"t", &tFloat},
|
||||
{"t", &t},
|
||||
{"rates.x", &rates.x},
|
||||
{"rates.y", &rates.y},
|
||||
{"rates.z", &rates.z},
|
||||
@@ -40,7 +39,6 @@ const int logColumns = sizeof(logEntries) / sizeof(logEntries[0]);
|
||||
float logBuffer[LOG_SIZE][logColumns];
|
||||
|
||||
void prepareLogData() {
|
||||
tFloat = t;
|
||||
attitudeEuler = attitude.toEuler();
|
||||
attitudeTargetEuler = attitudeTarget.toEuler();
|
||||
}
|
||||
@@ -48,7 +46,7 @@ void prepareLogData() {
|
||||
void logData() {
|
||||
if (!armed) return;
|
||||
static int logPointer = 0;
|
||||
static double logTime = 0;
|
||||
static float logTime = 0;
|
||||
if (t - logTime < LOG_PERIOD) return;
|
||||
logTime = t;
|
||||
|
||||
|
||||
@@ -12,11 +12,11 @@
|
||||
#define PERIOD_FAST 0.1
|
||||
#define MAVLINK_CONTROL_YAW_DEAD_ZONE 0.1f
|
||||
|
||||
float mavlinkControlScale = 0.7;
|
||||
bool mavlinkConnected = false;
|
||||
String mavlinkPrintBuffer;
|
||||
|
||||
extern double controlTime;
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlArmed, controlMode;
|
||||
extern float controlTime;
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
|
||||
|
||||
void processMavlink() {
|
||||
sendMavlink();
|
||||
@@ -26,8 +26,8 @@ void processMavlink() {
|
||||
void sendMavlink() {
|
||||
sendMavlinkPrint();
|
||||
|
||||
static double lastSlow = 0;
|
||||
static double lastFast = 0;
|
||||
static float lastSlow = 0;
|
||||
static float lastFast = 0;
|
||||
|
||||
mavlink_message_t msg;
|
||||
uint32_t time = t * 1000;
|
||||
@@ -36,16 +36,20 @@ void sendMavlink() {
|
||||
lastSlow = t;
|
||||
|
||||
mavlink_msg_heartbeat_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, MAV_TYPE_QUADROTOR, MAV_AUTOPILOT_GENERIC,
|
||||
MAV_MODE_FLAG_MANUAL_INPUT_ENABLED | (armed * MAV_MODE_FLAG_SAFETY_ARMED) | ((mode == STAB) * MAV_MODE_FLAG_STABILIZE_ENABLED),
|
||||
(armed ? MAV_MODE_FLAG_SAFETY_ARMED : 0) |
|
||||
((mode == STAB) ? MAV_MODE_FLAG_STABILIZE_ENABLED : 0) |
|
||||
((mode == AUTO) ? MAV_MODE_FLAG_AUTO_ENABLED : MAV_MODE_FLAG_MANUAL_INPUT_ENABLED),
|
||||
mode, MAV_STATE_STANDBY);
|
||||
sendMessage(&msg);
|
||||
|
||||
if (!mavlinkConnected) return; // send only heartbeat until connected
|
||||
|
||||
mavlink_msg_extended_sys_state_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
|
||||
MAV_VTOL_STATE_UNDEFINED, landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR);
|
||||
sendMessage(&msg);
|
||||
}
|
||||
|
||||
if (t - lastFast >= PERIOD_FAST) {
|
||||
if (t - lastFast >= PERIOD_FAST && mavlinkConnected) {
|
||||
lastFast = t;
|
||||
|
||||
const float zeroQuat[] = {0, 0, 0, 0};
|
||||
@@ -57,9 +61,9 @@ void sendMavlink() {
|
||||
channels[0], channels[1], channels[2], channels[3], channels[4], channels[5], channels[6], channels[7], UINT8_MAX);
|
||||
if (channels[0] != 0) sendMessage(&msg); // 0 means no RC input
|
||||
|
||||
float actuator[32];
|
||||
memcpy(actuator, motors, sizeof(motors));
|
||||
mavlink_msg_actuator_output_status_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time, 4, actuator);
|
||||
float controls[8];
|
||||
memcpy(controls, motors, sizeof(motors));
|
||||
mavlink_msg_actuator_control_target_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time, 0, controls);
|
||||
sendMessage(&msg);
|
||||
|
||||
mavlink_msg_scaled_imu_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time,
|
||||
@@ -79,6 +83,7 @@ void sendMessage(const void *msg) {
|
||||
void receiveMavlink() {
|
||||
uint8_t buf[MAVLINK_MAX_PACKET_LEN];
|
||||
int len = receiveWiFi(buf, MAVLINK_MAX_PACKET_LEN);
|
||||
if (len) mavlinkConnected = true;
|
||||
|
||||
// New packet, parse it
|
||||
mavlink_message_t msg;
|
||||
@@ -99,11 +104,10 @@ void handleMavlink(const void *_msg) {
|
||||
if (m.target && m.target != SYSTEM_ID) return; // 0 is broadcast
|
||||
|
||||
controlThrottle = m.z / 1000.0f;
|
||||
controlPitch = m.x / 1000.0f * mavlinkControlScale;
|
||||
controlRoll = m.y / 1000.0f * mavlinkControlScale;
|
||||
controlYaw = m.r / 1000.0f * mavlinkControlScale;
|
||||
controlMode = 1; // STAB mode
|
||||
controlArmed = 1; // armed
|
||||
controlPitch = m.x / 1000.0f;
|
||||
controlRoll = m.y / 1000.0f;
|
||||
controlYaw = m.r / 1000.0f;
|
||||
controlMode = NAN;
|
||||
controlTime = t;
|
||||
|
||||
if (abs(controlYaw) < MAVLINK_CONTROL_YAW_DEAD_ZONE) controlYaw = 0;
|
||||
@@ -174,24 +178,73 @@ void handleMavlink(const void *_msg) {
|
||||
doCommand(data, true);
|
||||
}
|
||||
|
||||
if (msg.msgid == MAVLINK_MSG_ID_SET_ATTITUDE_TARGET) {
|
||||
if (mode != AUTO) return;
|
||||
|
||||
mavlink_set_attitude_target_t m;
|
||||
mavlink_msg_set_attitude_target_decode(&msg, &m);
|
||||
if (m.target_system && m.target_system != SYSTEM_ID) return;
|
||||
|
||||
// copy attitude, rates and thrust targets
|
||||
ratesTarget.x = m.body_roll_rate;
|
||||
ratesTarget.y = -m.body_pitch_rate; // convert to flu
|
||||
ratesTarget.z = -m.body_yaw_rate;
|
||||
attitudeTarget.w = m.q[0];
|
||||
attitudeTarget.x = m.q[1];
|
||||
attitudeTarget.y = -m.q[2];
|
||||
attitudeTarget.z = -m.q[3];
|
||||
thrustTarget = m.thrust;
|
||||
ratesExtra = Vector(0, 0, 0);
|
||||
|
||||
if (m.type_mask & ATTITUDE_TARGET_TYPEMASK_ATTITUDE_IGNORE) attitudeTarget.invalidate();
|
||||
armed = m.thrust > 0;
|
||||
}
|
||||
|
||||
if (msg.msgid == MAVLINK_MSG_ID_SET_ACTUATOR_CONTROL_TARGET) {
|
||||
if (mode != AUTO) return;
|
||||
|
||||
mavlink_set_actuator_control_target_t m;
|
||||
mavlink_msg_set_actuator_control_target_decode(&msg, &m);
|
||||
if (m.target_system && m.target_system != SYSTEM_ID) return;
|
||||
|
||||
attitudeTarget.invalidate();
|
||||
ratesTarget.invalidate();
|
||||
torqueTarget.invalidate();
|
||||
memcpy(motors, m.controls, sizeof(motors)); // copy motor thrusts
|
||||
armed = motors[0] > 0 || motors[1] > 0 || motors[2] > 0 || motors[3] > 0;
|
||||
}
|
||||
|
||||
// Handle commands
|
||||
if (msg.msgid == MAVLINK_MSG_ID_COMMAND_LONG) {
|
||||
mavlink_command_long_t m;
|
||||
mavlink_msg_command_long_decode(&msg, &m);
|
||||
if (m.target_system && m.target_system != SYSTEM_ID) return;
|
||||
mavlink_message_t ack;
|
||||
mavlink_message_t response;
|
||||
bool accepted = false;
|
||||
|
||||
if (m.command == MAV_CMD_REQUEST_MESSAGE && m.param1 == MAVLINK_MSG_ID_AUTOPILOT_VERSION) {
|
||||
mavlink_msg_command_ack_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &ack, m.command, MAV_RESULT_ACCEPTED, UINT8_MAX, 0, msg.sysid, msg.compid);
|
||||
sendMessage(&ack);
|
||||
accepted = true;
|
||||
mavlink_msg_autopilot_version_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &response,
|
||||
MAV_PROTOCOL_CAPABILITY_PARAM_FLOAT | MAV_PROTOCOL_CAPABILITY_MAVLINK2, 1, 0, 1, 1, 0, 0, 0, 0, 0, 0, 0);
|
||||
sendMessage(&response);
|
||||
} else {
|
||||
mavlink_msg_command_ack_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &ack, m.command, MAV_RESULT_UNSUPPORTED, UINT8_MAX, 0, msg.sysid, msg.compid);
|
||||
sendMessage(&ack);
|
||||
}
|
||||
|
||||
if (m.command == MAV_CMD_COMPONENT_ARM_DISARM) {
|
||||
if (m.param1 && controlThrottle > 0.05) return; // don't arm if throttle is not low
|
||||
accepted = true;
|
||||
armed = m.param1 == 1;
|
||||
}
|
||||
|
||||
if (m.command == MAV_CMD_DO_SET_MODE) {
|
||||
if (m.param2 < 0 || m.param2 > AUTO) return; // incorrect mode
|
||||
accepted = true;
|
||||
mode = m.param2;
|
||||
}
|
||||
|
||||
// send command ack
|
||||
mavlink_message_t ack;
|
||||
mavlink_msg_command_ack_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &ack, m.command, accepted ? MAV_RESULT_ACCEPTED : MAV_RESULT_UNSUPPORTED, UINT8_MAX, 0, msg.sysid, msg.compid);
|
||||
sendMessage(&ack);
|
||||
}
|
||||
}
|
||||
|
||||
|
||||
@@ -25,30 +25,32 @@ const int MOTOR_FRONT_LEFT = 3;
|
||||
|
||||
void setupMotors() {
|
||||
print("Setup Motors\n");
|
||||
|
||||
// configure pins
|
||||
#ifdef ESP32
|
||||
ledcAttach(MOTOR_0_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
|
||||
ledcAttach(MOTOR_1_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
|
||||
ledcAttach(MOTOR_2_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
|
||||
ledcAttach(MOTOR_3_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
|
||||
|
||||
#else
|
||||
analogWriteResolution(PWM_RESOLUTION);
|
||||
analogWriteFrequency(PWM_FREQUENCY);
|
||||
#endif
|
||||
sendMotors();
|
||||
print("Motors initialized\n");
|
||||
}
|
||||
|
||||
int getDutyCycle(float value) {
|
||||
value = constrain(value, 0, 1);
|
||||
float pwm = mapff(value, 0, 1, PWM_MIN, PWM_MAX);
|
||||
float pwm = mapf(value, 0, 1, PWM_MIN, PWM_MAX);
|
||||
if (value == 0) pwm = PWM_STOP;
|
||||
float duty = mapff(pwm, 0, 1000000 / PWM_FREQUENCY, 0, (1 << PWM_RESOLUTION) - 1);
|
||||
float duty = mapf(pwm, 0, 1000000 / PWM_FREQUENCY, 0, (1 << PWM_RESOLUTION) - 1);
|
||||
return round(duty);
|
||||
}
|
||||
|
||||
void sendMotors() {
|
||||
ledcWrite(MOTOR_0_PIN, getDutyCycle(motors[0]));
|
||||
ledcWrite(MOTOR_1_PIN, getDutyCycle(motors[1]));
|
||||
ledcWrite(MOTOR_2_PIN, getDutyCycle(motors[2]));
|
||||
ledcWrite(MOTOR_3_PIN, getDutyCycle(motors[3]));
|
||||
analogWrite(MOTOR_0_PIN, getDutyCycle(motors[0]));
|
||||
analogWrite(MOTOR_1_PIN, getDutyCycle(motors[1]));
|
||||
analogWrite(MOTOR_2_PIN, getDutyCycle(motors[2]));
|
||||
analogWrite(MOTOR_3_PIN, getDutyCycle(motors[3]));
|
||||
}
|
||||
|
||||
bool motorsActive() {
|
||||
|
||||
@@ -8,7 +8,6 @@
|
||||
extern float channelZero[16];
|
||||
extern float channelMax[16];
|
||||
extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
|
||||
extern float mavlinkControlScale;
|
||||
|
||||
Preferences storage;
|
||||
|
||||
@@ -70,12 +69,7 @@ Parameter parameters[] = {
|
||||
{"RC_PITCH", &pitchChannel},
|
||||
{"RC_THROTTLE", &throttleChannel},
|
||||
{"RC_YAW", &yawChannel},
|
||||
{"RC_ARMED", &armedChannel},
|
||||
{"RC_MODE", &modeChannel},
|
||||
#if WIFI_ENABLED
|
||||
// MAVLink
|
||||
{"MAV_CTRL_SCALE", &mavlinkControlScale},
|
||||
#endif
|
||||
};
|
||||
|
||||
void setupParameters() {
|
||||
@@ -124,7 +118,7 @@ bool setParameter(const char *name, const float value) {
|
||||
}
|
||||
|
||||
void syncParameters() {
|
||||
static double lastSync = 0;
|
||||
static float lastSync = 0;
|
||||
if (t - lastSync < 1) return; // sync once per second
|
||||
if (motorsActive()) return; // don't use flash while flying, it may cause a delay
|
||||
lastSync = t;
|
||||
|
||||
30
flix/pid.h
@@ -9,40 +9,44 @@
|
||||
|
||||
class PID {
|
||||
public:
|
||||
float p = 0;
|
||||
float i = 0;
|
||||
float d = 0;
|
||||
float windup = 0;
|
||||
float p, i, d;
|
||||
float windup;
|
||||
float dtMax;
|
||||
|
||||
float derivative = 0;
|
||||
float integral = 0;
|
||||
|
||||
LowPassFilter<float> lpf; // low pass filter for derivative term
|
||||
|
||||
PID(float p, float i, float d, float windup = 0, float dAlpha = 1) : p(p), i(i), d(d), windup(windup), lpf(dAlpha) {};
|
||||
PID(float p, float i, float d, float windup = 0, float dAlpha = 1, float dtMax = 0.1) :
|
||||
p(p), i(i), d(d), windup(windup), lpf(dAlpha), dtMax(dtMax) {}
|
||||
|
||||
float update(float error, float dt) {
|
||||
integral += error * dt;
|
||||
float update(float error) {
|
||||
float dt = t - prevTime;
|
||||
|
||||
if (isfinite(prevError) && dt > 0) {
|
||||
// calculate derivative if both dt and prevError are valid
|
||||
derivative = (error - prevError) / dt;
|
||||
|
||||
// apply low pass filter to derivative
|
||||
derivative = lpf.update(derivative);
|
||||
if (dt > 0 && dt < dtMax) {
|
||||
integral += error * dt;
|
||||
derivative = lpf.update((error - prevError) / dt); // compute derivative and apply low-pass filter
|
||||
} else {
|
||||
integral = 0;
|
||||
derivative = 0;
|
||||
}
|
||||
|
||||
prevError = error;
|
||||
prevTime = t;
|
||||
|
||||
return p * error + constrain(i * integral, -windup, windup) + d * derivative; // PID
|
||||
}
|
||||
|
||||
void reset() {
|
||||
prevError = NAN;
|
||||
prevTime = NAN;
|
||||
integral = 0;
|
||||
derivative = 0;
|
||||
lpf.reset();
|
||||
}
|
||||
|
||||
private:
|
||||
float prevError = NAN;
|
||||
float prevTime = NAN;
|
||||
};
|
||||
|
||||
@@ -45,7 +45,7 @@ public:
|
||||
cx * cy * sz - sx * sy * cz);
|
||||
}
|
||||
|
||||
static Quaternion fromBetweenVectors(Vector u, Vector v) {
|
||||
static Quaternion fromBetweenVectors(const Vector& u, const Vector& v) {
|
||||
float dot = u.x * v.x + u.y * v.y + u.z * v.z;
|
||||
float w1 = u.y * v.z - u.z * v.y;
|
||||
float w2 = u.z * v.x - u.x * v.z;
|
||||
@@ -64,6 +64,22 @@ public:
|
||||
return isfinite(w) && isfinite(x) && isfinite(y) && isfinite(z);
|
||||
}
|
||||
|
||||
bool valid() const {
|
||||
return finite();
|
||||
}
|
||||
|
||||
bool invalid() const {
|
||||
return !valid();
|
||||
}
|
||||
|
||||
void invalidate() {
|
||||
w = NAN;
|
||||
x = NAN;
|
||||
y = NAN;
|
||||
z = NAN;
|
||||
}
|
||||
|
||||
|
||||
float norm() const {
|
||||
return sqrt(w * w + x * x + y * y + z * z);
|
||||
}
|
||||
@@ -116,29 +132,31 @@ public:
|
||||
return euler;
|
||||
}
|
||||
|
||||
float getRoll() const {
|
||||
return toEuler().x;
|
||||
}
|
||||
|
||||
float getPitch() const {
|
||||
return toEuler().y;
|
||||
}
|
||||
|
||||
float getYaw() const {
|
||||
// https://github.com/ros/geometry2/blob/589caf083cae9d8fae7effdb910454b4681b9ec1/tf2/include/tf2/impl/utils.h#L122
|
||||
float yaw;
|
||||
float sqx = x * x;
|
||||
float sqy = y * y;
|
||||
float sqz = z * z;
|
||||
float sqw = w * w;
|
||||
double sarg = -2 * (x * z - w * y) / (sqx + sqy + sqz + sqw);
|
||||
if (sarg <= -0.99999) {
|
||||
yaw = -2 * atan2(y, x);
|
||||
} else if (sarg >= 0.99999) {
|
||||
yaw = 2 * atan2(y, x);
|
||||
} else {
|
||||
yaw = atan2(2 * (x * y + w * z), sqw + sqx - sqy - sqz);
|
||||
}
|
||||
return yaw;
|
||||
return toEuler().z;
|
||||
}
|
||||
|
||||
void setRoll(float roll) {
|
||||
Vector euler = toEuler();
|
||||
*this = Quaternion::fromEuler(Vector(roll, euler.y, euler.z));
|
||||
}
|
||||
|
||||
void setPitch(float pitch) {
|
||||
Vector euler = toEuler();
|
||||
*this = Quaternion::fromEuler(Vector(euler.x, pitch, euler.z));
|
||||
}
|
||||
|
||||
void setYaw(float yaw) {
|
||||
// TODO: optimize?
|
||||
Vector euler = toEuler();
|
||||
euler.z = yaw;
|
||||
(*this) = Quaternion::fromEuler(euler);
|
||||
*this = Quaternion::fromEuler(Vector(euler.x, euler.y, yaw));
|
||||
}
|
||||
|
||||
Quaternion operator * (const Quaternion& q) const {
|
||||
|
||||
31
flix/rc.ino
@@ -6,24 +6,24 @@
|
||||
#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); // NOTE: Use RC(Serial2, 16, 17) if you use the old UART2 pins
|
||||
|
||||
uint16_t channels[16]; // raw rc channels
|
||||
double controlTime; // time of the last controls update
|
||||
float controlTime; // time of the last controls update
|
||||
float channelZero[16]; // calibration zero values
|
||||
float channelMax[16]; // calibration max values
|
||||
|
||||
// Channels mapping (using float to store in parameters):
|
||||
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, armedChannel = NAN, modeChannel = NAN;
|
||||
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
|
||||
|
||||
void setupRC() {
|
||||
print("Setup RC\n");
|
||||
RC.begin();
|
||||
rc.begin();
|
||||
}
|
||||
|
||||
bool readRC() {
|
||||
if (RC.read()) {
|
||||
SBUSData data = RC.data();
|
||||
if (rc.read()) {
|
||||
SBUSData data = rc.data();
|
||||
for (int i = 0; i < 16; i++) channels[i] = data.ch[i]; // copy channels data
|
||||
normalizeRC();
|
||||
controlTime = t;
|
||||
@@ -42,7 +42,6 @@ void normalizeRC() {
|
||||
controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : NAN;
|
||||
controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : NAN;
|
||||
controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : NAN;
|
||||
controlArmed = armedChannel >= 0 ? controls[(int)armedChannel] : 1; // assume armed by default
|
||||
controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN;
|
||||
}
|
||||
|
||||
@@ -50,16 +49,15 @@ void calibrateRC() {
|
||||
uint16_t zero[16];
|
||||
uint16_t center[16];
|
||||
uint16_t max[16];
|
||||
print("1/9 Calibrating RC: put all switches to default positions [3 sec]\n");
|
||||
print("1/8 Calibrating RC: put all switches to default positions [3 sec]\n");
|
||||
pause(3);
|
||||
calibrateRCChannel(NULL, zero, zero, "2/9 Move sticks [3 sec]\n... ...\n... .o.\n.o. ...\n");
|
||||
calibrateRCChannel(NULL, center, center, "3/9 Move sticks [3 sec]\n... ...\n.o. .o.\n... ...\n");
|
||||
calibrateRCChannel(&throttleChannel, zero, max, "4/9 Move sticks [3 sec]\n.o. ...\n... .o.\n... ...\n");
|
||||
calibrateRCChannel(&yawChannel, center, max, "5/9 Move sticks [3 sec]\n... ...\n..o .o.\n... ...\n");
|
||||
calibrateRCChannel(&pitchChannel, zero, max, "6/9 Move sticks [3 sec]\n... .o.\n... ...\n.o. ...\n");
|
||||
calibrateRCChannel(&rollChannel, zero, max, "7/9 Move sticks [3 sec]\n... ...\n... ..o\n.o. ...\n");
|
||||
calibrateRCChannel(&armedChannel, zero, max, "8/9 Switch to armed [3 sec]\n");
|
||||
calibrateRCChannel(&modeChannel, zero, max, "9/9 Disarm and switch mode to max [3 sec]\n");
|
||||
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");
|
||||
printRCCalibration();
|
||||
}
|
||||
|
||||
@@ -94,6 +92,5 @@ void printRCCalibration() {
|
||||
print("Pitch %-7g%-7g%-7g\n", pitchChannel, pitchChannel >= 0 ? channelZero[(int)pitchChannel] : NAN, pitchChannel >= 0 ? channelMax[(int)pitchChannel] : NAN);
|
||||
print("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("Armed %-7g%-7g%-7g\n", armedChannel, armedChannel >= 0 ? channelZero[(int)armedChannel] : NAN, armedChannel >= 0 ? channelMax[(int)armedChannel] : NAN);
|
||||
print("Mode %-7g%-7g%-7g\n", modeChannel, modeChannel >= 0 ? channelZero[(int)modeChannel] : NAN, modeChannel >= 0 ? channelMax[(int)modeChannel] : NAN);
|
||||
}
|
||||
|
||||
48
flix/safety.ino
Normal file
@@ -0,0 +1,48 @@
|
||||
// Copyright (c) 2024 Oleg Kalachev <okalachev@gmail.com>
|
||||
// Repository: https://github.com/okalachev/flix
|
||||
|
||||
// Fail-safe functions
|
||||
|
||||
#define RC_LOSS_TIMEOUT 1
|
||||
#define DESCEND_TIME 10
|
||||
|
||||
extern float controlTime;
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw;
|
||||
|
||||
void failsafe() {
|
||||
rcLossFailsafe();
|
||||
autoFailsafe();
|
||||
}
|
||||
|
||||
// RC loss failsafe
|
||||
void rcLossFailsafe() {
|
||||
if (controlTime == 0) return; // no RC at all
|
||||
if (!armed) return;
|
||||
if (t - controlTime > RC_LOSS_TIMEOUT) {
|
||||
descend();
|
||||
}
|
||||
}
|
||||
|
||||
// Smooth descend on RC lost
|
||||
void descend() {
|
||||
mode = AUTO;
|
||||
attitudeTarget = Quaternion();
|
||||
thrustTarget -= dt / DESCEND_TIME;
|
||||
if (thrustTarget < 0) {
|
||||
thrustTarget = 0;
|
||||
armed = false;
|
||||
}
|
||||
}
|
||||
|
||||
// Allow pilot to interrupt automatic flight
|
||||
void autoFailsafe() {
|
||||
static float roll, pitch, yaw, throttle;
|
||||
if (roll != controlRoll || pitch != controlPitch || yaw != controlYaw || abs(throttle - controlThrottle) > 0.05) {
|
||||
// controls changed
|
||||
if (mode == AUTO) mode = STAB; // regain control by the pilot
|
||||
}
|
||||
roll = controlRoll;
|
||||
pitch = controlPitch;
|
||||
yaw = controlYaw;
|
||||
throttle = controlThrottle;
|
||||
}
|
||||
@@ -6,7 +6,7 @@
|
||||
float loopRate; // Hz
|
||||
|
||||
void step() {
|
||||
double now = micros() / 1000000.0;
|
||||
float now = micros() / 1000000.0;
|
||||
dt = now - t;
|
||||
t = now;
|
||||
|
||||
@@ -18,7 +18,7 @@ void step() {
|
||||
}
|
||||
|
||||
void computeLoopRate() {
|
||||
static double windowStart = 0;
|
||||
static float windowStart = 0;
|
||||
static uint32_t rate = 0;
|
||||
rate++;
|
||||
if (t - windowStart >= 1) { // 1 second window
|
||||
|
||||
37
flix/util.h
@@ -6,17 +6,24 @@
|
||||
#pragma once
|
||||
|
||||
#include <math.h>
|
||||
#ifdef ESP32
|
||||
#include <soc/soc.h>
|
||||
#include <soc/rtc_cntl_reg.h>
|
||||
#endif
|
||||
|
||||
const float ONE_G = 9.80665;
|
||||
extern float t;
|
||||
|
||||
float mapf(long x, long in_min, long in_max, float out_min, float out_max) {
|
||||
return (float)(x - in_min) * (out_max - out_min) / (float)(in_max - in_min) + out_min;
|
||||
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;
|
||||
}
|
||||
|
||||
float mapff(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) {
|
||||
return !isfinite(x);
|
||||
}
|
||||
|
||||
bool valid(float x) {
|
||||
return isfinite(x);
|
||||
}
|
||||
|
||||
// Wrap angle to [-PI, PI)
|
||||
@@ -32,7 +39,9 @@ float wrapAngle(float angle) {
|
||||
|
||||
// Disable reset on low voltage
|
||||
void disableBrownOut() {
|
||||
#ifdef ESP32
|
||||
REG_CLR_BIT(RTC_CNTL_BROWN_OUT_REG, RTC_CNTL_BROWN_OUT_ENA);
|
||||
#endif
|
||||
}
|
||||
|
||||
// Trim and split string by spaces
|
||||
@@ -44,3 +53,23 @@ void splitString(String& str, String& token0, String& token1, String& token2) {
|
||||
token1 = strtok(NULL, " "); // String(NULL) creates empty string
|
||||
token2 = strtok(NULL, "");
|
||||
}
|
||||
|
||||
// Delay filter for boolean signals - ensures the signal is on for at least 'delay' seconds
|
||||
class Delay {
|
||||
public:
|
||||
float delay;
|
||||
float start = NAN;
|
||||
|
||||
Delay(float delay) : delay(delay) {}
|
||||
|
||||
bool update(bool on) {
|
||||
if (!on) {
|
||||
start = NAN;
|
||||
return false;
|
||||
}
|
||||
if (isnan(start)) {
|
||||
start = t;
|
||||
}
|
||||
return t - start >= delay;
|
||||
}
|
||||
};
|
||||
|
||||
@@ -21,6 +21,21 @@ public:
|
||||
return isfinite(x) && isfinite(y) && isfinite(z);
|
||||
}
|
||||
|
||||
bool valid() const {
|
||||
return finite();
|
||||
}
|
||||
|
||||
bool invalid() const {
|
||||
return !valid();
|
||||
}
|
||||
|
||||
void invalidate() {
|
||||
x = NAN;
|
||||
y = NAN;
|
||||
z = NAN;
|
||||
}
|
||||
|
||||
|
||||
float norm() const {
|
||||
return sqrt(x * x + y * y + z * z);
|
||||
}
|
||||
|
||||
@@ -13,6 +13,7 @@
|
||||
#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;
|
||||
|
||||
@@ -24,7 +25,7 @@ void setupWiFi() {
|
||||
|
||||
void sendWiFi(const uint8_t *buf, int len) {
|
||||
if (WiFi.softAPIP() == IPAddress(0, 0, 0, 0) && WiFi.status() != WL_CONNECTED) return;
|
||||
udp.beginPacket(WiFi.softAPBroadcastIP(), WIFI_UDP_REMOTE_PORT);
|
||||
udp.beginPacket(udp.remoteIP() ? udp.remoteIP() : WIFI_UDP_REMOTE_ADDR, WIFI_UDP_REMOTE_PORT);
|
||||
udp.write(buf, len);
|
||||
udp.endPacket();
|
||||
}
|
||||
|
||||
@@ -1,7 +1,7 @@
|
||||
cmake_minimum_required(VERSION 3.5 FATAL_ERROR)
|
||||
project(flix_gazebo)
|
||||
|
||||
# === gazebo plugin
|
||||
# Gazebo plugin
|
||||
find_package(gazebo REQUIRED)
|
||||
find_package(SDL2 REQUIRED)
|
||||
include_directories(${GAZEBO_INCLUDE_DIRS})
|
||||
|
||||
@@ -4,7 +4,7 @@
|
||||
|
||||
## Building and running
|
||||
|
||||
See [building and running instructions](../docs/build.md#simulation).
|
||||
See [building and running instructions](../docs/usage.md#simulation).
|
||||
|
||||
## Code structure
|
||||
|
||||
|
||||
@@ -12,10 +12,11 @@
|
||||
|
||||
#define WIFI_ENABLED 1
|
||||
|
||||
double t = NAN;
|
||||
float t = NAN;
|
||||
float dt;
|
||||
float motors[4];
|
||||
float controlRoll, controlPitch, controlYaw, controlThrottle, controlArmed, controlMode;
|
||||
float controlRoll, controlPitch, controlYaw, controlThrottle = NAN;
|
||||
float controlMode = NAN;
|
||||
Vector acc;
|
||||
Vector gyro;
|
||||
Vector rates;
|
||||
@@ -28,9 +29,9 @@ void computeLoopRate();
|
||||
void applyGyro();
|
||||
void applyAcc();
|
||||
void control();
|
||||
void interpretRC();
|
||||
void interpretControls();
|
||||
void controlAttitude();
|
||||
void controlRate();
|
||||
void controlRates();
|
||||
void controlTorque();
|
||||
const char* getModeName();
|
||||
void sendMotors();
|
||||
@@ -54,9 +55,9 @@ void mavlinkPrint(const char* str);
|
||||
void sendMavlinkPrint();
|
||||
inline Quaternion fluToFrd(const Quaternion &q);
|
||||
void failsafe();
|
||||
void armingFailsafe();
|
||||
void rcLossFailsafe();
|
||||
void descend();
|
||||
void autoFailsafe();
|
||||
int parametersCount();
|
||||
const char *getParameterName(int index);
|
||||
float getParameter(int index);
|
||||
|
||||
@@ -21,7 +21,7 @@
|
||||
#include "cli.ino"
|
||||
#include "control.ino"
|
||||
#include "estimate.ino"
|
||||
#include "failsafe.ino"
|
||||
#include "safety.ino"
|
||||
#include "log.ino"
|
||||
#include "lpf.h"
|
||||
#include "mavlink.ino"
|
||||
@@ -59,6 +59,7 @@ public:
|
||||
|
||||
void OnReset() {
|
||||
attitude = Quaternion(); // reset estimated attitude
|
||||
armed = false;
|
||||
__resetTime += __micros;
|
||||
gzmsg << "Flix plugin reset" << endl;
|
||||
}
|
||||
|
||||
@@ -13,6 +13,7 @@
|
||||
|
||||
#define WIFI_UDP_PORT 14580
|
||||
#define WIFI_UDP_REMOTE_PORT 14550
|
||||
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
|
||||
|
||||
int wifiSocket;
|
||||
|
||||
@@ -35,7 +36,7 @@ void sendWiFi(const uint8_t *buf, int len) {
|
||||
if (wifiSocket == 0) setupWiFi();
|
||||
sockaddr_in addr; // remote address
|
||||
addr.sin_family = AF_INET;
|
||||
addr.sin_addr.s_addr = INADDR_BROADCAST; // send UDP broadcast
|
||||
addr.sin_addr.s_addr = inet_addr(WIFI_UDP_REMOTE_ADDR);
|
||||
addr.sin_port = htons(WIFI_UDP_REMOTE_PORT);
|
||||
sendto(wifiSocket, buf, len, 0, (sockaddr *)&addr, sizeof(addr));
|
||||
}
|
||||
|
||||
@@ -49,6 +49,8 @@ for configuration in props['configurations']:
|
||||
print('Check configuration', configuration['name'])
|
||||
|
||||
for include_path in configuration.get('includePath', []):
|
||||
if include_path.startswith('/opt/') or include_path.startswith('/usr/'): # don't check non-Arduino libs
|
||||
continue
|
||||
check_path(include_path)
|
||||
|
||||
for forced_include in configuration.get('forcedInclude', []):
|
||||
|
||||
@@ -59,6 +59,13 @@ flix.on('disconnected', lambda: print('Disconnected from Flix'))
|
||||
flix.on('print', lambda text: print(f'Flix says: {text}'))
|
||||
```
|
||||
|
||||
Unsubscribe from events using `off` method:
|
||||
|
||||
```python
|
||||
flix.off('print') # unsubscribe from print events
|
||||
flix.off(callback) # unsubscribe specific callback
|
||||
```
|
||||
|
||||
You can also wait for specific events using `wait` method. This method returns the data associated with the event:
|
||||
|
||||
```python
|
||||
@@ -66,13 +73,14 @@ gyro = flix.wait('gyro') # wait for gyroscope update
|
||||
attitude = flix.wait('attitude', timeout=3) # wait for attitude update, raise TimeoutError after 3 seconds
|
||||
```
|
||||
|
||||
The `value` argument specifies a condition for filtering events. It can be either an expected value or a callable:
|
||||
The second argument (`value`) specifies a condition for filtering events. It can be either an expected value or a callable:
|
||||
|
||||
```python
|
||||
flix.wait('armed', value=True) # wait until armed
|
||||
flix.wait('armed', value=False) # wait until disarmed
|
||||
flix.wait('motors', value=lambda motors: not any(motors)) # wait until all motors stop
|
||||
flix.wait('attitude_euler', value=lambda att: att[0] > 0) # wait until roll angle is positive
|
||||
flix.wait('armed', True) # wait until armed
|
||||
flix.wait('armed', False) # wait until disarmed
|
||||
flix.wait('mode', 'AUTO') # wait until flight mode is switched to AUTO
|
||||
flix.wait('motors', lambda motors: not any(motors)) # wait until all motors stop
|
||||
flix.wait('attitude_euler', lambda att: att[0] > 0) # wait until roll angle is positive
|
||||
```
|
||||
|
||||
Full list of events:
|
||||
@@ -107,7 +115,7 @@ 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
|
||||
flix.set_param('PITCH_P', 5) # set parameter value
|
||||
```
|
||||
|
||||
Execute CLI commands using `cli` method. This method returns command response:
|
||||
@@ -121,21 +129,65 @@ flix.cli('reboot') # reboot the drone
|
||||
> [!TIP]
|
||||
> Use `help` command to get the list of available commands.
|
||||
|
||||
You can arm and disarm the drone using `set_armed` method (warning: the drone will fall if disarmed in the air):
|
||||
|
||||
```python
|
||||
flix.set_armed(True) # arm the drone
|
||||
flix.set_armed(False) # disarm the drone
|
||||
```
|
||||
|
||||
You can imitate pilot's controls using `set_controls` method:
|
||||
|
||||
```python
|
||||
flix.set_controls(roll=0, pitch=0, yaw=0, throttle=0.6)
|
||||
```
|
||||
|
||||
> [!WARNING]
|
||||
> This method **is not intended for automatic flights**, only for adding support for a custom pilot input device.
|
||||
|
||||
### Automatic flight
|
||||
|
||||
The flight control feature is in development. List of methods intended for automatic flight control:
|
||||
To perform automatic flight, switch the mode to *AUTO*, either from the remote control, or from the code:
|
||||
|
||||
* `set_position`
|
||||
* `set_velocity`
|
||||
* `set_attitude`
|
||||
* `set_rates`
|
||||
* `set_motors`
|
||||
* `set_controls`
|
||||
* `set_mode`
|
||||
```python
|
||||
flix.set_mode('AUTO')
|
||||
```
|
||||
|
||||
In this mode you can set flight control targets. Setting attitude target:
|
||||
|
||||
```python
|
||||
flix.set_attitude([0.1, 0.2, 0.3], 0.6) # set target roll, pitch, yaw and thrust
|
||||
flix.set_attitude([1, 0, 0, 0], 0.6) # set target attitude quaternion and thrust
|
||||
```
|
||||
|
||||
Setting angular rates target:
|
||||
|
||||
```python
|
||||
flix.set_rates([0.1, 0.2, 0.3], 0.6) # set target roll rate, pitch rate, yaw rate and thrust
|
||||
```
|
||||
|
||||
You also can control raw motors outputs directly:
|
||||
|
||||
```python
|
||||
flix.set_motors([0.5, 0.5, 0.5, 0.5]) # set motors outputs in range [0, 1]
|
||||
```
|
||||
|
||||
In *AUTO* mode, the drone will arm automatically if the thrust is greater than zero, and disarm if thrust is zero. Therefore, to disarm the drone, set thrust to zero:
|
||||
|
||||
```python
|
||||
flix.set_attitude([0, 0, 0], 0) # disarm the drone
|
||||
```
|
||||
|
||||
The following methods are in development and are not functional yet:
|
||||
|
||||
* `set_position` — set target position.
|
||||
* `set_velocity` — set target velocity.
|
||||
|
||||
To exit from *AUTO* mode move control sticks and the drone will switch to *STAB* mode.
|
||||
|
||||
## Usage alongside QGroundControl
|
||||
|
||||
You can use the Flix library alongside the QGroundControl app, using a proxy mode. To do that:
|
||||
You can use the Flix library alongside the QGroundControl app, using proxy mode. To do that:
|
||||
|
||||
1. Run proxy for `pyflix` and QGroundControl in background:
|
||||
|
||||
@@ -151,6 +203,8 @@ You can use the Flix library alongside the QGroundControl app, using a proxy mod
|
||||
* *Port*: 14560
|
||||
4. Restart QGroundControl.
|
||||
|
||||
<img src="../../docs/img/qgc-proxy.png" width="300">
|
||||
|
||||
Now you can run `pyflix` scripts and QGroundControl simultaneously.
|
||||
|
||||
## Tools
|
||||
@@ -201,11 +255,11 @@ You can send values from the firmware like this (`mavlink.ino`):
|
||||
|
||||
```cpp
|
||||
// Send float named value
|
||||
mavlink_msg_named_value_float_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, t, "some_value", loopRate);
|
||||
mavlink_msg_named_value_float_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, t, "loop_rate", loopRate);
|
||||
sendMessage(&msg);
|
||||
|
||||
// Send vector named value
|
||||
mavlink_msg_debug_vect_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, "some_vector", t, gyroBias.x, gyroBias.y, gyroBias.z);
|
||||
mavlink_msg_debug_vect_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, "gyro_bias", t, gyroBias.x, gyroBias.y, gyroBias.z);
|
||||
sendMessage(&msg);
|
||||
```
|
||||
|
||||
|
||||
@@ -6,7 +6,7 @@
|
||||
import os
|
||||
import time
|
||||
from queue import Queue, Empty
|
||||
from typing import Literal, Optional, Callable, List, Dict, Any, Union
|
||||
from typing import Optional, Callable, List, Dict, Any, Union, Sequence
|
||||
import logging
|
||||
import errno
|
||||
from threading import Thread, Timer
|
||||
@@ -36,10 +36,11 @@ class Flix:
|
||||
|
||||
system_id: int
|
||||
messages: Dict[str, Dict[str, Any]] # MAVLink messages storage
|
||||
values: Dict[Union[str, int], Union[float, List[float]]] = {} # named values
|
||||
values: Dict[Union[str, int], Union[float, List[float]]] # named values
|
||||
|
||||
_connection_timeout = 3
|
||||
_print_buffer: str = ''
|
||||
_modes = ['MANUAL', 'ACRO', 'STAB', 'AUTO']
|
||||
|
||||
def __init__(self, system_id: int=1, wait_connection: bool=True):
|
||||
if not (0 <= system_id < 256):
|
||||
@@ -55,12 +56,11 @@ class Flix:
|
||||
if e.errno != errno.EADDRINUSE:
|
||||
raise
|
||||
# Port busy - using proxy
|
||||
logger.debug('Listening on port 14560 (proxy)')
|
||||
logger.debug('Listening on port 14555 (proxy)')
|
||||
self.connection: mavutil.mavfile = mavutil.mavlink_connection('udpin:0.0.0.0:14555', source_system=254) # type: ignore
|
||||
self.connection.target_system = system_id
|
||||
self.mavlink: mavlink.MAVLink = self.connection.mav
|
||||
self._event_listeners: Dict[str, List[Callable[..., Any]]] = {}
|
||||
self.messages = {}
|
||||
self._disconnected_timer = Timer(0, self._disconnected)
|
||||
self._reader_thread = Thread(target=self._read_mavlink, daemon=True)
|
||||
self._reader_thread.start()
|
||||
@@ -78,6 +78,8 @@ class Flix:
|
||||
self.motors = [0, 0, 0, 0]
|
||||
self.acc = [0, 0, 0]
|
||||
self.gyro = [0, 0, 0]
|
||||
self.messages = {}
|
||||
self.values = {}
|
||||
|
||||
def on(self, event: str, callback: Callable):
|
||||
event = event.lower()
|
||||
@@ -85,10 +87,15 @@ class Flix:
|
||||
self._event_listeners[event] = []
|
||||
self._event_listeners[event].append(callback)
|
||||
|
||||
def off(self, callback: Callable):
|
||||
for event in self._event_listeners:
|
||||
if callback in self._event_listeners[event]:
|
||||
self._event_listeners[event].remove(callback)
|
||||
def off(self, event_or_callback: Union[str, Callable]):
|
||||
if isinstance(event_or_callback, str):
|
||||
event = event_or_callback.lower()
|
||||
if event in self._event_listeners:
|
||||
del self._event_listeners[event]
|
||||
else:
|
||||
for event in self._event_listeners:
|
||||
if event_or_callback in self._event_listeners[event]:
|
||||
self._event_listeners[event].remove(event_or_callback)
|
||||
|
||||
def _trigger(self, event: str, *args):
|
||||
event = event.lower()
|
||||
@@ -147,7 +154,7 @@ class Flix:
|
||||
|
||||
def _handle_mavlink_message(self, msg: mavlink.MAVLink_message):
|
||||
if isinstance(msg, mavlink.MAVLink_heartbeat_message):
|
||||
self.mode = ['MANUAL', 'ACRO', 'STAB', 'USER'][msg.custom_mode]
|
||||
self.mode = self._modes[msg.custom_mode] if msg.custom_mode < len(self._modes) else f'UNKNOWN({msg.custom_mode})'
|
||||
self.armed = msg.base_mode & mavlink.MAV_MODE_FLAG_SAFETY_ARMED != 0
|
||||
self._trigger('mode', self.mode)
|
||||
self._trigger('armed', self.armed)
|
||||
@@ -168,6 +175,11 @@ class Flix:
|
||||
msg.chan5_raw, msg.chan6_raw, msg.chan7_raw, msg.chan8_raw]
|
||||
self._trigger('channels', self.channels)
|
||||
|
||||
if isinstance(msg, mavlink.MAVLink_actuator_control_target_message):
|
||||
self.motors = msg.controls[:4] # type: ignore
|
||||
self._trigger('motors', self.motors)
|
||||
|
||||
# TODO: to be removed: the old way of passing motor outputs
|
||||
if isinstance(msg, mavlink.MAVLink_actuator_output_status_message):
|
||||
self.motors = msg.actuator[:4] # type: ignore
|
||||
self._trigger('motors', self.motors)
|
||||
@@ -231,6 +243,19 @@ class Flix:
|
||||
def _flu_to_mavlink(v: List[float]) -> List[float]:
|
||||
return Flix._mavlink_to_flu(v)
|
||||
|
||||
def _command_send(self, command: int, params: Sequence[float]):
|
||||
if len(params) != 7:
|
||||
raise ValueError('Command must have 7 parameters')
|
||||
for attempt in range(3):
|
||||
try:
|
||||
logger.debug(f'Send command {command} with params {params} (attempt #{attempt + 1})')
|
||||
self.mavlink.command_long_send(self.system_id, 0, command, 0, *params) # type: ignore
|
||||
self.wait('mavlink.COMMAND_ACK', value=lambda msg: msg.command == command and msg.result == mavlink.MAV_RESULT_ACCEPTED, timeout=0.1)
|
||||
return
|
||||
except TimeoutError:
|
||||
continue
|
||||
raise RuntimeError(f'Failed to send command {command} after 3 attempts')
|
||||
|
||||
def _connected(self):
|
||||
# Reset disconnection timer
|
||||
self._disconnected_timer.cancel()
|
||||
@@ -275,6 +300,14 @@ class Flix:
|
||||
continue
|
||||
raise RuntimeError(f'Failed to set parameter {name} to {value} after 3 attempts')
|
||||
|
||||
def set_mode(self, mode: Union[str, int]):
|
||||
if isinstance(mode, str):
|
||||
mode = self._modes.index(mode.upper())
|
||||
self._command_send(mavlink.MAV_CMD_DO_SET_MODE, (0, mode, 0, 0, 0, 0, 0))
|
||||
|
||||
def set_armed(self, armed: bool):
|
||||
self._command_send(mavlink.MAV_CMD_COMPONENT_ARM_DISARM, (1 if armed else 0, 0, 0, 0, 0, 0, 0))
|
||||
|
||||
def set_position(self, position: List[float], yaw: Optional[float] = None, wait: bool = False, tolerance: float = 0.1):
|
||||
raise NotImplementedError('Position control is not implemented yet')
|
||||
|
||||
@@ -282,17 +315,37 @@ class Flix:
|
||||
raise NotImplementedError('Velocity control is not implemented yet')
|
||||
|
||||
def set_attitude(self, attitude: List[float], thrust: float):
|
||||
raise NotImplementedError('Automatic flight is not implemented yet')
|
||||
if len(attitude) == 3:
|
||||
attitude = Quaternion([attitude[0], attitude[1], attitude[2]]).q # type: ignore
|
||||
elif len(attitude) != 4:
|
||||
raise ValueError('Attitude must be [roll, pitch, yaw] or [w, x, y, z] quaternion')
|
||||
if not (0 <= thrust <= 1):
|
||||
raise ValueError('Thrust must be in range [0, 1]')
|
||||
attitude = self._flu_to_mavlink(attitude)
|
||||
for _ in range(2): # duplicate to ensure delivery
|
||||
self.mavlink.set_attitude_target_send(0, self.system_id, 0, 0,
|
||||
[attitude[0], attitude[1], attitude[2], attitude[3]],
|
||||
0, 0, 0, thrust)
|
||||
|
||||
def set_rates(self, rates: List[float], thrust: float):
|
||||
raise NotImplementedError('Automatic flight is not implemented yet')
|
||||
if len(rates) != 3:
|
||||
raise ValueError('Rates must be [roll_rate, pitch_rate, yaw_rate]')
|
||||
if not (0 <= thrust <= 1):
|
||||
raise ValueError('Thrust must be in range [0, 1]')
|
||||
rates = self._flu_to_mavlink(rates)
|
||||
for _ in range(2): # duplicate to ensure delivery
|
||||
self.mavlink.set_attitude_target_send(0, self.system_id, 0,
|
||||
mavlink.ATTITUDE_TARGET_TYPEMASK_ATTITUDE_IGNORE,
|
||||
[1, 0, 0, 0],
|
||||
rates[0], rates[1], rates[2], thrust)
|
||||
|
||||
def set_motors(self, motors: List[float]):
|
||||
if len(motors) != 4:
|
||||
raise ValueError('motors must have 4 values')
|
||||
if not all(0 <= m <= 1 for m in motors):
|
||||
raise ValueError('motors must be in range [0, 1]')
|
||||
raise NotImplementedError
|
||||
for _ in range(2): # duplicate to ensure delivery
|
||||
self.mavlink.set_actuator_control_target_send(int(time.time() * 1000000), 0, self.system_id, 0, motors + [0] * 4) # type: ignore
|
||||
|
||||
def set_controls(self, roll: float, pitch: float, yaw: float, throttle: float):
|
||||
"""Send pilot's controls. Warning: not intended for automatic control"""
|
||||
@@ -300,10 +353,7 @@ class Flix:
|
||||
raise ValueError('roll, pitch, yaw must be in range [-1, 1]')
|
||||
if not 0 <= throttle <= 1:
|
||||
raise ValueError('throttle must be in range [0, 1]')
|
||||
self.mavlink.manual_control_send(self.system_id, roll * 1000, pitch * 1000, yaw * 1000, throttle * 1000, 0) # type: ignore
|
||||
|
||||
def set_mode(self, mode: Literal['MANUAL', 'ACRO', 'STAB', 'USER']):
|
||||
raise NotImplementedError('Setting mode is not implemented yet')
|
||||
self.mavlink.manual_control_send(self.system_id, int(pitch * 1000), int(roll * 1000), int(throttle * 1000), int(yaw * 1000), 0) # type: ignore
|
||||
|
||||
def cli(self, cmd: str, wait_response: bool = True) -> str:
|
||||
cmd = cmd.strip()
|
||||
@@ -320,7 +370,9 @@ class Flix:
|
||||
self.mavlink.serial_control_send(0, 0, 0, 0, len(cmd_bytes), cmd_bytes)
|
||||
if not wait_response:
|
||||
return ''
|
||||
response = self.wait('print_full', timeout=0.1, value=lambda text: text.startswith(response_prefix))
|
||||
timeout = 0.1
|
||||
if cmd == 'log': timeout = 10 # log download may take more time
|
||||
response = self.wait('print_full', timeout=timeout, value=lambda text: text.startswith(response_prefix))
|
||||
return response[len(response_prefix):].strip()
|
||||
except TimeoutError:
|
||||
continue
|
||||
|
||||
@@ -24,13 +24,16 @@ def main():
|
||||
if addr in TARGETS: # packet from target
|
||||
if source_addr is None:
|
||||
continue
|
||||
sock.sendto(data, source_addr)
|
||||
try:
|
||||
sock.sendto(data, source_addr)
|
||||
packets += 1
|
||||
except: pass
|
||||
else: # packet from source
|
||||
source_addr = addr
|
||||
for target in TARGETS:
|
||||
sock.sendto(data, target)
|
||||
packets += 1
|
||||
|
||||
packets += 1
|
||||
print(f'\rPackets: {packets}', end='')
|
||||
|
||||
if __name__ == '__main__':
|
||||
|
||||
@@ -1,6 +1,6 @@
|
||||
[project]
|
||||
name = "pyflix"
|
||||
version = "0.5"
|
||||
version = "0.9"
|
||||
description = "Python API for Flix drone"
|
||||
authors = [{ name="Oleg Kalachev", email="okalachev@gmail.com" }]
|
||||
license = "MIT"
|
||||
|
||||