2 Commits

Author SHA1 Message Date
Oleg Kalachev
0908674a60 Add level calibration 2025-12-26 11:29:12 +03:00
Oleg Kalachev
13a7e67b92 Add parameters for IMU orientation definition 2025-12-26 06:29:19 +03:00
30 changed files with 252 additions and 354 deletions

View File

@@ -25,6 +25,8 @@ jobs:
path: flix/build
- 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

View File

@@ -7,7 +7,6 @@
"MD024": false,
"MD033": false,
"MD034": false,
"MD040": false,
"MD059": false,
"MD044": {
"html_elements": false,

View File

@@ -6,18 +6,19 @@
"${workspaceFolder}/flix",
"${workspaceFolder}/gazebo",
"${workspaceFolder}/tools/**",
"~/.arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32",
"~/.arduino15/packages/esp32/hardware/esp32/3.3.6/libraries/**",
"~/.arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32",
"~/.arduino15/packages/esp32/tools/esp32-libs/3.3.6/include/**",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/**",
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
"~/Arduino/libraries/**",
"/usr/include/gazebo-11/",
"/usr/include/ignition/math6/"
],
"forcedInclude": [
"${workspaceFolder}/.vscode/intellisense.h",
"~/.arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32/Arduino.h",
"~/.arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32/pins_arduino.h",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
"${workspaceFolder}/flix/cli.ino",
"${workspaceFolder}/flix/control.ino",
"${workspaceFolder}/flix/estimate.ino",
@@ -30,10 +31,9 @@
"${workspaceFolder}/flix/rc.ino",
"${workspaceFolder}/flix/time.ino",
"${workspaceFolder}/flix/wifi.ino",
"${workspaceFolder}/flix/parameters.ino",
"${workspaceFolder}/flix/safety.ino"
"${workspaceFolder}/flix/parameters.ino"
],
"compilerPath": "~/.arduino15/packages/esp32/tools/esp-x32/2511/bin/xtensa-esp32-elf-g++",
"compilerPath": "~/.arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++",
"cStandard": "c11",
"cppStandard": "c++17",
"defines": [
@@ -53,18 +53,19 @@
"name": "Mac",
"includePath": [
"${workspaceFolder}/flix",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.6/libraries/**",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32",
"~/Library/Arduino15/packages/esp32/tools/esp32-libs/3.3.6/include/**",
"~/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/gazebo-11/",
"/opt/homebrew/include/ignition/math6/"
],
"forcedInclude": [
"${workspaceFolder}/.vscode/intellisense.h",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32/Arduino.h",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32/pins_arduino.h",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
"${workspaceFolder}/flix/flix.ino",
"${workspaceFolder}/flix/cli.ino",
"${workspaceFolder}/flix/control.ino",
@@ -77,10 +78,9 @@
"${workspaceFolder}/flix/rc.ino",
"${workspaceFolder}/flix/time.ino",
"${workspaceFolder}/flix/wifi.ino",
"${workspaceFolder}/flix/parameters.ino",
"${workspaceFolder}/flix/safety.ino"
"${workspaceFolder}/flix/parameters.ino"
],
"compilerPath": "~/Library/Arduino15/packages/esp32/tools/esp-x32/2511/bin/xtensa-esp32-elf-g++",
"compilerPath": "~/Library/Arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++",
"cStandard": "c11",
"cppStandard": "c++17",
"defines": [
@@ -103,16 +103,17 @@
"${workspaceFolder}/flix",
"${workspaceFolder}/gazebo",
"${workspaceFolder}/tools/**",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.6/libraries/**",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32",
"~/AppData/Local/Arduino15/packages/esp32/tools/esp32-libs/3.3.6/include/**",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
"~/AppData/Local/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/**",
"~/AppData/Local/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
"~/Documents/Arduino/libraries/**"
],
"forcedInclude": [
"${workspaceFolder}/.vscode/intellisense.h",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32/Arduino.h",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32/pins_arduino.h",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
"${workspaceFolder}/flix/cli.ino",
"${workspaceFolder}/flix/control.ino",
"${workspaceFolder}/flix/estimate.ino",
@@ -125,10 +126,9 @@
"${workspaceFolder}/flix/rc.ino",
"${workspaceFolder}/flix/time.ino",
"${workspaceFolder}/flix/wifi.ino",
"${workspaceFolder}/flix/parameters.ino",
"${workspaceFolder}/flix/safety.ino"
"${workspaceFolder}/flix/parameters.ino"
],
"compilerPath": "~/AppData/Local/Arduino15/packages/esp32/tools/esp-x32/2511/bin/xtensa-esp32-elf-g++.exe",
"compilerPath": "~/AppData/Local/Arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++.exe",
"cStandard": "c11",
"cppStandard": "c++17",
"defines": [

View File

@@ -13,10 +13,10 @@ monitor:
dependencies .dependencies:
arduino-cli core update-index --config-file arduino-cli.yaml
arduino-cli core install esp32:esp32@3.3.6 --config-file arduino-cli.yaml
arduino-cli core install esp32:esp32@3.2.0 --config-file arduino-cli.yaml
arduino-cli lib update-index
arduino-cli lib install "FlixPeriph"
arduino-cli lib install "MAVLink"@2.0.25
arduino-cli lib install "MAVLink"@2.0.16
touch .dependencies
gazebo/build cmake: gazebo/CMakeLists.txt

View File

@@ -1,9 +1,6 @@
<!-- markdownlint-disable MD041 -->
# Flix
<p align="center">
<img src="docs/img/flix.svg" width=180 alt="Flix logo"><br>
<b>Flix</b> (<i>flight + X</i>) — open source ESP32-based quadcopter made from scratch.
</p>
**Flix** (*flight + X*) — open source ESP32-based quadcopter made from scratch.
<table>
<tr>
@@ -21,13 +18,15 @@
* Dedicated for education and research.
* Made from general-purpose components.
* Simple and clean source code in Arduino (<2k lines firmware).
* Connectivity using Wi-Fi and MAVLink protocol.
* 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 for scripting and automatic flights.
* Python library.
* Textbook on flight control theory and practice ([in development](https://quadcopter.dev)).
* *Position control (planned)*.
* *Position control (using external camera) and autonomous flights¹*.
*¹ — planned.*
## It actually flies

View File

@@ -35,7 +35,7 @@
### Подсистема управления
Состояние органов управления обрабатывается в функции `interpretControls()` и преобразуется в **команду управления**, которая включает следующее:
Состояние органов управления обрабатывается в функции `interpretControls()` и преобразуется в *команду управления*, которая включает следующее:
* `attitudeTarget` *(Quaternion)* — целевая ориентация дрона.
* `ratesTarget` *(Vector)* — целевые угловые скорости, *рад/с*.

View File

@@ -87,13 +87,13 @@ Flix поддерживает следующие модели IMU:
#include <FlixPeriph.h>
#include <SPI.h>
MPU9250 imu(SPI);
MPU9250 IMU(SPI);
void setup() {
Serial.begin(115200);
bool success = imu.begin();
bool success = IMU.begin();
if (!success) {
Serial.println("Failed to initialize the IMU");
Serial.println("Failed to initialize IMU");
}
}
```
@@ -108,21 +108,21 @@ void setup() {
#include <FlixPeriph.h>
#include <SPI.h>
MPU9250 imu(SPI);
MPU9250 IMU(SPI);
void setup() {
Serial.begin(115200);
bool success = imu.begin();
bool success = IMU.begin();
if (!success) {
Serial.println("Failed to initialize the IMU");
Serial.println("Failed to initialize IMU");
}
}
void loop() {
imu.waitForData();
IMU.waitForData();
float gx, gy, gz;
imu.getGyro(gx, gy, gz);
IMU.getGyro(gx, gy, gz);
Serial.printf("gx:%f gy:%f gz:%f\n", gx, gy, gz);
delay(50); // замедление вывода
@@ -135,36 +135,36 @@ void loop() {
## Конфигурация гироскопа
В коде Flix настройка IMU происходит в функции `configureIMU`. В этой функции настраиваются три основных параметра гироскопа: диапазон измерений, частота сэмплирования и частота LPF-фильтра.
В коде Flix настройка IMU происходит в функции `configureIMU`. В этой функции настраиваются три основных параметра гироскопа: диапазон измерений, частота сэмплов и частота LPF-фильтра.
### Частота сэмплирования
### Частота сэмплов
Большинство IMU могут обновлять данные с разной частотой. В полетных контроллерах обычно используется частота обновления от 500 Гц до 8 кГц. Чем выше частота, тем выше точность управления полетом, но и тем больше нагрузка на микроконтроллер.
Большинство IMU могут обновлять данные с разной частотой. В полетных контроллерах обычно используется частота обновления от 500 Гц до 8 кГц. Чем выше частота сэмплов, тем выше точность управления полетом, но и больше нагрузка на микроконтроллер.
Частота сэмплирования устанавливается методом `setSampleRate()`. В Flix используется частота 1 кГц:
Частота сэмплов устанавливается методом `setSampleRate()`. В Flix используется частота 1 кГц:
```cpp
IMU.setRate(IMU.RATE_1KHZ_APPROX);
```
Поскольку не все поддерживаемые IMU могут работать строго на частоте 1 кГц, в библиотеке FlixPeriph существует возможность приближенной настройки частоты сэмплирования. Например, у IMU ICM-20948 при такой настройке реальная частота сэмплирования будет равна 1125 Гц.
Поскольку не все поддерживаемые IMU могут работать строго на частоте 1 кГц, в библиотеке FlixPeriph существует возможность приближенной настройки частоты сэмплов. Например, у IMU ICM-20948 при такой настройке реальная частота сэмплирования будет равна 1125 Гц.
Другие доступные для установки в библиотеке FlixPeriph частоты сэмплирования:
* `RATE_MIN` — минимальная частота для конкретного IMU.
* `RATE_MIN` — минимальная частота сэмплов для конкретного IMU.
* `RATE_50HZ_APPROX` — значение, близкое к 50 Гц.
* `RATE_1KHZ_APPROX` — значение, близкое к 1 кГц.
* `RATE_8KHZ_APPROX` — значение, близкое к 8 кГц.
* `RATE_MAX` — максимальная частота для конкретного IMU.
* `RATE_MAX` — максимальная частота сэмплов для конкретного IMU.
#### Диапазон измерений
Большинство MEMS-гироскопов поддерживают несколько диапазонов измерений угловой скорости. Главное преимущество выбора меньшего диапазона — бо́льшая чувствительность. В полетных контроллерах обычно выбирается максимальный диапазон измерений от 2000 до 2000 градусов в секунду, чтобы обеспечить возможность быстрых маневров.
Большинство MEMS-гироскопов поддерживают несколько диапазонов измерений угловой скорости. Главное преимущество выбора меньшего диапазона — бо́льшая чувствительность. В полетных контроллерах обычно выбирается максимальный диапазон измерений от 2000 до 2000 градусов в секунду, чтобы обеспечить возможность динамичных маневров.
В библиотеке FlixPeriph диапазон измерений гироскопа устанавливается методом `setGyroRange()`:
```cpp
imu.setGyroRange(imu.GYRO_RANGE_2000DPS);
IMU.setGyroRange(IMU.GYRO_RANGE_2000DPS);
```
### LPF-фильтр
@@ -172,7 +172,7 @@ imu.setGyroRange(imu.GYRO_RANGE_2000DPS);
IMU InvenSense могут фильтровать измерения на аппаратном уровне при помощи фильтра нижних частот (LPF). Flix реализует собственный фильтр для гироскопа, чтобы иметь больше гибкости при поддержке разных IMU. Поэтому для встроенного LPF устанавливается максимальная частота среза:
```cpp
imu.setDLPF(imu.DLPF_MAX);
IMU.setDLPF(IMU.DLPF_MAX);
```
## Калибровка гироскопа
@@ -181,7 +181,7 @@ imu.setDLPF(imu.DLPF_MAX);
\\[ gyro_{xyz}=rates_{xyz}+bias_{xyz}+noise \\]
Для точной работы подсистемы оценки ориентации и управления дроном необходимо оценить *bias* гироскопа и учесть его в вычислениях. Для этого при запуске программы производится калибровка гироскопа, которая реализована в функции `calibrateGyro()`. Эта функция считывает данные с гироскопа в состоянии покоя 1000 раз и усредняет их. Полученные значения считаются *bias* гироскопа и в дальнейшем вычитаются из измерений.
Для качественной работы подсистемы оценки ориентации и управления дроном необходимо оценить *bias* гироскопа и учесть его в вычислениях. Для этого при запуске программы производится калибровка гироскопа, которая реализована в функции `calibrateGyro()`. Эта функция считывает данные с гироскопа в состоянии покоя 1000 раз и усредняет их. Полученные значения считаются *bias* гироскопа и в дальнейшем вычитаются из измерений.
Программа для вывода данных с гироскопа с калибровкой:
@@ -189,23 +189,23 @@ imu.setDLPF(imu.DLPF_MAX);
#include <FlixPeriph.h>
#include <SPI.h>
MPU9250 imu(SPI);
MPU9250 IMU(SPI);
float gyroBiasX, gyroBiasY, gyroBiasZ; // bias гироскопа
void setup() {
Serial.begin(115200);
bool success = imu.begin();
bool success = IMU.begin();
if (!success) {
Serial.println("Failed to initialize the IMU");
Serial.println("Failed to initialize IMU");
}
calibrateGyro();
}
void loop() {
float gx, gy, gz;
imu.waitForData();
imu.getGyro(gx, gy, gz);
IMU.waitForData();
IMU.getGyro(gx, gy, gz);
// Устранение bias гироскопа
gx -= gyroBiasX;
@@ -226,9 +226,9 @@ void calibrateGyro() {
// Получение 1000 измерений гироскопа
for (int i = 0; i < samples; i++) {
imu.waitForData();
IMU.waitForData();
float gx, gy, gz;
imu.getGyro(gx, gy, gz);
IMU.getGyro(gx, gy, gz);
gyroBiasX += gx;
gyroBiasY += gy;
gyroBiasZ += gz;

View File

@@ -38,13 +38,13 @@ Utility files:
### Control subsystem
Pilot inputs are interpreted in `interpretControls()`, and then converted to the **control command**, which consists of the following:
Pilot inputs are interpreted in `interpretControls()`, and then converted to the *control command*, which consists of the following:
* `attitudeTarget` *(Quaternion)* — target attitude of the drone.
* `ratesTarget` *(Vector)* — target angular rates, *rad/s*.
* `ratesExtra` *(Vector)* — additional (feed-forward) angular rates, used for yaw rate control in STAB mode, *rad/s*.
* `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 motor thrust target, range [0, 1].
* `thrustTarget` *(float)* — collective thrust target, range [0, 1].
Control command is handled in `controlAttitude()`, `controlRates()`, `controlTorque()` functions. Each function may be skipped if the corresponding control target is set to `NAN`.
@@ -62,11 +62,6 @@ print("Test value: %.2f\n", testValue);
In order to add a console command, modify the `doCommand()` function in `cli.ino` file.
> [!IMPORTANT]
> Avoid using delays in in-flight commands, it will **crash** the drone! (The design is one-threaded.)
>
> For on-the-ground commands, use `pause()` function, instead of `delay()`. This function allows to pause in a way that MAVLink connection will continue working.
## Building the firmware
See build instructions in [usage.md](usage.md).

View File

@@ -1,38 +0,0 @@
<svg xmlns="http://www.w3.org/2000/svg" viewBox="0 0 734.86 378.46">
<defs>
<style>
.a {
fill: none;
stroke: #d5d5d5;
stroke-miterlimit: 10;
stroke-width: 31px;
}
.b {
fill: #c1c1c1;
}
.c {
fill: #ff9400;
}
.d {
fill: #d5d5d5;
}
</style>
</defs>
<g>
<g>
<line class="a" x1="448.78" y1="294.23" x2="648.77" y2="93.24"/>
<line class="a" x1="449.78" y1="94.24" x2="649.77" y2="295.23"/>
<circle class="b" cx="549.27" cy="193.73" r="41.5"/>
<circle class="c" cx="449.35" cy="93.74" r="77.95"/>
<circle class="c" cx="648.89" cy="93.53" r="77.95"/>
<circle class="c" cx="647.89" cy="294.51" r="77.95"/>
<circle class="c" cx="448.9" cy="294.51" r="77.95"/>
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Before

Width:  |  Height:  |  Size: 2.2 KiB

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@@ -4,7 +4,7 @@
Do the following:
* **Check ESP32 core is installed**. Check if the version matches the one used in the [tutorial](usage.md#building-the-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*.
@@ -16,7 +16,7 @@ Do the following:
* **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/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
* **Check if the console is working**. Perform `help` command in Serial Monitor. You should see the list of available commands. You can also access the console using QGroundControl (*Vehicle Setup* ⇒ *Analyze Tools**MAVLink Console*).
* **Check if the 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.
* **Check the IMU is working**. Perform `imu` command and check its output:
@@ -25,7 +25,7 @@ Do the following:
* The `accel` and `gyro` fields should change as you move the drone.
* **Calibrate the accelerometer.** if is wasn't done before. Type `ca` command in Serial Monitor and follow the instructions.
* **Check the attitude estimation**. Connect to the drone using QGroundControl. Rotate the drone in different orientations and check if the attitude estimation shown in QGroundControl is correct.
* **Check the IMU orientation is set correctly**. If the attitude estimation is rotated, set the correct IMU orientation as described in the [tutorial](usage.md#define-imu-orientation).
* **Check the IMU orientation is set correctly**. If the attitude estimation is rotated, make sure `rotateIMU` function is defined correctly in `imu.ino` file.
* **Check the motors type**. Motors with exact 3.7V voltage are needed, not ranged working voltage (3.7V — 6V).
* **Check the motors**. Perform the following commands using Serial Monitor:
* `mfr` — should rotate front right motor (counter-clockwise).

View File

@@ -20,10 +20,10 @@ You can build and upload the firmware using either **Arduino IDE** (easier for b
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 3.3.6. 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.
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 2.0.25.
* `MAVLink`, version 2.0.16.
5. Open the `flix/flix.ino` sketch from downloaded firmware sources in Arduino IDE.
6. 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.
7. [Build and upload](https://docs.arduino.cc/software/ide-v2/tutorials/getting-started/ide-v2-uploading-a-sketch) the firmware using Arduino IDE.
@@ -80,7 +80,7 @@ QGroundControl is a ground control station software that can be used to monitor
1. Install mobile or desktop version of [QGroundControl](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html).
2. Power up the drone.
3. Connect your computer or smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
4. Launch QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
4. Launch QGroundControl app. It should connect and begin showing the drone's telemetry automatically
### Access console
@@ -108,13 +108,11 @@ The drone is configured using parameters. To access and modify them, go to the Q
<img src="img/parameters.png" width="400">
You can also work with parameters using `p` command in the console. Parameter names are case-insensitive.
### Define IMU orientation
Use parameters, to define the IMU board axes orientation relative to the drone's axes: `IMU_ROT_ROLL`, `IMU_ROT_PITCH`, and `IMU_ROT_YAW`.
The drone has *X* axis pointing forward, *Y* axis pointing left, and *Z* axis pointing up, and the supported IMU boards have *X* axis pointing to the pins side and *Z* axis pointing up from the component side:
The drone has *X* axis pointing forward, *Y* axis pointing left, and *Z* axis pointing up, and the supported IMU boards have *X* axis pointing to the pins side and *Z* axis pointing up from the side with the components:
<img src="img/imu-axes.png" width="200">
@@ -122,10 +120,10 @@ Use the following table to set the parameters for common IMU orientations:
|Orientation|Parameters|Orientation|Parameters|
|:-:|-|-|-|
|<img src="img/imu-rot-1.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0 |<img src="img/imu-rot-5.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0|
|<img src="img/imu-rot-2.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|<img src="img/imu-rot-6.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|
|<img src="img/imu-rot-3.png" width="180">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|<img src="img/imu-rot-7.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|
|<img src="img/imu-rot-4.png" width="180"><br>☑️ **Default**|<br>`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|<img src="img/imu-rot-8.png" width="180">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|
|<img src="img/imu-rot-1.png" width="200">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0 |<img src="img/imu-rot-5.png" width="200">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 0|
|<img src="img/imu-rot-2.png" width="200">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|<img src="img/imu-rot-6.png" width="200">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|
|<img src="img/imu-rot-3.png" width="200">|`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|<img src="img/imu-rot-7.png" width="200">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 3.142|
|<img src="img/imu-rot-4.png" width="200"><br>☑️ **Default**|<br>`IMU_ROT_ROLL` = 0<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = -1.571|<img src="img/imu-rot-8.png" width="200">|`IMU_ROT_ROLL` = 3.142<br>`IMU_ROT_PITCH` = 0<br>`IMU_ROT_YAW` = 1.571|
### Calibrate accelerometer
@@ -143,9 +141,9 @@ Before flight you need to calibrate the accelerometer:
* The `accel` and `gyro` fields should change as you move the drone.
* The `landed` field should be `1` when the drone is still on the ground and `0` when you lift it up.
2. Check the attitude estimation: connect to the drone using QGroundControl, rotate the drone in different orientations and check if the attitude estimation shown in QGroundControl is correct. Compare your attitude indicator (in the *large vertical* mode) to the video:
2. Check the attitude estimation: connect to the drone using QGroundControl, rotate the drone in different orientations and check if the attitude estimation shown in QGroundControl is correct. Attitude indicator in QGroundControl is shown below:
<a href="https://youtu.be/yVRN23-GISU"><img width=300 src="https://i3.ytimg.com/vi/yVRN23-GISU/maxresdefault.jpg"></a>
<img src="img/qgc-attitude.png" height="200">
3. Perform motor tests in the console. Use the following commands **— remove the propellers before running the tests!**
@@ -154,10 +152,6 @@ Before flight you need to calibrate the accelerometer:
* `mrl` — should rotate rear left motor (counter-clockwise).
* `mrr` — should rotate rear right motor (clockwise).
Rotation diagram:
<img src="img/motors.svg" width=200>
> [!WARNING]
> Never run the motors when powering the drone from USB, always use the battery for that.
@@ -165,7 +159,7 @@ Before flight you need to calibrate the accelerometer:
There are several ways to control the drone's flight: using **smartphone** (Wi-Fi), using **SBUS remote control**, or using **USB remote control** (Wi-Fi).
### Control with a smartphone
### 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.
@@ -177,7 +171,7 @@ There are several ways to control the drone's flight: using **smartphone** (Wi-F
> [!TIP]
> Decrease `CTL_TILT_MAX` parameter when flying using the smartphone to make the controls less sensitive.
### Control with a remote control
### Control with remote control
Before using remote SBUS-connected remote control, you need to calibrate it:
@@ -185,7 +179,7 @@ Before using remote SBUS-connected remote control, you need to calibrate it:
2. Type `cr` command and follow the instructions.
3. Use the remote control to fly the drone!
### Control with a USB remote control
### 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.
@@ -243,43 +237,11 @@ In this mode, the pilot inputs are ignored (except the mode switch, if configure
If the pilot moves the control sticks, the drone will switch back to *STAB* mode.
## Wi-Fi configuration
You can configure the Wi-Fi using parameters and console commands.
The Wi-Fi mode is chosen using `WIFI_MODE` parameter in QGroundControl or in the console:
* `0` — Wi-Fi is disabled.
* `1` — Access Point mode (*AP*) — the drone creates a Wi-Fi network.
* `2` — Client mode (*STA*) — the drone connects to an existing Wi-Fi network.
* `3` — *ESP-NOW (not implemented yet)*.
> [!WARNING]
> Tests showed that Client mode may cause **additional delays** in remote control (due to retranslations), so it's generally not recommended.
The SSID and password are configured using the `ap` and `sta` console commands:
```
ap <ssid> <password>
sta <ssid> <password>
```
Example of configuring the Access Point mode:
```
ap my-flix-ssid mypassword123
p WIFI_MODE 1
```
Disabling Wi-Fi:
```
p WIFI_MODE 0
```
<img src="img/parameters.png" width="400">
## Flight log
After the flight, you can download the flight log for analysis wirelessly. Use the following command on your computer for that:
After the flight, you can download the flight log for analysis wirelessly. Use the following for that:
```bash
make log

View File

@@ -16,7 +16,7 @@ Author: [goldarte](https://t.me/goldarte).<br>
## School 548 course
Special course on quadcopter design and engineering took place in october-november 2025 in School 548, Moscow. The course included UAV control theory, electronics, drone assembly and setup practice, using the Flix project.
Special quadcopter design and engineering course took place in october-november 2025 in School 548, Moscow. Course included UAV control theory, electronics, and practical drone assembly and setup using the Flix project.
<img height=200 src="img/user/school548/1.jpg"> <img height=200 src="img/user/school548/2.jpg"> <img height=200 src="img/user/school548/3.jpg">
@@ -25,7 +25,7 @@ STL files and other materials: see [here](https://drive.google.com/drive/folders
### Selected works
Author: [KiraFlux](https://t.me/@kiraflux_0XC0000005).<br>
Description: **custom ESPNOW remote control** was implemented, modified firmware to support ESPNOW protocol.<br>
Description: **custom ESPNOW remote control** is implemented, firmware modified to support ESPNOW protocol.<br>
Telegram posts: [1](https://t.me/opensourcequadcopter/106), [2](https://t.me/opensourcequadcopter/114).<br>
Modified Flix firmware: https://github.com/KiraFlux/flix/tree/klyax.<br>
Remote control project: https://github.com/KiraFlux/ESP32-DJC.<br>

View File

@@ -6,16 +6,14 @@
#include "pid.h"
#include "vector.h"
#include "util.h"
#include "lpf.h"
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern const int RAW, ACRO, STAB, AUTO;
extern float t, dt, loopRate;
extern uint16_t channels[16];
extern float controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
extern int mode;
extern bool armed;
extern LowPassFilter<Vector> gyroBiasFilter;
const char* motd =
"\nWelcome to\n"
@@ -40,12 +38,11 @@ const char* motd =
"raw/stab/acro/auto - set mode\n"
"rc - show RC data\n"
"wifi - show Wi-Fi info\n"
"ap <ssid> <password> - setup Wi-Fi access point\n"
"sta <ssid> <password> - setup Wi-Fi client mode\n"
"mot - show motor output\n"
"log [dump] - print log header [and data]\n"
"cr - calibrate RC\n"
"ca - calibrate accel\n"
"cl - calibrate level\n"
"mfr, mfl, mrr, mrl - test motor (remove props)\n"
"sys - show system info\n"
"reset - reset drone's state\n"
@@ -58,7 +55,9 @@ void print(const char* format, ...) {
vsnprintf(buf, sizeof(buf), format, args);
va_end(args);
Serial.print(buf);
#if WIFI_ENABLED
mavlinkPrint(buf);
#endif
}
void pause(float duration) {
@@ -66,7 +65,9 @@ void pause(float duration) {
while (t - start < duration) {
step();
handleInput();
#if WIFI_ENABLED
processMavlink();
#endif
delay(50);
}
}
@@ -132,15 +133,12 @@ void doCommand(String str, bool echo = false) {
}
print("\nroll: %g pitch: %g yaw: %g throttle: %g mode: %g\n",
controlRoll, controlPitch, controlYaw, controlThrottle, controlMode);
print("time: %.1f\n", controlTime);
print("mode: %s\n", getModeName());
print("armed: %d\n", armed);
} else if (command == "wifi") {
#if WIFI_ENABLED
printWiFiInfo();
} else if (command == "ap") {
configWiFi(true, arg0.c_str(), arg1.c_str());
} else if (command == "sta") {
configWiFi(false, arg0.c_str(), arg1.c_str());
#endif
} 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]);
@@ -151,6 +149,8 @@ void doCommand(String str, bool echo = false) {
calibrateRC();
} else if (command == "ca") {
calibrateAccel();
} else if (command == "cl") {
calibrateLevel();
} else if (command == "mfr") {
testMotor(MOTOR_FRONT_RIGHT);
} else if (command == "mfl") {
@@ -180,7 +180,6 @@ void doCommand(String str, bool echo = false) {
#endif
} else if (command == "reset") {
attitude = Quaternion();
gyroBiasFilter.reset();
} else if (command == "reboot") {
ESP.restart();
} else {

View File

@@ -38,12 +38,6 @@ const int RAW = 0, ACRO = 1, STAB = 2, AUTO = 3; // flight modes
int mode = STAB;
bool armed = false;
Quaternion attitudeTarget;
Vector ratesTarget;
Vector ratesExtra; // feedforward rates
Vector torqueTarget;
float thrustTarget;
PID rollRatePID(ROLLRATE_P, ROLLRATE_I, ROLLRATE_D, ROLLRATE_I_LIM, RATES_D_LPF_ALPHA);
PID pitchRatePID(PITCHRATE_P, PITCHRATE_I, PITCHRATE_D, PITCHRATE_I_LIM, RATES_D_LPF_ALPHA);
PID yawRatePID(YAWRATE_P, YAWRATE_I, YAWRATE_D);
@@ -53,6 +47,12 @@ PID yawPID(YAW_P, 0, 0);
Vector maxRate(ROLLRATE_MAX, PITCHRATE_MAX, YAWRATE_MAX);
float tiltMax = TILT_MAX;
Quaternion attitudeTarget;
Vector ratesTarget;
Vector ratesExtra; // feedforward rates
Vector torqueTarget;
float thrustTarget;
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;

View File

@@ -8,10 +8,6 @@
#include "lpf.h"
#include "util.h"
Vector rates; // estimated angular rates, rad/s
Quaternion attitude; // estimated attitude
bool landed;
float accWeight = 0.003;
LowPassFilter<Vector> ratesFilter(0.2); // cutoff frequency ~ 40 Hz

View File

@@ -7,13 +7,18 @@
#include "quaternion.h"
#include "util.h"
extern float t, dt;
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
extern Vector gyro, acc;
extern Vector rates;
extern Quaternion attitude;
extern bool landed;
extern float motors[4];
#define WIFI_ENABLED 1
float t = NAN; // current step time, s
float dt; // time delta from previous step, s
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
float controlMode = NAN;
Vector gyro; // gyroscope data
Vector acc; // accelerometer data, m/s/s
Vector rates; // filtered angular rates, rad/s
Quaternion attitude; // estimated attitude
bool landed; // are we landed and stationary
float motors[4]; // normalized motors thrust in range [0..1]
void setup() {
Serial.begin(115200);
@@ -23,7 +28,9 @@ void setup() {
setupLED();
setupMotors();
setLED(true);
#if WIFI_ENABLED
setupWiFi();
#endif
setupIMU();
setupRC();
setLED(false);
@@ -38,7 +45,9 @@ void loop() {
control();
sendMotors();
handleInput();
#if WIFI_ENABLED
processMavlink();
#endif
logData();
syncParameters();
}

View File

@@ -12,14 +12,9 @@
MPU9250 imu(SPI);
Vector imuRotation(0, 0, -PI / 2); // imu orientation as Euler angles
Vector gyro; // gyroscope output, rad/s
Vector gyroBias;
Vector acc; // accelerometer output, m/s/s
Vector accBias;
Vector accScale(1, 1, 1);
LowPassFilter<Vector> gyroBiasFilter(0.001);
Vector gyroBias;
void setupIMU() {
print("Setup IMU\n");
@@ -52,6 +47,8 @@ void readIMU() {
void calibrateGyroOnce() {
static Delay landedDelay(2);
if (!landedDelay.update(landed)) return; // calibrate only if definitely stationary
static LowPassFilter<Vector> gyroBiasFilter(0.001);
gyroBias = gyroBiasFilter.update(gyro);
}
@@ -110,6 +107,14 @@ void calibrateAccelOnce() {
accBias = (accMax + accMin) / 2;
}
void calibrateLevel() {
print("Place perfectly level [1 sec]\n");
pause(1);
Quaternion correction = Quaternion::fromBetweenVectors(Quaternion::rotateVector(Vector(0, 0, 1), attitude), Vector(0, 0, 1));
imuRotation = Quaternion::rotate(correction, Quaternion::fromEuler(imuRotation)).toEuler();
print("✓ Done: %.3f %.3f %.3f\n", degrees(imuRotation.x), degrees(imuRotation.y), degrees(imuRotation.z));
}
void printIMUCalibration() {
print("gyro bias: %f %f %f\n", gyroBias.x, gyroBias.y, gyroBias.z);
print("accel bias: %f %f %f\n", accBias.x, accBias.y, accBias.z);

View File

@@ -14,6 +14,15 @@ public:
LowPassFilter(float alpha): alpha(alpha) {};
T update(const T input) {
if (alpha == 1) { // filter disabled
return input;
}
if (!initialized) {
output = input;
initialized = true;
}
return output += alpha * (input - output);
}
@@ -22,6 +31,9 @@ public:
}
void reset() {
output = T(); // set to zero
initialized = false;
}
private:
bool initialized = false;
};

View File

@@ -3,16 +3,20 @@
// MAVLink communication
#if WIFI_ENABLED
#include <MAVLink.h>
#include "util.h"
extern float controlTime;
#define SYSTEM_ID 1
#define MAVLINK_RATE_SLOW 1
#define MAVLINK_RATE_FAST 10
bool mavlinkConnected = false;
String mavlinkPrintBuffer;
int mavlinkSysId = 1;
Rate telemetryFast(10);
Rate telemetrySlow(2);
extern float controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
void processMavlink() {
sendMavlink();
@@ -25,8 +29,10 @@ void sendMavlink() {
mavlink_message_t msg;
uint32_t time = t * 1000;
if (telemetrySlow) {
mavlink_msg_heartbeat_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, MAV_TYPE_QUADROTOR, MAV_AUTOPILOT_GENERIC,
static Rate slow(MAVLINK_RATE_SLOW), fast(MAVLINK_RATE_FAST);
if (slow) {
mavlink_msg_heartbeat_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, MAV_TYPE_QUADROTOR, MAV_AUTOPILOT_GENERIC,
(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),
@@ -35,27 +41,27 @@ void sendMavlink() {
if (!mavlinkConnected) return; // send only heartbeat until connected
mavlink_msg_extended_sys_state_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
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 (telemetryFast && mavlinkConnected) {
if (fast && mavlinkConnected) {
const float zeroQuat[] = {0, 0, 0, 0};
mavlink_msg_attitude_quaternion_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
mavlink_msg_attitude_quaternion_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
time, attitude.w, attitude.x, -attitude.y, -attitude.z, rates.x, -rates.y, -rates.z, zeroQuat); // convert to frd
sendMessage(&msg);
mavlink_msg_rc_channels_raw_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, controlTime * 1000, 0,
mavlink_msg_rc_channels_raw_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, controlTime * 1000, 0,
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 controls[8];
memcpy(controls, motors, sizeof(motors));
mavlink_msg_actuator_control_target_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, time, 0, controls);
mavlink_msg_actuator_control_target_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time, 0, controls);
sendMessage(&msg);
mavlink_msg_scaled_imu_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, time,
mavlink_msg_scaled_imu_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time,
acc.x * 1000, -acc.y * 1000, -acc.z * 1000, // convert to frd
gyro.x * 1000, -gyro.y * 1000, -gyro.z * 1000,
0, 0, 0, 0);
@@ -90,7 +96,7 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_MANUAL_CONTROL) {
mavlink_manual_control_t m;
mavlink_msg_manual_control_decode(&msg, &m);
if (m.target && m.target != mavlinkSysId) return; // 0 is broadcast
if (m.target && m.target != SYSTEM_ID) return; // 0 is broadcast
controlThrottle = m.z / 1000.0f;
controlPitch = m.x / 1000.0f;
@@ -103,11 +109,11 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_PARAM_REQUEST_LIST) {
mavlink_param_request_list_t m;
mavlink_msg_param_request_list_decode(&msg, &m);
if (m.target_system && m.target_system != mavlinkSysId) return;
if (m.target_system && m.target_system != SYSTEM_ID) return;
mavlink_message_t msg;
for (int i = 0; i < parametersCount(); i++) {
mavlink_msg_param_value_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
mavlink_msg_param_value_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
getParameterName(i), getParameter(i), MAV_PARAM_TYPE_REAL32, parametersCount(), i);
sendMessage(&msg);
}
@@ -116,7 +122,7 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_PARAM_REQUEST_READ) {
mavlink_param_request_read_t m;
mavlink_msg_param_request_read_decode(&msg, &m);
if (m.target_system && m.target_system != mavlinkSysId) return;
if (m.target_system && m.target_system != SYSTEM_ID) return;
char name[MAVLINK_MSG_PARAM_REQUEST_READ_FIELD_PARAM_ID_LEN + 1];
strlcpy(name, m.param_id, sizeof(name)); // param_id might be not null-terminated
@@ -125,7 +131,7 @@ void handleMavlink(const void *_msg) {
memcpy(name, getParameterName(m.param_index), 16);
}
mavlink_message_t msg;
mavlink_msg_param_value_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
mavlink_msg_param_value_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
name, value, MAV_PARAM_TYPE_REAL32, parametersCount(), m.param_index);
sendMessage(&msg);
}
@@ -133,33 +139,32 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_PARAM_SET) {
mavlink_param_set_t m;
mavlink_msg_param_set_decode(&msg, &m);
if (m.target_system && m.target_system != mavlinkSysId) return;
if (m.target_system && m.target_system != SYSTEM_ID) return;
char name[MAVLINK_MSG_PARAM_SET_FIELD_PARAM_ID_LEN + 1];
strlcpy(name, m.param_id, sizeof(name)); // param_id might be not null-terminated
bool success = setParameter(name, m.param_value);
if (!success) return;
setParameter(name, m.param_value);
// send ack
mavlink_message_t msg;
mavlink_msg_param_value_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
m.param_id, getParameter(name), MAV_PARAM_TYPE_REAL32, parametersCount(), 0); // index is unknown
mavlink_msg_param_value_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
m.param_id, m.param_value, MAV_PARAM_TYPE_REAL32, parametersCount(), 0); // index is unknown
sendMessage(&msg);
}
if (msg.msgid == MAVLINK_MSG_ID_MISSION_REQUEST_LIST) { // handle to make qgc happy
mavlink_mission_request_list_t m;
mavlink_msg_mission_request_list_decode(&msg, &m);
if (m.target_system && m.target_system != mavlinkSysId) return;
if (m.target_system && m.target_system != SYSTEM_ID) return;
mavlink_message_t msg;
mavlink_msg_mission_count_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, 0, 0, 0, MAV_MISSION_TYPE_MISSION, 0);
mavlink_msg_mission_count_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, 0, 0, 0, MAV_MISSION_TYPE_MISSION, 0);
sendMessage(&msg);
}
if (msg.msgid == MAVLINK_MSG_ID_SERIAL_CONTROL) {
mavlink_serial_control_t m;
mavlink_msg_serial_control_decode(&msg, &m);
if (m.target_system && m.target_system != mavlinkSysId) return;
if (m.target_system && m.target_system != SYSTEM_ID) return;
char data[MAVLINK_MSG_SERIAL_CONTROL_FIELD_DATA_LEN + 1];
strlcpy(data, (const char *)m.data, m.count); // data might be not null-terminated
@@ -171,7 +176,7 @@ void handleMavlink(const void *_msg) {
mavlink_set_attitude_target_t m;
mavlink_msg_set_attitude_target_decode(&msg, &m);
if (m.target_system && m.target_system != mavlinkSysId) return;
if (m.target_system && m.target_system != SYSTEM_ID) return;
// copy attitude, rates and thrust targets
ratesTarget.x = m.body_roll_rate;
@@ -193,7 +198,7 @@ void handleMavlink(const void *_msg) {
mavlink_set_actuator_control_target_t m;
mavlink_msg_set_actuator_control_target_decode(&msg, &m);
if (m.target_system && m.target_system != mavlinkSysId) return;
if (m.target_system && m.target_system != SYSTEM_ID) return;
attitudeTarget.invalidate();
ratesTarget.invalidate();
@@ -205,12 +210,12 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_LOG_REQUEST_DATA) {
mavlink_log_request_data_t m;
mavlink_msg_log_request_data_decode(&msg, &m);
if (m.target_system && m.target_system != mavlinkSysId) return;
if (m.target_system && m.target_system != SYSTEM_ID) return;
// Send all log records
for (int i = 0; i < sizeof(logBuffer) / sizeof(logBuffer[0]); i++) {
mavlink_message_t msg;
mavlink_msg_log_data_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, 0, i,
mavlink_msg_log_data_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, 0, i,
sizeof(logBuffer[0]), (uint8_t *)logBuffer[i]);
sendMessage(&msg);
}
@@ -220,13 +225,13 @@ void handleMavlink(const void *_msg) {
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 != mavlinkSysId) return;
if (m.target_system && m.target_system != SYSTEM_ID) return;
mavlink_message_t response;
bool accepted = false;
if (m.command == MAV_CMD_REQUEST_MESSAGE && m.param1 == MAVLINK_MSG_ID_AUTOPILOT_VERSION) {
accepted = true;
mavlink_msg_autopilot_version_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &response,
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);
}
@@ -245,7 +250,7 @@ void handleMavlink(const void *_msg) {
// send command ack
mavlink_message_t ack;
mavlink_msg_command_ack_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &ack, m.command, accepted ? MAV_RESULT_ACCEPTED : MAV_RESULT_UNSUPPORTED, UINT8_MAX, 0, msg.sysid, msg.compid);
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);
}
}
@@ -262,7 +267,7 @@ void sendMavlinkPrint() {
char data[MAVLINK_MSG_SERIAL_CONTROL_FIELD_DATA_LEN + 1];
strlcpy(data, str + i, sizeof(data));
mavlink_message_t msg;
mavlink_msg_serial_control_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
mavlink_msg_serial_control_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
SERIAL_CONTROL_DEV_SHELL,
i + MAVLINK_MSG_SERIAL_CONTROL_FIELD_DATA_LEN < strlen(str) ? SERIAL_CONTROL_FLAG_MULTI : 0, // more chunks to go
0, 0, strlen(data), (uint8_t *)data, 0, 0);
@@ -270,3 +275,5 @@ void sendMavlinkPrint() {
}
mavlinkPrintBuffer.clear();
}
#endif

View File

@@ -17,8 +17,7 @@
#define PWM_MIN 0
#define PWM_MAX 1000000 / PWM_FREQUENCY
float motors[4]; // normalized motor thrusts in range [0..1]
// Motors array indexes:
const int MOTOR_REAR_LEFT = 0;
const int MOTOR_REAR_RIGHT = 1;
const int MOTOR_FRONT_RIGHT = 2;

View File

@@ -9,20 +9,13 @@
extern float channelZero[16];
extern float channelMax[16];
extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
extern int wifiMode, udpLocalPort, udpRemotePort;
extern float rcLossTimeout, descendTime;
Preferences storage;
struct Parameter {
const char *name; // max length is 15 (Preferences key limit)
bool integer;
union { float *f; int *i; }; // pointer to variable
float cache; // what's stored in flash
Parameter(const char *name, float *variable) : name(name), integer(false), f(variable) {};
Parameter(const char *name, int *variable) : name(name), integer(true), i(variable) {};
float getValue() const { return integer ? *i : *f; };
void setValue(const float value) { if (integer) *i = value; else *f = value; };
float *variable;
float value; // cache
};
Parameter parameters[] = {
@@ -59,7 +52,6 @@ Parameter parameters[] = {
{"IMU_ACC_SCALE_X", &accScale.x},
{"IMU_ACC_SCALE_Y", &accScale.y},
{"IMU_ACC_SCALE_Z", &accScale.z},
{"IMU_GYRO_BIAS_A", &gyroBiasFilter.alpha},
// estimate
{"EST_ACC_WEIGHT", &accWeight},
{"EST_RATES_LPF_A", &ratesFilter.alpha},
@@ -85,17 +77,6 @@ Parameter parameters[] = {
{"RC_THROTTLE", &throttleChannel},
{"RC_YAW", &yawChannel},
{"RC_MODE", &modeChannel},
// wifi
{"WIFI_MODE", &wifiMode},
{"WIFI_LOC_PORT", &udpLocalPort},
{"WIFI_REM_PORT", &udpRemotePort},
// mavlink
{"MAV_SYS_ID", &mavlinkSysId},
{"MAV_RATE_SLOW", &telemetrySlow.rate},
{"MAV_RATE_FAST", &telemetryFast.rate},
// safety
{"SF_RC_LOSS_TIME", &rcLossTimeout},
{"SF_DESCEND_TIME", &descendTime},
};
void setupParameters() {
@@ -103,10 +84,10 @@ void setupParameters() {
// Read parameters from storage
for (auto &parameter : parameters) {
if (!storage.isKey(parameter.name)) {
storage.putFloat(parameter.name, parameter.getValue()); // store default value
storage.putFloat(parameter.name, *parameter.variable);
}
parameter.setValue(storage.getFloat(parameter.name, 0));
parameter.cache = parameter.getValue();
*parameter.variable = storage.getFloat(parameter.name, *parameter.variable);
parameter.value = *parameter.variable;
}
}
@@ -121,13 +102,13 @@ const char *getParameterName(int index) {
float getParameter(int index) {
if (index < 0 || index >= parametersCount()) return NAN;
return parameters[index].getValue();
return *parameters[index].variable;
}
float getParameter(const char *name) {
for (auto &parameter : parameters) {
if (strcasecmp(parameter.name, name) == 0) {
return parameter.getValue();
if (strcmp(parameter.name, name) == 0) {
return *parameter.variable;
}
}
return NAN;
@@ -135,9 +116,8 @@ float getParameter(const char *name) {
bool setParameter(const char *name, const float value) {
for (auto &parameter : parameters) {
if (strcasecmp(parameter.name, name) == 0) {
if (parameter.integer && !isfinite(value)) return false; // can't set integer to NaN or Inf
parameter.setValue(value);
if (strcmp(parameter.name, name) == 0) {
*parameter.variable = value;
return true;
}
}
@@ -150,18 +130,16 @@ void syncParameters() {
if (motorsActive()) return; // don't use flash while flying, it may cause a delay
for (auto &parameter : parameters) {
if (parameter.getValue() == parameter.cache) continue; // no change
if (isnan(parameter.getValue()) && isnan(parameter.cache)) continue; // both are NaN
if (isinf(parameter.getValue()) && isinf(parameter.cache)) continue; // both are Inf
storage.putFloat(parameter.name, parameter.getValue());
parameter.cache = parameter.getValue(); // update cache
if (parameter.value == *parameter.variable) continue;
if (isnan(parameter.value) && isnan(*parameter.variable)) continue; // handle NAN != NAN
storage.putFloat(parameter.name, *parameter.variable);
parameter.value = *parameter.variable;
}
}
void printParameters() {
for (auto &parameter : parameters) {
print("%s = %g\n", parameter.name, parameter.getValue());
print("%s = %g\n", parameter.name, *parameter.variable);
}
}

View File

@@ -6,17 +6,14 @@
#include <SBUS.h>
#include "util.h"
SBUS rc(Serial2);
SBUS rc(Serial2); // NOTE: Use RC(Serial2, 16, 17) if you use the old UART2 pins
uint16_t channels[16]; // raw rc channels
float controlTime; // time of the last controls update
float channelZero[16]; // calibration zero values
float channelMax[16]; // calibration max values
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
float controlMode = NAN;
float controlTime = NAN; // time of the last controls update
// Channels mapping (nan means not assigned):
// Channels mapping (using float to store in parameters):
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
void setupRC() {
@@ -41,11 +38,11 @@ void normalizeRC() {
controls[i] = mapf(channels[i], channelZero[i], channelMax[i], 0, 1);
}
// Update control values
controlRoll = rollChannel >= 0 ? controls[(int)rollChannel] : 0;
controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : 0;
controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : 0;
controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : 0;
controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN; // mode switch should not have affect if not set
controlRoll = rollChannel >= 0 ? controls[(int)rollChannel] : NAN;
controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : NAN;
controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : NAN;
controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : NAN;
controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN;
}
void calibrateRC() {

View File

@@ -3,12 +3,12 @@
// Fail-safe functions
#define RC_LOSS_TIMEOUT 1
#define DESCEND_TIME 10
extern float controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw;
float rcLossTimeout = 1;
float descendTime = 10;
void failsafe() {
rcLossFailsafe();
autoFailsafe();
@@ -16,8 +16,9 @@ void failsafe() {
// RC loss failsafe
void rcLossFailsafe() {
if (controlTime == 0) return; // no RC at all
if (!armed) return;
if (t - controlTime > rcLossTimeout) {
if (t - controlTime > RC_LOSS_TIMEOUT) {
descend();
}
}
@@ -26,7 +27,7 @@ void rcLossFailsafe() {
void descend() {
mode = AUTO;
attitudeTarget = Quaternion();
thrustTarget -= dt / descendTime;
thrustTarget -= dt / DESCEND_TIME;
if (thrustTarget < 0) {
thrustTarget = 0;
armed = false;

View File

@@ -3,8 +3,6 @@
// Time related functions
float t = NAN; // current time, s
float dt; // time delta with the previous step, s
float loopRate; // Hz
void step() {

View File

@@ -35,6 +35,7 @@ public:
z = NAN;
}
float norm() const {
return sqrt(x * x + y * y + z * z);
}

View File

@@ -1,76 +1,49 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Wi-Fi communication
// Wi-Fi support
#if WIFI_ENABLED
#include <WiFi.h>
#include <WiFiAP.h>
#include <WiFiUdp.h>
#include "Preferences.h"
extern Preferences storage; // use the main preferences storage
const int W_DISABLED = 0, W_AP = 1, W_STA = 2;
int wifiMode = W_AP;
int udpLocalPort = 14550;
int udpRemotePort = 14550;
IPAddress udpRemoteIP = "255.255.255.255";
#define WIFI_SSID "flix"
#define WIFI_PASSWORD "flixwifi"
#define WIFI_UDP_PORT 14550
#define WIFI_UDP_REMOTE_PORT 14550
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
WiFiUDP udp;
void setupWiFi() {
print("Setup Wi-Fi\n");
if (wifiMode == W_AP) {
WiFi.softAP(storage.getString("WIFI_AP_SSID", "flix").c_str(), storage.getString("WIFI_AP_PASS", "flixwifi").c_str());
} else if (wifiMode == W_STA) {
WiFi.begin(storage.getString("WIFI_STA_SSID", "").c_str(), storage.getString("WIFI_STA_PASS", "").c_str());
}
udp.begin(udpLocalPort);
WiFi.softAP(WIFI_SSID, WIFI_PASSWORD);
udp.begin(WIFI_UDP_PORT);
}
void sendWiFi(const uint8_t *buf, int len) {
if (WiFi.softAPgetStationNum() == 0 && !WiFi.isConnected()) return;
udp.beginPacket(udpRemoteIP, udpRemotePort);
if (WiFi.softAPIP() == IPAddress(0, 0, 0, 0) && WiFi.status() != WL_CONNECTED) return;
udp.beginPacket(udp.remoteIP() ? udp.remoteIP() : WIFI_UDP_REMOTE_ADDR, WIFI_UDP_REMOTE_PORT);
udp.write(buf, len);
udp.endPacket();
}
int receiveWiFi(uint8_t *buf, int len) {
udp.parsePacket();
if (udp.remoteIP()) udpRemoteIP = udp.remoteIP();
return udp.read(buf, len);
}
void printWiFiInfo() {
if (WiFi.getMode() == WIFI_MODE_AP) {
print("Mode: Access Point (AP)\n");
print("MAC: %s\n", WiFi.softAPmacAddress().c_str());
print("SSID: %s\n", WiFi.softAPSSID().c_str());
print("Password: ***\n");
print("Clients: %d\n", WiFi.softAPgetStationNum());
print("IP: %s\n", WiFi.softAPIP().toString().c_str());
} else if (WiFi.getMode() == WIFI_MODE_STA) {
print("Mode: Client (STA)\n");
print("Connected: %d\n", WiFi.isConnected());
print("MAC: %s\n", WiFi.macAddress().c_str());
print("SSID: %s\n", WiFi.SSID().c_str());
print("Password: ***\n");
print("IP: %s\n", WiFi.localIP().toString().c_str());
} else {
print("Mode: Disabled\n");
return;
}
print("Remote IP: %s\n", udpRemoteIP.toString().c_str());
print("MAC: %s\n", WiFi.softAPmacAddress().c_str());
print("SSID: %s\n", WiFi.softAPSSID().c_str());
print("Password: %s\n", WIFI_PASSWORD);
print("Clients: %d\n", WiFi.softAPgetStationNum());
print("Status: %d\n", WiFi.status());
print("IP: %s\n", WiFi.softAPIP().toString().c_str());
print("Remote IP: %s\n", udp.remoteIP().toString().c_str());
print("MAVLink connected: %d\n", mavlinkConnected);
}
void configWiFi(bool ap, const char *ssid, const char *password) {
if (ap) {
storage.putString("WIFI_AP_SSID", ssid);
storage.putString("WIFI_AP_PASS", password);
} else {
storage.putString("WIFI_STA_SSID", ssid);
storage.putString("WIFI_STA_PASS", password);
}
print("✓ Reboot to apply new settings\n");
}
#endif

View File

@@ -10,15 +10,19 @@
#include "Arduino.h"
#include "wifi.h"
extern float t, dt;
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
extern Vector rates;
extern Quaternion attitude;
extern bool landed;
extern float motors[4];
#define WIFI_ENABLED 1
Vector gyro, acc, imuRotation;
Vector accBias, gyroBias, accScale(1, 1, 1);
float t = NAN;
float dt;
float motors[4];
float controlRoll, controlPitch, controlYaw, controlThrottle = NAN;
float controlMode = NAN;
Vector acc;
Vector gyro;
Vector rates;
Quaternion attitude;
bool landed;
Vector imuRotation;
// declarations
void step();
@@ -68,7 +72,8 @@ void resetParameters();
void setLED(bool on) {};
void calibrateGyro() { print("Skip gyro calibrating\n"); };
void calibrateAccel() { print("Skip accel calibrating\n"); };
void calibrateLevel() { print("Skip level calibrating\n"); };
void printIMUCalibration() { print("cal: N/A\n"); };
void printIMUInfo() {};
void printWiFiInfo() {};
void configWiFi(bool, const char*, const char*) { print("Skip WiFi config\n"); };
Vector accBias, gyroBias, accScale(1, 1, 1);

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@@ -13,7 +13,7 @@ lines = []
print('Downloading log...')
count = 0
dev.write('log dump\n'.encode())
dev.write('log\n'.encode())
while True:
line = dev.readline()
if not line:

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@@ -43,7 +43,6 @@ records = [record for record in records if record[0] != 0]
print(f'Received records: {len(records)}')
os.makedirs(f'{DIR}/log', exist_ok=True)
log = open(f'{DIR}/log/{datetime.datetime.now().isoformat()}.csv', 'wb')
log.write(header.encode() + b'\n')
for record in records:

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@@ -95,7 +95,7 @@ Full list of events:
|`armed`|Armed state update|Armed state (*bool*)|
|`mode`|Flight mode update|Flight mode (*str*)|
|`landed`|Landed state update|Landed state (*bool*)|
|`print`|The drone prints text to the console|Text|
|`print`|The drone sends text to the console|Text|
|`attitude`|Attitude update|Attitude quaternion (*list*)|
|`attitude_euler`|Attitude update|Euler angles (*list*)|
|`rates`|Angular rates update|Angular rates (*list*)|
@@ -112,7 +112,7 @@ Full list of events:
> [!NOTE]
> Update events trigger on every new piece of data from the drone, and do not mean the value has changed.
### Basic methods
### Common methods
Get and set firmware parameters using `get_param` and `set_param` methods: