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
28 changed files with 233 additions and 350 deletions

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@@ -25,8 +25,8 @@ jobs:
path: flix/build path: flix/build
- name: Build firmware for ESP32-S3 - name: Build firmware for ESP32-S3
run: make BOARD=esp32:esp32:esp32s3 run: make BOARD=esp32:esp32:esp32s3
- name: Build firmware for ESP32-C3 - name: Build firmware with WiFi disabled
run: make BOARD=esp32:esp32:esp32c3 run: sed -i 's/^#define WIFI_ENABLED 1$/#define WIFI_ENABLED 0/' flix/flix.ino && make
- name: Check c_cpp_properties.json - name: Check c_cpp_properties.json
run: tools/check_c_cpp_properties.py run: tools/check_c_cpp_properties.py

View File

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

View File

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

View File

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

View File

@@ -1,9 +1,6 @@
<!-- markdownlint-disable MD041 --> # Flix
<p align="center"> **Flix** (*flight + X*) — open source ESP32-based quadcopter made from scratch.
<img src="docs/img/flix.svg" width=180 alt="Flix logo"><br>
<b>Flix</b> (<i>flight + X</i>) — open source ESP32-based quadcopter made from scratch.
</p>
<table> <table>
<tr> <tr>
@@ -21,13 +18,15 @@
* Dedicated for education and research. * Dedicated for education and research.
* Made from general-purpose components. * Made from general-purpose components.
* Simple and clean source code in Arduino (<2k lines firmware). * 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. * Control using USB gamepad, remote control or smartphone.
* Wi-Fi and MAVLink support.
* Wireless command line interface and analyzing. * Wireless command line interface and analyzing.
* Precise simulation with Gazebo. * 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)). * 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 ## It actually flies

View File

@@ -35,7 +35,7 @@
### Подсистема управления ### 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. * `attitudeTarget` *(Quaternion)* — целевая ориентация дрона.
* `ratesTarget` *(Vector)* — целевые угловые скорости, *рад/с*. * `ratesTarget` *(Vector)* — целевые угловые скорости, *рад/с*.

View File

@@ -87,13 +87,13 @@ Flix поддерживает следующие модели IMU:
#include <FlixPeriph.h> #include <FlixPeriph.h>
#include <SPI.h> #include <SPI.h>
MPU9250 imu(SPI); MPU9250 IMU(SPI);
void setup() { void setup() {
Serial.begin(115200); Serial.begin(115200);
bool success = imu.begin(); bool success = IMU.begin();
if (!success) { 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 <FlixPeriph.h>
#include <SPI.h> #include <SPI.h>
MPU9250 imu(SPI); MPU9250 IMU(SPI);
void setup() { void setup() {
Serial.begin(115200); Serial.begin(115200);
bool success = imu.begin(); bool success = IMU.begin();
if (!success) { if (!success) {
Serial.println("Failed to initialize the IMU"); Serial.println("Failed to initialize IMU");
} }
} }
void loop() { void loop() {
imu.waitForData(); IMU.waitForData();
float gx, gy, gz; 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); Serial.printf("gx:%f gy:%f gz:%f\n", gx, gy, gz);
delay(50); // замедление вывода delay(50); // замедление вывода
@@ -135,36 +135,36 @@ void loop() {
## Конфигурация гироскопа ## 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 ```cpp
IMU.setRate(IMU.RATE_1KHZ_APPROX); 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: 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_50HZ_APPROX` — значение, близкое к 50 Гц.
* `RATE_1KHZ_APPROX` — значение, близкое к 1 кГц. * `RATE_1KHZ_APPROX` — значение, близкое к 1 кГц.
* `RATE_8KHZ_APPROX` — значение, близкое к 8 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 #### 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()`: В библиотеке FlixPeriph диапазон измерений гироскопа устанавливается методом `setGyroRange()`:
```cpp ```cpp
imu.setGyroRange(imu.GYRO_RANGE_2000DPS); IMU.setGyroRange(IMU.GYRO_RANGE_2000DPS);
``` ```
### LPF-фильтр ### 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: 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 ```cpp
imu.setDLPF(imu.DLPF_MAX); IMU.setDLPF(IMU.DLPF_MAX);
``` ```
## Калибровка гироскопа ## Калибровка гироскопа
@@ -181,7 +181,7 @@ imu.setDLPF(imu.DLPF_MAX);
\\[ gyro_{xyz}=rates_{xyz}+bias_{xyz}+noise \\] \\[ 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: Программа для вывода данных с гироскопа с калибровкой:
@@ -189,23 +189,23 @@ imu.setDLPF(imu.DLPF_MAX);
#include <FlixPeriph.h> #include <FlixPeriph.h>
#include <SPI.h> #include <SPI.h>
MPU9250 imu(SPI); MPU9250 IMU(SPI);
float gyroBiasX, gyroBiasY, gyroBiasZ; // bias гироскопа float gyroBiasX, gyroBiasY, gyroBiasZ; // bias гироскопа
void setup() { void setup() {
Serial.begin(115200); Serial.begin(115200);
bool success = imu.begin(); bool success = IMU.begin();
if (!success) { if (!success) {
Serial.println("Failed to initialize the IMU"); Serial.println("Failed to initialize IMU");
} }
calibrateGyro(); calibrateGyro();
} }
void loop() { void loop() {
float gx, gy, gz; float gx, gy, gz;
imu.waitForData(); IMU.waitForData();
imu.getGyro(gx, gy, gz); IMU.getGyro(gx, gy, gz);
// Устранение bias гироскопа // Устранение bias гироскопа
gx -= gyroBiasX; gx -= gyroBiasX;
@@ -226,9 +226,9 @@ void calibrateGyro() {
// Получение 1000 измерений гироскопа // Получение 1000 измерений гироскопа
for (int i = 0; i < samples; i++) { for (int i = 0; i < samples; i++) {
imu.waitForData(); IMU.waitForData();
float gx, gy, gz; float gx, gy, gz;
imu.getGyro(gx, gy, gz); IMU.getGyro(gx, gy, gz);
gyroBiasX += gx; gyroBiasX += gx;
gyroBiasY += gy; gyroBiasY += gy;
gyroBiasZ += gz; gyroBiasZ += gz;

View File

@@ -38,13 +38,13 @@ Utility files:
### Control subsystem ### 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. * `attitudeTarget` *(Quaternion)* — target attitude of the drone.
* `ratesTarget` *(Vector)* — target angular rates, *rad/s*. * `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]. * `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`. 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. 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 ## Building the firmware
See build instructions in [usage.md](usage.md). See build instructions in [usage.md](usage.md).

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View File

@@ -4,7 +4,7 @@
Do the following: 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 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*. * **Check the chosen board**. The correct board to choose in Arduino IDE for ESP32 Mini is *WEMOS D1 MINI ESP32*.
@@ -25,7 +25,7 @@ Do the following:
* The `accel` and `gyro` fields should change as you move the drone. * 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. * **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 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 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: * **Check the motors**. Perform the following commands using Serial Monitor:
* `mfr` — should rotate front right motor (counter-clockwise). * `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). 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).* 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): 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. * `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. 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. 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. 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). 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. 2. Power up the drone.
3. Connect your computer or smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`). 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 ### 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"> <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 ### 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`. 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"> <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| |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-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="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-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="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-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="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-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 ### 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 `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. * 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!** 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). * `mrl` — should rotate rear left motor (counter-clockwise).
* `mrr` — should rotate rear right motor (clockwise). * `mrr` — should rotate rear right motor (clockwise).
Rotation diagram:
<img src="img/motors.svg" width=200>
> [!WARNING] > [!WARNING]
> Never run the motors when powering the drone from USB, always use the battery for that. > 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). 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. 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. 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] > [!TIP]
> Decrease `CTL_TILT_MAX` parameter when flying using the smartphone to make the controls less sensitive. > 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: 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. 2. Type `cr` command and follow the instructions.
3. Use the remote control to fly the drone! 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. 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. If the pilot moves the control sticks, the drone will switch back to *STAB* mode.
## Wi-Fi configuration <img src="img/parameters.png" width="400">
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
```
## Flight log ## 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 ```bash
make log make log

View File

@@ -16,7 +16,7 @@ Author: [goldarte](https://t.me/goldarte).<br>
## School 548 course ## 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"> <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 ### Selected works
Author: [KiraFlux](https://t.me/@kiraflux_0XC0000005).<br> 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> 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> Modified Flix firmware: https://github.com/KiraFlux/flix/tree/klyax.<br>
Remote control project: https://github.com/KiraFlux/ESP32-DJC.<br> Remote control project: https://github.com/KiraFlux/ESP32-DJC.<br>

View File

@@ -11,7 +11,7 @@ extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRO
extern const int RAW, ACRO, STAB, AUTO; extern const int RAW, ACRO, STAB, AUTO;
extern float t, dt, loopRate; extern float t, dt, loopRate;
extern uint16_t channels[16]; extern uint16_t channels[16];
extern float controlTime; extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
extern int mode; extern int mode;
extern bool armed; extern bool armed;
@@ -38,12 +38,11 @@ const char* motd =
"raw/stab/acro/auto - set mode\n" "raw/stab/acro/auto - set mode\n"
"rc - show RC data\n" "rc - show RC data\n"
"wifi - show Wi-Fi info\n" "wifi - show Wi-Fi info\n"
"ap <ssid> <password> - setup Wi-Fi access point\n"
"sta <ssid> <password> - setup Wi-Fi client mode\n"
"mot - show motor output\n" "mot - show motor output\n"
"log [dump] - print log header [and data]\n" "log [dump] - print log header [and data]\n"
"cr - calibrate RC\n" "cr - calibrate RC\n"
"ca - calibrate accel\n" "ca - calibrate accel\n"
"cl - calibrate level\n"
"mfr, mfl, mrr, mrl - test motor (remove props)\n" "mfr, mfl, mrr, mrl - test motor (remove props)\n"
"sys - show system info\n" "sys - show system info\n"
"reset - reset drone's state\n" "reset - reset drone's state\n"
@@ -56,7 +55,9 @@ void print(const char* format, ...) {
vsnprintf(buf, sizeof(buf), format, args); vsnprintf(buf, sizeof(buf), format, args);
va_end(args); va_end(args);
Serial.print(buf); Serial.print(buf);
#if WIFI_ENABLED
mavlinkPrint(buf); mavlinkPrint(buf);
#endif
} }
void pause(float duration) { void pause(float duration) {
@@ -64,7 +65,9 @@ void pause(float duration) {
while (t - start < duration) { while (t - start < duration) {
step(); step();
handleInput(); handleInput();
#if WIFI_ENABLED
processMavlink(); processMavlink();
#endif
delay(50); delay(50);
} }
} }
@@ -130,15 +133,12 @@ void doCommand(String str, bool echo = false) {
} }
print("\nroll: %g pitch: %g yaw: %g throttle: %g mode: %g\n", print("\nroll: %g pitch: %g yaw: %g throttle: %g mode: %g\n",
controlRoll, controlPitch, controlYaw, controlThrottle, controlMode); controlRoll, controlPitch, controlYaw, controlThrottle, controlMode);
print("time: %.1f\n", controlTime);
print("mode: %s\n", getModeName()); print("mode: %s\n", getModeName());
print("armed: %d\n", armed); print("armed: %d\n", armed);
} else if (command == "wifi") { } else if (command == "wifi") {
#if WIFI_ENABLED
printWiFiInfo(); printWiFiInfo();
} else if (command == "ap") { #endif
configWiFi(true, arg0.c_str(), arg1.c_str());
} else if (command == "sta") {
configWiFi(false, arg0.c_str(), arg1.c_str());
} else if (command == "mot") { } else if (command == "mot") {
print("front-right %g front-left %g rear-right %g rear-left %g\n", 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]); motors[MOTOR_FRONT_RIGHT], motors[MOTOR_FRONT_LEFT], motors[MOTOR_REAR_RIGHT], motors[MOTOR_REAR_LEFT]);
@@ -149,6 +149,8 @@ void doCommand(String str, bool echo = false) {
calibrateRC(); calibrateRC();
} else if (command == "ca") { } else if (command == "ca") {
calibrateAccel(); calibrateAccel();
} else if (command == "cl") {
calibrateLevel();
} else if (command == "mfr") { } else if (command == "mfr") {
testMotor(MOTOR_FRONT_RIGHT); testMotor(MOTOR_FRONT_RIGHT);
} else if (command == "mfl") { } else if (command == "mfl") {

View File

@@ -38,12 +38,6 @@ const int RAW = 0, ACRO = 1, STAB = 2, AUTO = 3; // flight modes
int mode = STAB; int mode = STAB;
bool armed = false; 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 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 pitchRatePID(PITCHRATE_P, PITCHRATE_I, PITCHRATE_D, PITCHRATE_I_LIM, RATES_D_LPF_ALPHA);
PID yawRatePID(YAWRATE_P, YAWRATE_I, YAWRATE_D); 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); Vector maxRate(ROLLRATE_MAX, PITCHRATE_MAX, YAWRATE_MAX);
float tiltMax = TILT_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 const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode; extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;

View File

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

View File

@@ -7,14 +7,18 @@
#include "quaternion.h" #include "quaternion.h"
#include "util.h" #include "util.h"
#define WIFI_ENABLED 1
extern float t, dt; float t = NAN; // current step time, s
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode; float dt; // time delta from previous step, s
extern Vector gyro, acc; float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
extern Vector rates; float controlMode = NAN;
extern Quaternion attitude; Vector gyro; // gyroscope data
extern bool landed; Vector acc; // accelerometer data, m/s/s
extern float motors[4]; 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() { void setup() {
Serial.begin(115200); Serial.begin(115200);
@@ -24,7 +28,9 @@ void setup() {
setupLED(); setupLED();
setupMotors(); setupMotors();
setLED(true); setLED(true);
#if WIFI_ENABLED
setupWiFi(); setupWiFi();
#endif
setupIMU(); setupIMU();
setupRC(); setupRC();
setLED(false); setLED(false);
@@ -39,7 +45,9 @@ void loop() {
control(); control();
sendMotors(); sendMotors();
handleInput(); handleInput();
#if WIFI_ENABLED
processMavlink(); processMavlink();
#endif
logData(); logData();
syncParameters(); syncParameters();
} }

View File

@@ -12,12 +12,9 @@
MPU9250 imu(SPI); MPU9250 imu(SPI);
Vector imuRotation(0, 0, -PI / 2); // imu orientation as Euler angles Vector imuRotation(0, 0, -PI / 2); // imu orientation as Euler angles
Vector gyro; // gyroscope output, rad/s
Vector gyroBias;
Vector acc; // accelerometer output, m/s/s
Vector accBias; Vector accBias;
Vector accScale(1, 1, 1); Vector accScale(1, 1, 1);
Vector gyroBias;
void setupIMU() { void setupIMU() {
print("Setup IMU\n"); print("Setup IMU\n");
@@ -110,6 +107,14 @@ void calibrateAccelOnce() {
accBias = (accMax + accMin) / 2; 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() { void printIMUCalibration() {
print("gyro bias: %f %f %f\n", gyroBias.x, gyroBias.y, gyroBias.z); 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); print("accel bias: %f %f %f\n", accBias.x, accBias.y, accBias.z);

View File

@@ -3,16 +3,20 @@
// MAVLink communication // MAVLink communication
#if WIFI_ENABLED
#include <MAVLink.h> #include <MAVLink.h>
#include "util.h" #include "util.h"
extern float controlTime; #define SYSTEM_ID 1
#define MAVLINK_RATE_SLOW 1
#define MAVLINK_RATE_FAST 10
bool mavlinkConnected = false; bool mavlinkConnected = false;
String mavlinkPrintBuffer; String mavlinkPrintBuffer;
int mavlinkSysId = 1;
Rate telemetryFast(10); extern float controlTime;
Rate telemetrySlow(2); extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
void processMavlink() { void processMavlink() {
sendMavlink(); sendMavlink();
@@ -25,8 +29,10 @@ void sendMavlink() {
mavlink_message_t msg; mavlink_message_t msg;
uint32_t time = t * 1000; uint32_t time = t * 1000;
if (telemetrySlow) { static Rate slow(MAVLINK_RATE_SLOW), fast(MAVLINK_RATE_FAST);
mavlink_msg_heartbeat_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, MAV_TYPE_QUADROTOR, MAV_AUTOPILOT_GENERIC,
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) | (armed ? MAV_MODE_FLAG_SAFETY_ARMED : 0) |
((mode == STAB) ? MAV_MODE_FLAG_STABILIZE_ENABLED : 0) | ((mode == STAB) ? MAV_MODE_FLAG_STABILIZE_ENABLED : 0) |
((mode == AUTO) ? MAV_MODE_FLAG_AUTO_ENABLED : MAV_MODE_FLAG_MANUAL_INPUT_ENABLED), ((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 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); MAV_VTOL_STATE_UNDEFINED, landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR);
sendMessage(&msg); sendMessage(&msg);
} }
if (telemetryFast && mavlinkConnected) { if (fast && mavlinkConnected) {
const float zeroQuat[] = {0, 0, 0, 0}; 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 time, attitude.w, attitude.x, -attitude.y, -attitude.z, rates.x, -rates.y, -rates.z, zeroQuat); // convert to frd
sendMessage(&msg); 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); 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 if (channels[0] != 0) sendMessage(&msg); // 0 means no RC input
float controls[8]; float controls[8];
memcpy(controls, motors, sizeof(motors)); 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); 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 acc.x * 1000, -acc.y * 1000, -acc.z * 1000, // convert to frd
gyro.x * 1000, -gyro.y * 1000, -gyro.z * 1000, gyro.x * 1000, -gyro.y * 1000, -gyro.z * 1000,
0, 0, 0, 0); 0, 0, 0, 0);
@@ -90,7 +96,7 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_MANUAL_CONTROL) { if (msg.msgid == MAVLINK_MSG_ID_MANUAL_CONTROL) {
mavlink_manual_control_t m; mavlink_manual_control_t m;
mavlink_msg_manual_control_decode(&msg, &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; controlThrottle = m.z / 1000.0f;
controlPitch = m.x / 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) { if (msg.msgid == MAVLINK_MSG_ID_PARAM_REQUEST_LIST) {
mavlink_param_request_list_t m; mavlink_param_request_list_t m;
mavlink_msg_param_request_list_decode(&msg, &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; mavlink_message_t msg;
for (int i = 0; i < parametersCount(); i++) { 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); getParameterName(i), getParameter(i), MAV_PARAM_TYPE_REAL32, parametersCount(), i);
sendMessage(&msg); sendMessage(&msg);
} }
@@ -116,7 +122,7 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_PARAM_REQUEST_READ) { if (msg.msgid == MAVLINK_MSG_ID_PARAM_REQUEST_READ) {
mavlink_param_request_read_t m; mavlink_param_request_read_t m;
mavlink_msg_param_request_read_decode(&msg, &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]; 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 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); memcpy(name, getParameterName(m.param_index), 16);
} }
mavlink_message_t msg; 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); name, value, MAV_PARAM_TYPE_REAL32, parametersCount(), m.param_index);
sendMessage(&msg); sendMessage(&msg);
} }
@@ -133,15 +139,14 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_PARAM_SET) { if (msg.msgid == MAVLINK_MSG_ID_PARAM_SET) {
mavlink_param_set_t m; mavlink_param_set_t m;
mavlink_msg_param_set_decode(&msg, &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]; 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 strlcpy(name, m.param_id, sizeof(name)); // param_id might be not null-terminated
bool success = setParameter(name, m.param_value); setParameter(name, m.param_value);
if (!success) return;
// send ack // send ack
mavlink_message_t msg; 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,
m.param_id, m.param_value, MAV_PARAM_TYPE_REAL32, parametersCount(), 0); // index is unknown m.param_id, m.param_value, MAV_PARAM_TYPE_REAL32, parametersCount(), 0); // index is unknown
sendMessage(&msg); sendMessage(&msg);
} }
@@ -149,17 +154,17 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_MISSION_REQUEST_LIST) { // handle to make qgc happy if (msg.msgid == MAVLINK_MSG_ID_MISSION_REQUEST_LIST) { // handle to make qgc happy
mavlink_mission_request_list_t m; mavlink_mission_request_list_t m;
mavlink_msg_mission_request_list_decode(&msg, &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_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); sendMessage(&msg);
} }
if (msg.msgid == MAVLINK_MSG_ID_SERIAL_CONTROL) { if (msg.msgid == MAVLINK_MSG_ID_SERIAL_CONTROL) {
mavlink_serial_control_t m; mavlink_serial_control_t m;
mavlink_msg_serial_control_decode(&msg, &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]; char data[MAVLINK_MSG_SERIAL_CONTROL_FIELD_DATA_LEN + 1];
strlcpy(data, (const char *)m.data, m.count); // data might be not null-terminated 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_set_attitude_target_t m;
mavlink_msg_set_attitude_target_decode(&msg, &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 // copy attitude, rates and thrust targets
ratesTarget.x = m.body_roll_rate; ratesTarget.x = m.body_roll_rate;
@@ -193,7 +198,7 @@ void handleMavlink(const void *_msg) {
mavlink_set_actuator_control_target_t m; mavlink_set_actuator_control_target_t m;
mavlink_msg_set_actuator_control_target_decode(&msg, &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(); attitudeTarget.invalidate();
ratesTarget.invalidate(); ratesTarget.invalidate();
@@ -205,12 +210,12 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_LOG_REQUEST_DATA) { if (msg.msgid == MAVLINK_MSG_ID_LOG_REQUEST_DATA) {
mavlink_log_request_data_t m; mavlink_log_request_data_t m;
mavlink_msg_log_request_data_decode(&msg, &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 // Send all log records
for (int i = 0; i < sizeof(logBuffer) / sizeof(logBuffer[0]); i++) { for (int i = 0; i < sizeof(logBuffer) / sizeof(logBuffer[0]); i++) {
mavlink_message_t msg; 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]); sizeof(logBuffer[0]), (uint8_t *)logBuffer[i]);
sendMessage(&msg); sendMessage(&msg);
} }
@@ -220,13 +225,13 @@ void handleMavlink(const void *_msg) {
if (msg.msgid == MAVLINK_MSG_ID_COMMAND_LONG) { if (msg.msgid == MAVLINK_MSG_ID_COMMAND_LONG) {
mavlink_command_long_t m; mavlink_command_long_t m;
mavlink_msg_command_long_decode(&msg, &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; mavlink_message_t response;
bool accepted = false; bool accepted = false;
if (m.command == MAV_CMD_REQUEST_MESSAGE && m.param1 == MAVLINK_MSG_ID_AUTOPILOT_VERSION) { if (m.command == MAV_CMD_REQUEST_MESSAGE && m.param1 == MAVLINK_MSG_ID_AUTOPILOT_VERSION) {
accepted = true; 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); MAV_PROTOCOL_CAPABILITY_PARAM_FLOAT | MAV_PROTOCOL_CAPABILITY_MAVLINK2, 1, 0, 1, 1, 0, 0, 0, 0, 0, 0, 0);
sendMessage(&response); sendMessage(&response);
} }
@@ -245,7 +250,7 @@ void handleMavlink(const void *_msg) {
// send command ack // send command ack
mavlink_message_t 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); sendMessage(&ack);
} }
} }
@@ -262,7 +267,7 @@ void sendMavlinkPrint() {
char data[MAVLINK_MSG_SERIAL_CONTROL_FIELD_DATA_LEN + 1]; char data[MAVLINK_MSG_SERIAL_CONTROL_FIELD_DATA_LEN + 1];
strlcpy(data, str + i, sizeof(data)); strlcpy(data, str + i, sizeof(data));
mavlink_message_t msg; 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, SERIAL_CONTROL_DEV_SHELL,
i + MAVLINK_MSG_SERIAL_CONTROL_FIELD_DATA_LEN < strlen(str) ? SERIAL_CONTROL_FLAG_MULTI : 0, // more chunks to go 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); 0, 0, strlen(data), (uint8_t *)data, 0, 0);
@@ -270,3 +275,5 @@ void sendMavlinkPrint() {
} }
mavlinkPrintBuffer.clear(); mavlinkPrintBuffer.clear();
} }
#endif

View File

@@ -17,8 +17,7 @@
#define PWM_MIN 0 #define PWM_MIN 0
#define PWM_MAX 1000000 / PWM_FREQUENCY #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_LEFT = 0;
const int MOTOR_REAR_RIGHT = 1; const int MOTOR_REAR_RIGHT = 1;
const int MOTOR_FRONT_RIGHT = 2; const int MOTOR_FRONT_RIGHT = 2;

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@@ -9,20 +9,13 @@
extern float channelZero[16]; extern float channelZero[16];
extern float channelMax[16]; extern float channelMax[16];
extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel; extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
extern int wifiMode, udpLocalPort, udpRemotePort;
extern float rcLossTimeout, descendTime;
Preferences storage; Preferences storage;
struct Parameter { struct Parameter {
const char *name; // max length is 15 (Preferences key limit) const char *name; // max length is 15 (Preferences key limit)
bool integer; float *variable;
union { float *f; int *i; }; // pointer to variable float value; // cache
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; };
}; };
Parameter parameters[] = { Parameter parameters[] = {
@@ -84,17 +77,6 @@ Parameter parameters[] = {
{"RC_THROTTLE", &throttleChannel}, {"RC_THROTTLE", &throttleChannel},
{"RC_YAW", &yawChannel}, {"RC_YAW", &yawChannel},
{"RC_MODE", &modeChannel}, {"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() { void setupParameters() {
@@ -102,10 +84,10 @@ void setupParameters() {
// Read parameters from storage // Read parameters from storage
for (auto &parameter : parameters) { for (auto &parameter : parameters) {
if (!storage.isKey(parameter.name)) { 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.variable = storage.getFloat(parameter.name, *parameter.variable);
parameter.cache = parameter.getValue(); parameter.value = *parameter.variable;
} }
} }
@@ -120,13 +102,13 @@ const char *getParameterName(int index) {
float getParameter(int index) { float getParameter(int index) {
if (index < 0 || index >= parametersCount()) return NAN; if (index < 0 || index >= parametersCount()) return NAN;
return parameters[index].getValue(); return *parameters[index].variable;
} }
float getParameter(const char *name) { float getParameter(const char *name) {
for (auto &parameter : parameters) { for (auto &parameter : parameters) {
if (strcasecmp(parameter.name, name) == 0) { if (strcmp(parameter.name, name) == 0) {
return parameter.getValue(); return *parameter.variable;
} }
} }
return NAN; return NAN;
@@ -134,9 +116,8 @@ float getParameter(const char *name) {
bool setParameter(const char *name, const float value) { bool setParameter(const char *name, const float value) {
for (auto &parameter : parameters) { for (auto &parameter : parameters) {
if (strcasecmp(parameter.name, name) == 0) { if (strcmp(parameter.name, name) == 0) {
if (parameter.integer && !isfinite(value)) return false; // can't set integer to NaN or Inf *parameter.variable = value;
parameter.setValue(value);
return true; return true;
} }
} }
@@ -149,18 +130,16 @@ void syncParameters() {
if (motorsActive()) return; // don't use flash while flying, it may cause a delay if (motorsActive()) return; // don't use flash while flying, it may cause a delay
for (auto &parameter : parameters) { for (auto &parameter : parameters) {
if (parameter.getValue() == parameter.cache) continue; // no change if (parameter.value == *parameter.variable) continue;
if (isnan(parameter.getValue()) && isnan(parameter.cache)) continue; // both are NaN if (isnan(parameter.value) && isnan(*parameter.variable)) continue; // handle NAN != NAN
if (isinf(parameter.getValue()) && isinf(parameter.cache)) continue; // both are Inf storage.putFloat(parameter.name, *parameter.variable);
parameter.value = *parameter.variable;
storage.putFloat(parameter.name, parameter.getValue());
parameter.cache = parameter.getValue(); // update cache
} }
} }
void printParameters() { void printParameters() {
for (auto &parameter : parameters) { for (auto &parameter : parameters) {
print("%s = %g\n", parameter.name, parameter.getValue()); print("%s = %g\n", parameter.name, *parameter.variable);
} }
} }

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@@ -6,21 +6,14 @@
#include <SBUS.h> #include <SBUS.h>
#include "util.h" #include "util.h"
#ifdef ESP32C3 SBUS rc(Serial2); // NOTE: Use RC(Serial2, 16, 17) if you use the old UART2 pins
SBUS rc(Serial1);
#else
SBUS rc(Serial2);
#endif
uint16_t channels[16]; // raw rc channels uint16_t channels[16]; // raw rc channels
float controlTime; // time of the last controls update
float channelZero[16]; // calibration zero values float channelZero[16]; // calibration zero values
float channelMax[16]; // calibration max values float channelMax[16]; // calibration max values
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1] // Channels mapping (using float to store in parameters):
float controlMode = NAN;
float controlTime = NAN; // time of the last controls update
// Channels mapping (nan means not assigned):
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN; float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
void setupRC() { void setupRC() {
@@ -45,11 +38,11 @@ void normalizeRC() {
controls[i] = mapf(channels[i], channelZero[i], channelMax[i], 0, 1); controls[i] = mapf(channels[i], channelZero[i], channelMax[i], 0, 1);
} }
// Update control values // Update control values
controlRoll = rollChannel >= 0 ? controls[(int)rollChannel] : 0; controlRoll = rollChannel >= 0 ? controls[(int)rollChannel] : NAN;
controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : 0; controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : NAN;
controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : 0; controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : NAN;
controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : 0; controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : NAN;
controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN; // mode switch should not have affect if not set controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN;
} }
void calibrateRC() { void calibrateRC() {

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

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

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

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

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@@ -10,15 +10,19 @@
#include "Arduino.h" #include "Arduino.h"
#include "wifi.h" #include "wifi.h"
extern float t, dt; #define WIFI_ENABLED 1
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
extern Vector rates;
extern Quaternion attitude;
extern bool landed;
extern float motors[4];
Vector gyro, acc, imuRotation; float t = NAN;
Vector accBias, gyroBias, accScale(1, 1, 1); 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 // declarations
void step(); void step();
@@ -68,7 +72,8 @@ void resetParameters();
void setLED(bool on) {}; void setLED(bool on) {};
void calibrateGyro() { print("Skip gyro calibrating\n"); }; void calibrateGyro() { print("Skip gyro calibrating\n"); };
void calibrateAccel() { print("Skip accel calibrating\n"); }; void calibrateAccel() { print("Skip accel calibrating\n"); };
void calibrateLevel() { print("Skip level calibrating\n"); };
void printIMUCalibration() { print("cal: N/A\n"); }; void printIMUCalibration() { print("cal: N/A\n"); };
void printIMUInfo() {}; void printIMUInfo() {};
void printWiFiInfo() {}; 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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@@ -43,7 +43,6 @@ records = [record for record in records if record[0] != 0]
print(f'Received records: {len(records)}') 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 = open(f'{DIR}/log/{datetime.datetime.now().isoformat()}.csv', 'wb')
log.write(header.encode() + b'\n') log.write(header.encode() + b'\n')
for record in records: for record in records:

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