60 Commits

Author SHA1 Message Date
Oleg Kalachev
c3b818c2ae Try using installable Preferences library 2025-11-18 18:19:02 +03:00
Oleg Kalachev
531b3f4d04 Use analogWrite api instead of ledc 2025-11-18 16:54:51 +03:00
Oleg Kalachev
795b248b94 Adapt firmware for non-esp32 boards 2025-11-04 13:47:41 +03:00
Oleg Kalachev
77c4b5fc5b Test build for STM32 2025-11-04 13:42:05 +03:00
Oleg Kalachev
1a017ccb97 Keep only one floating point version of map function
Two variants are redundant
2025-11-02 00:02:28 +03:00
Oleg Kalachev
7170b20d1d Simplify command for command handling 2025-10-21 19:41:10 +03:00
Oleg Kalachev
dc9aed113b Minor code fixes 2025-10-21 19:41:05 +03:00
Oleg Kalachev
08b6123eb7 Fixes to troubleshooting 2025-10-21 19:40:54 +03:00
Oleg Kalachev
1a8b63ee04 Send only mavlink heartbeats until connected 2025-10-21 19:39:17 +03:00
Oleg Kalachev
8c49a40516 Skip attitude/rate control if thrustTarget is ineffective
To prevent i term windup.
2025-10-20 23:01:17 +03:00
Oleg Kalachev
ca595edce5 Refactor PID control to simplify the code and modifications
Each PID uses its internal dt, so may be various contexts with different rate.
PID has max dt, so no need to reset explicitly.
2025-10-20 22:54:18 +03:00
KiraFlux
d06eb2a1aa Quaternion::fromBetweenVectors: pass u and v as const references (#21) 2025-10-19 20:46:46 +03:00
Oleg Kalachev
e50a9d5fea Revert t variable type to float instead of double
For the sake of simplicity and consistency.
2025-10-19 20:46:38 +03:00
Oleg Kalachev
ebac78dc0f Minor change 2025-10-19 20:46:26 +03:00
Oleg Kalachev
186cf88d84 Add generic Delay filter 2025-10-19 20:46:11 +03:00
Oleg Kalachev
253aae2220 Lowercase imu and rc variables
To make it more obvious these are variables, not classes.
2025-10-19 20:45:56 +03:00
Oleg Kalachev
6f0964fac4 Rename failsafe.ino to safety.ino
To aggregate all the safety related functionality.
2025-10-19 20:44:54 +03:00
Oleg Kalachev
1d034f268d Add ESP32-S3 build to Actions 2025-10-19 20:44:46 +03:00
Oleg Kalachev
1ca7d32862 Update VSCode settings
Disable error squiggles as they often work incorrectly.
Decrease number of include libraries to index.
2025-10-14 11:43:55 +03:00
Oleg Kalachev
ab941e34fa Fix Gazebo installation
Installation script is deprecated, install using package on Ubuntu 20.04
2025-10-13 18:56:14 +03:00
Oleg Kalachev
7bee3d1751 Improve rc failsafe logic
Don't trigger failsafe if there's no RC at all
Use AUTO mode for descending, instead of STAB
Increase RC loss timeout and descend time
2025-10-12 21:27:08 +03:00
Oleg Kalachev
06ec5f3160 Disarm the drone on simulator plugin reset
In order to reset yaw target.
2025-10-07 15:45:48 +03:00
Oleg Kalachev
c4533e3ac8 Reset yaw target when drone disarmed
Prevent unexpected behavior when the drone tries to restore its old yaw on takeoff.
2025-10-07 15:43:28 +03:00
Oleg Kalachev
e673b50f52 Include FlixPeriph header instead of MPU9250
This simplifies choosing IMU model
2025-10-07 08:43:12 +03:00
Oleg Kalachev
5151bb9133 Ensure showing correct raw data in imu command
Some IMUs will reset acc and gyro buffer on whoAmI() call
2025-10-07 08:43:06 +03:00
Oleg Kalachev
c08c8ad91c pyflix@0.9 2025-10-03 06:49:44 +03:00
Oleg Kalachev
e44f32fca7 pyflix: don't quit on any sendto error 2025-10-03 06:47:56 +03:00
Oleg Kalachev
ca03bdb260 pyflix: partially fix wireless downloading logs 2025-10-03 06:46:56 +03:00
Oleg Kalachev
b3dffe99fb pyflix: add passing event name to off method 2025-10-03 06:46:29 +03:00
Oleg Kalachev
6e6a71fa69 Remove unneeded advice from troubleshooting 2025-10-03 06:45:16 +03:00
Oleg Kalachev
838fe11f6b Simplify mode index check in set_mode 2025-09-26 05:03:36 +03:00
Oleg Kalachev
8b36509932 pyflix@0.8 2025-09-25 16:55:06 +03:00
Oleg Kalachev
0268c8ebcf Some fixes and updates in pyflix
Fix set_controls
Add set_armed method
2025-09-25 16:53:49 +03:00
Oleg Kalachev
09bf09e520 Update schematics diagram 2025-09-25 06:16:02 +03:00
Oleg Kalachev
4c89b10767 Fix fields order in psq command 2025-09-20 22:35:36 +03:00
Oleg Kalachev
a79df52959 Don't trigger rc failsafe in AUTO mode or if disamed 2025-09-20 20:36:36 +03:00
Oleg Kalachev
e88888baeb Fix rc calibration steps enumeration again 2025-09-11 11:47:28 +03:00
Oleg Kalachev
de69b228ff Fix rc calibration steps enumeration 2025-09-02 11:03:44 +03:00
Oleg Kalachev
f9739dcd7e Don't arm by mavlink command if throttle is not low 2025-08-29 03:47:51 +03:00
Oleg Kalachev
708c8f04dc Minor docs fix 2025-08-28 05:17:46 +03:00
Oleg Kalachev
2128201440 Fix simulation build 2025-08-28 01:13:38 +03:00
Oleg Kalachev
8e3c86f5ee pyflix@0.7 2025-08-28 00:52:27 +03:00
Oleg Kalachev
40fc4b96b5 Implement AUTO mode for automatic flights
Support SET_ATTITUDE_TARGET, SET_ACTUATOR_CONTROL_TARGET in mavlink.
ACTUATOR_OUTPUT_STATUS is changed ACTUATOR_CONTROL_TARGET to match used message for setting motor outputs.
Add support for changing mode from mavlink.
Support automatic flights in pyflix.
2025-08-28 00:49:24 +03:00
Oleg Kalachev
10fafbc4a0 Send udp packets in unicast after connection is established
This makes qgc connection faster.
Add WIFI_UDP_REMOTE_ADDR macro for default remote address for both the firmware and simulation.
2025-08-27 05:01:07 +03:00
Oleg Kalachev
d47d7b8bd4 Support arm/disarm mavlink commands
Refactor commands handling to remove repeating ack message packing.
2025-08-27 04:45:25 +03:00
Oleg Kalachev
a7fdc2a88f Minor change in cli help message 2025-08-27 04:43:24 +03:00
Oleg Kalachev
c1788e2c75 Refactor arming logic
Arm and disarm with gestures only: left stick right/down for arming, left/down for disarming.
Remove arming switch as it complicates arming gestures logic.
Remove MAV_CTRL_SCALE parameter as it complicates arming gestures logic, advise to decrease TILT_MAX when controlling with a smartphone.
Put some minimal thrust to motors to indicate armed state.
Rename build article to usage article, add flight instructions.
2025-08-27 03:19:26 +03:00
Oleg Kalachev
beb655fdcb Add illustration for qgc proxy for pyflix 2025-08-27 03:13:28 +03:00
Oleg Kalachev
bf0cdac111 Major update of the articles
Reflect control subsystem refactoring.
Update dataflow diagram.
Add control subsystem diagram.
Minor updates.
2025-08-27 00:09:42 +03:00
Oleg Kalachev
b21e81a68b Add cli commands for switching mode
Make mode variable int instead of enum, which is more convinient.
2025-08-26 21:55:27 +03:00
Oleg Kalachev
8418723ccc Refactor control subsystem
Add interpretControls function to convert pilot commands and mode into control targets and make control functions independent from the mode.
Add ratesExtra target for rates feed-forward; remove yawMode.
Rename controlRate to controlRates to reflect rates variable name.
Remove USER mode.
2025-08-26 01:00:56 +03:00
Oleg Kalachev
a1539157b8 Show raw values in imu command 2025-08-22 17:20:33 +03:00
Oleg Kalachev
80922dc68a Some updates to readme and build article
Add info on using USB gamepad
Replace KINGKONG transmitter with BetaFPV LiteRadio
Add RoboCamp video
2025-08-20 22:06:17 +03:00
Oleg Kalachev
fcd2738763 Add link to stls from robocamp 2025-08-19 15:20:24 +03:00
Oleg Kalachev
fa07ed3a4e Minor docs change 2025-08-15 00:51:08 +03:00
Oleg Kalachev
dee4d97ab3 Add getRoll, getPitch, setRoll, setPitch methods
Add methods to Quaternion for consistency with getYaw and setYaw
2025-08-09 18:10:11 +03:00
Oleg Kalachev
ea35db37da Minor code simplification 2025-08-09 17:53:06 +03:00
Oleg Kalachev
cd953f24ad Add RoboCamp to built drones article 2025-08-07 14:29:39 +03:00
Oleg Kalachev
3f80712641 Some updates to articles 2025-08-06 23:52:35 +03:00
Oleg Kalachev
18bacb64f3 Make rc loss timeout longer 2025-07-31 12:35:28 +03:00
49 changed files with 1097 additions and 1135 deletions

View File

@@ -23,10 +23,19 @@ jobs:
with:
name: firmware-binary
path: flix/build
- name: Build firmware without Wi-Fi
- name: Build firmware for ESP32-S3
run: make BOARD=esp32:esp32:esp32s3
- name: Build firmware with WiFi disabled
run: sed -i 's/^#define WIFI_ENABLED 1$/#define WIFI_ENABLED 0/' flix/flix.ino && make
- name: Check c_cpp_properties.json
run: tools/check_c_cpp_properties.py
- name: Build for Black Pill F411CE (STM32)
run: |
arduino-cli config set board_manager.additional_urls https://github.com/stm32duino/BoardManagerFiles/raw/main/package_stmicroelectronics_index.json
arduino-cli core install STMicroelectronics:stm32
arduino-cli board listall STMicroelectronics:stm32
arduino-cli lib install "Preferences"
make BOARD=STMicroelectronics:stm32:GenF4:pnum=BLACKPILL_F411CE
build_macos:
runs-on: macos-latest
@@ -53,15 +62,25 @@ jobs:
run: python3 tools/check_c_cpp_properties.py
build_simulator:
runs-on: ubuntu-22.04
runs-on: ubuntu-latest
container:
image: ubuntu:20.04
steps:
- name: Install dependencies
run: |
apt-get update
DEBIAN_FRONTEND=noninteractive apt-get install -y curl wget build-essential cmake g++ pkg-config gnupg2 lsb-release sudo
- name: Install Arduino CLI
uses: arduino/setup-arduino-cli@v1.1.1
- uses: actions/checkout@v4
- name: Install Gazebo
run: curl -sSL http://get.gazebosim.org | sh
run: |
sudo sh -c 'echo "deb http://packages.osrfoundation.org/gazebo/ubuntu-stable `lsb_release -cs` main" > /etc/apt/sources.list.d/gazebo-stable.list'
wget https://packages.osrfoundation.org/gazebo.key -O - | sudo apt-key add -
sudo apt-get update
sudo apt-get install -y gazebo11 libgazebo11-dev
- name: Install SDL2
run: sudo apt-get install libsdl2-dev
run: sudo apt-get install -y libsdl2-dev
- name: Build simulator
run: make build_simulator
- uses: actions/upload-artifact@v4

View File

@@ -5,13 +5,15 @@
"includePath": [
"${workspaceFolder}/flix",
"${workspaceFolder}/gazebo",
"${workspaceFolder}/tools/**",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/**",
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
"~/Arduino/libraries/**",
"/usr/include/**"
"/usr/include/gazebo-11/",
"/usr/include/ignition/math6/"
],
"forcedInclude": [
"${workspaceFolder}/.vscode/intellisense.h",
@@ -51,14 +53,14 @@
"name": "Mac",
"includePath": [
"${workspaceFolder}/flix",
// "${workspaceFolder}/gazebo",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
"~/Library/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/include/**",
"~/Library/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
"~/Documents/Arduino/libraries/**",
"/opt/homebrew/include/**"
"/opt/homebrew/include/gazebo-11/",
"/opt/homebrew/include/ignition/math6/"
],
"forcedInclude": [
"${workspaceFolder}/.vscode/intellisense.h",
@@ -100,6 +102,7 @@
"includePath": [
"${workspaceFolder}/flix",
"${workspaceFolder}/gazebo",
"${workspaceFolder}/tools/**",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",

View File

@@ -1,5 +1,6 @@
{
"C_Cpp.intelliSenseEngineFallback": "enabled",
"C_Cpp.errorSquiggles": "disabled",
"files.associations": {
"*.sdf": "xml",
"*.ino": "cpp",

View File

@@ -17,11 +17,11 @@
* Dedicated for education and research.
* Made from general-purpose components.
* Simple and clean source code in Arduino.
* Control using remote control or smartphone.
* Precise simulation with Gazebo.
* Simple and clean source code in Arduino (<2k lines firmware).
* Control using USB gamepad, remote control or smartphone.
* Wi-Fi and MAVLink support.
* Wireless command line interface and analyzing.
* Precise simulation with Gazebo.
* Python library.
* Textbook on flight control theory and practice ([in development](https://quadcopter.dev)).
* *Position control (using external camera) and autonomous flights¹*.
@@ -38,7 +38,11 @@ Version 0 demo video: https://youtu.be/8GzzIQ3C6DQ.
<a href="https://youtu.be/8GzzIQ3C6DQ"><img width=500 src="https://i3.ytimg.com/vi/8GzzIQ3C6DQ/maxresdefault.jpg"></a>
See the [user builds gallery](docs/user.md).
Usage in education (RoboCamp): https://youtu.be/Wd3yaorjTx0.
<a href="https://youtu.be/Wd3yaorjTx0"><img width=500 src="https://i3.ytimg.com/vi/Wd3yaorjTx0/sddefault.jpg"></a>
See the [user builds gallery](docs/user.md):
<a href="docs/user.md"><img src="docs/img/user/user.jpg" width=500></a>
@@ -51,7 +55,7 @@ The simulator is implemented using Gazebo and runs the original Arduino code:
## Articles
* [Assembly instructions](docs/assembly.md).
* [Building and running the code](docs/build.md).
* [Usage: build, setup and flight](docs/usage.md).
* [Troubleshooting](docs/troubleshooting.md).
* [Firmware architecture overview](docs/firmware.md).
* [Python library tutorial](tools/pyflix/README.md).
@@ -63,8 +67,8 @@ The simulator is implemented using Gazebo and runs the original Arduino code:
|Type|Part|Image|Quantity|
|-|-|:-:|:-:|
|Microcontroller board|ESP32 Mini|<img src="docs/img/esp32.jpg" width=100>|1|
|IMU (and barometer²) board|GY91, MPU-9265 (or other MPU9250/MPU6500 board)<br>ICM20948³<br>GY-521 (MPU-6050)³⁻¹|<img src="docs/img/gy-91.jpg" width=90 align=center><br><img src="docs/img/icm-20948.jpg" width=100><br><img src="docs/img/gy-521.jpg" width=100>|1|
|<span style="background:yellow">(Recommended) Buck-boost converter</span>|To be determined, output 5V or 3.3V, see [user-contributed schematics](https://miro.com/app/board/uXjVN-dTjoo=/?moveToWidget=3458764612179508274&cot=14)|<img src="docs/img/buck-boost.jpg" width=100>|1|
|IMU (and barometer²) board|GY91, MPU-9265 (or other MPU9250/MPU6500 board)<br>ICM20948V2 (ICM20948)³<br>GY-521 (MPU-6050)³⁻¹|<img src="docs/img/gy-91.jpg" width=90 align=center><br><img src="docs/img/icm-20948.jpg" width=100><br><img src="docs/img/gy-521.jpg" width=100>|1|
|<span style="background:yellow">Buck-boost converter</span> (recommended)|To be determined, output 5V or 3.3V, see [user-contributed schematics](https://miro.com/app/board/uXjVN-dTjoo=/?moveToWidget=3458764612179508274&cot=14)|<img src="docs/img/buck-boost.jpg" width=100>|1|
|Motor|8520 3.7V brushed motor (shaft 0.8mm).<br>Motor with exact 3.7V voltage is needed, not ranged working voltage (3.7V — 6V).|<img src="docs/img/motor.jpeg" width=100>|4|
|Propeller|Hubsan 55 mm|<img src="docs/img/prop.jpg" width=100>|4|
|MOSFET (transistor)|100N03A or [analog](https://t.me/opensourcequadcopter/33)|<img src="docs/img/100n03a.jpg" width=100>|4|
@@ -77,16 +81,16 @@ The simulator is implemented using Gazebo and runs the original Arduino code:
|Frame main part|3D printed⁴:<br>[`flix-frame-1.1.stl`](docs/assets/flix-frame-1.1.stl) [`flix-frame-1.1.step`](docs/assets/flix-frame-1.1.step)<br>Recommended settings: layer 0.2 mm, line 0.4 mm, infill 100%.|<img src="docs/img/frame1.jpg" width=100>|1|
|Frame top part|3D printed:<br>[`esp32-holder.stl`](docs/assets/esp32-holder.stl) [`esp32-holder.step`](docs/assets/esp32-holder.step)|<img src="docs/img/esp32-holder.jpg" width=100>|1|
|Washer for IMU board mounting|3D printed:<br>[`washer-m3.stl`](docs/assets/washer-m3.stl) [`washer-m3.step`](docs/assets/washer-m3.step)|<img src="docs/img/washer-m3.jpg" width=100>|2|
|*RC transmitter (optional)*|*KINGKONG TINY X8 (warning: lacks USB support) or other⁵*|<img src="docs/img/tx.jpg" width=100>|1|
|Controller (recommended)|CC2500 transmitter, like BetaFPV LiteRadio CC2500 (RC receiver/Wi-Fi).<br>Two-sticks gamepad (Wi-Fi only) — see [recommended gamepads](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/setup_view/joystick.html#supported-joysticks).<br>Other⁵|<img src="docs/img/betafpv.jpg" width=100><img src="docs/img/logitech.jpg" width=80>|1|
|*RC receiver (optional)*|*DF500 or other⁵*|<img src="docs/img/rx.jpg" width=100>|1|
|Wires|28 AWG recommended|<img src="docs/img/wire-28awg.jpg" width=100>||
|Tape, double-sided tape||||
*² — barometer is not used for now.*<br>
*³ — change `MPU9250` to `ICM20948` in `imu.ino` file if using ICM-20948 board.*<br>
*³ — change `MPU9250` to `ICM20948` or `MPU6050` in `imu.ino` file for using the appropriate boards.*<br>
*³⁻¹ — MPU-6050 supports I²C interface only (not recommended). To use it change IMU declaration to `MPU6050 IMU(Wire)`.*<br>
*⁴ — this frame is optimized for GY-91 board, if using other, the board mount holes positions should be modified.*<br>
*⁵ — you may use any transmitter-receiver pair with SBUS interface.*
*⁵ — you also may use any transmitter-receiver pair with SBUS interface.*
Tools required for assembly:
@@ -102,7 +106,9 @@ Feel free to modify the design and or code, and create your own improved version
### Simplified connection diagram
<img src="docs/img/schematics1.svg" width=800 alt="Flix version 1 schematics">
<img src="docs/img/schematics1.svg" width=700 alt="Flix version 1 schematics">
*(Dashed is optional).*
Motor connection scheme:

View File

@@ -1,8 +1,10 @@
# Архитектура прошивки
<img src="img/dataflow.svg" width=800 alt="Firmware dataflow diagram">
Прошивка Flix это обычный скетч Arduino, реализованный в однопоточном стиле. Код инициализации находится в функции `setup()`, а главный цикл — в функции `loop()`. Скетч состоит из нескольких файлов, каждый из которых отвечает за определенную подсистему.
Главный цикл работает на частоте 1000 Гц. Передача данных между подсистемами происходит через глобальные переменные:
<img src="img/dataflow.svg" width=600 alt="Firmware dataflow diagram">
Главный цикл `loop()` работает на частоте 1000 Гц. Передача данных между подсистемами происходит через глобальные переменные:
* `t` *(float)* — текущее время шага, *с*.
* `dt` *(float)* — дельта времени между текущим и предыдущим шагами, *с*.
@@ -15,18 +17,34 @@
## Исходные файлы
Исходные файлы прошивки находятся в директории `flix`. Ключевые файлы:
Исходные файлы прошивки находятся в директории `flix`. Основные файлы:
* [`flix.ino`](https://github.com/okalachev/flix/blob/canonical/flix/flix.ino) — основной входной файл, скетч Arduino. Включает определение глобальных переменных и главный цикл.
* [`imu.ino`](https://github.com/okalachev/flix/blob/canonical/flix/imu.ino) — чтение данных с датчика IMU (гироскоп и акселерометр), калибровка IMU.
* [`rc.ino`](https://github.com/okalachev/flix/blob/canonical/flix/rc.ino) — чтение данных с RC-приемника, калибровка RC.
* [`mavlink.ino`](https://github.com/okalachev/flix/blob/canonical/flix/mavlink.ino) — взаимодействие с QGroundControl через MAVLink.
* [`estimate.ino`](https://github.com/okalachev/flix/blob/canonical/flix/estimate.ino) — оценка ориентации дрона, комплементарный фильтр.
* [`control.ino`](https://github.com/okalachev/flix/blob/canonical/flix/control.ino) — управление ориентацией и угловыми скоростями дрона, трехмерный двухуровневый каскадный PID-регулятор.
* [`motors.ino`](https://github.com/okalachev/flix/blob/canonical/flix/motors.ino) — управление выходными сигналами на моторы через ШИМ.
* [`flix.ino`](https://github.com/okalachev/flix/blob/master/flix/flix.ino) — основной файл Arduino-скетча. Определяет некоторые глобальные переменные и главный цикл.
* [`imu.ino`](https://github.com/okalachev/flix/blob/master/flix/imu.ino) — чтение данных с датчика IMU (гироскоп и акселерометр), калибровка IMU.
* [`rc.ino`](https://github.com/okalachev/flix/blob/master/flix/rc.ino) — чтение данных с RC-приемника, калибровка RC.
* [`estimate.ino`](https://github.com/okalachev/flix/blob/master/flix/estimate.ino) — оценка ориентации дрона, комплементарный фильтр.
* [`control.ino`](https://github.com/okalachev/flix/blob/master/flix/control.ino) — подсистема управления, трехмерный двухуровневый каскадный ПИД-регулятор.
* [`motors.ino`](https://github.com/okalachev/flix/blob/master/flix/motors.ino) — выход PWM на моторы.
* [`mavlink.ino`](https://github.com/okalachev/flix/blob/master/flix/mavlink.ino) — взаимодействие с QGroundControl или [pyflix](https://github.com/okalachev/flix/tree/master/tools/pyflix) через протокол MAVLink.
Вспомогательные файлы включают:
Вспомогательные файлы:
* [`vector.h`](https://github.com/okalachev/flix/blob/canonical/flix/vector.h), [`quaternion.h`](https://github.com/okalachev/flix/blob/canonical/flix/quaternion.h) — реализация библиотек векторов и кватернионов проекта.
* [`pid.h`](https://github.com/okalachev/flix/blob/canonical/flix/pid.h) — реализация общего ПИД-регулятора.
* [`lpf.h`](https://github.com/okalachev/flix/blob/canonical/flix/lpf.h) — реализация общего фильтра нижних частот.
* [`vector.h`](https://github.com/okalachev/flix/blob/master/flix/vector.h), [`quaternion.h`](https://github.com/okalachev/flix/blob/master/flix/quaternion.h) — библиотеки векторов и кватернионов.
* [`pid.h`](https://github.com/okalachev/flix/blob/master/flix/pid.h) — ПИД-регулятор.
* [`lpf.h`](https://github.com/okalachev/flix/blob/master/flix/lpf.h) — фильтр нижних частот.
### Подсистема управления
Состояние органов управления обрабатывается в функции `interpretControls()` и преобразуется в *команду управления*, которая включает следующее:
* `attitudeTarget` *(Quaternion)* — целевая ориентация дрона.
* `ratesTarget` *(Vector)* — целевые угловые скорости, *рад/с*.
* `ratesExtra` *(Vector)* — дополнительные (feed-forward) угловые скорости, для управления рысканием в режиме STAB, *рад/с*.
* `torqueTarget` *(Vector)* — целевой крутящий момент, диапазон [-1, 1].
* `thrustTarget` *(float)* — целевая общая тяга, диапазон [0, 1].
Команда управления обрабатывается в функциях `controlAttitude()`, `controlRates()`, `controlTorque()`. Если значение одной из переменных установлено в `NAN`, то соответствующая функция пропускается.
<img src="img/control.svg" width=300 alt="Control subsystem diagram">
Состояние *armed* хранится в переменной `armed`, а текущий режим — в переменной `mode`.

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# Building and running
To build the firmware or the simulator, you need to clone the repository using git:
```bash
git clone https://github.com/okalachev/flix.git
cd flix
```
## Simulation
### Ubuntu
The latest version of Ubuntu supported by Gazebo 11 simulator is 22.04. If you have a newer version, consider using a virtual machine.
1. Install Arduino CLI:
```bash
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
```
2. Install Gazebo 11:
```bash
curl -sSL http://get.gazebosim.org | sh
```
Set up your Gazebo environment variables:
```bash
echo "source /usr/share/gazebo/setup.sh" >> ~/.bashrc
source ~/.bashrc
```
3. Install SDL2 and other dependencies:
```bash
sudo apt-get update && sudo apt-get install build-essential libsdl2-dev
```
4. Add your user to the `input` group to enable joystick support (you need to re-login after this command):
```bash
sudo usermod -a -G input $USER
```
5. Run the simulation:
```bash
make simulator
```
### macOS
1. Install Homebrew package manager, if you don't have it installed:
```bash
/bin/bash -c "$(curl -fsSL https://raw.githubusercontent.com/Homebrew/install/HEAD/install.sh)"
```
2. Install Arduino CLI, Gazebo 11 and SDL2:
```bash
brew tap osrf/simulation
brew install arduino-cli
brew install gazebo11
brew install sdl2
```
Set up your Gazebo environment variables:
```bash
echo "source /opt/homebrew/share/gazebo/setup.sh" >> ~/.zshrc
source ~/.zshrc
```
3. Run the simulation:
```bash
make simulator
```
### Setup and flight
#### Control with smartphone
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone. For **iOS**, use [QGroundControl build from TAJISOFT](https://apps.apple.com/ru/app/qgc-from-tajisoft/id1618653051).
2. Connect your smartphone to the same Wi-Fi network as the machine running the simulator.
3. If you're using a virtual machine, make sure that its network is set to the **bridged** mode with Wi-Fi adapter selected.
4. Run the simulation.
5. Open QGroundControl app. It should connect and begin showing the virtual drone's telemetry automatically.
6. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
7. Use the virtual joystick to fly the drone!
#### Control with USB remote control
1. Connect your USB remote control to the machine running the simulator.
2. Run the simulation.
3. Calibrate the RC using `cr` command in the command line interface.
4. Run the simulation again.
5. Use the USB remote control to fly the drone!
## Firmware
### Arduino IDE (Windows, Linux, macOS)
1. Install [Arduino IDE](https://www.arduino.cc/en/software) (version 2 is recommended).
2. Windows users might need to install [USB to UART bridge driver from Silicon Labs](https://www.silabs.com/developers/usb-to-uart-bridge-vcp-drivers).
3. Install ESP32 core, version 3.2.0. See the [official Espressif's instructions](https://docs.espressif.com/projects/arduino-esp32/en/latest/installing.html#installing-using-arduino-ide) on installing ESP32 Core in Arduino IDE.
4. Install the following libraries using [Library Manager](https://docs.arduino.cc/software/ide-v2/tutorials/ide-v2-installing-a-library):
* `FlixPeriph`, the latest version.
* `MAVLink`, version 2.0.16.
5. Clone the project using git or [download the source code as a ZIP archive](https://codeload.github.com/okalachev/flix/zip/refs/heads/master).
6. Open the downloaded Arduino sketch `flix/flix.ino` in Arduino IDE.
7. Connect your ESP32 board to the computer and choose correct board type in Arduino IDE (*WEMOS D1 MINI ESP32* for ESP32 Mini) and the port.
8. [Build and upload](https://docs.arduino.cc/software/ide-v2/tutorials/getting-started/ide-v2-uploading-a-sketch) the firmware using Arduino IDE.
### Command line (Windows, Linux, macOS)
1. [Install Arduino CLI](https://arduino.github.io/arduino-cli/installation/).
On Linux, use:
```bash
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
```
2. Windows users might need to install [USB to UART bridge driver from Silicon Labs](https://www.silabs.com/developers/usb-to-uart-bridge-vcp-drivers).
3. Compile the firmware using `make`. Arduino dependencies will be installed automatically:
```bash
make
```
You can flash the firmware to the board using command:
```bash
make upload
```
You can also compile the firmware, upload it and start serial port monitoring using command:
```bash
make upload monitor
```
See other available Make commands in the [Makefile](../Makefile).
> [!TIP]
> You can test the firmware on a bare ESP32 board without connecting IMU and other peripherals. The Wi-Fi network `flix` should appear and all the basic functionality including CLI and QGroundControl connection should work.
### Setup and flight
Before flight you need to calibrate the accelerometer:
1. Open Serial Monitor in Arduino IDE (or use `make monitor` command in the command line).
2. Type `ca` command there and follow the instructions.
#### Control with smartphone
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone.
2. Power the drone using the battery.
3. Connect your smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
4. Open QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
5. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
6. Use the virtual joystick to fly the drone!
#### Control with remote control
Before flight using remote control, you need to calibrate it:
1. Open Serial Monitor in Arduino IDE (or use `make monitor` command in the command line).
2. Type `cr` command there and follow the instructions.
3. Use the remote control to fly the drone!
#### Control with USB remote control
If your drone doesn't have RC receiver installed, you can use USB remote control and QGroundControl app to fly it.
1. Install [QGroundControl](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html) app on your computer.
2. Connect your USB remote control to the computer.
3. Power up the drone.
4. Connect your computer to the appeared `flix` Wi-Fi network (password: `flixwifi`).
5. Launch QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
6. Go the the QGroundControl menu ⇒ *Vehicle Setup**Joystick*. Calibrate you USB remote control there.
7. Use the USB remote control to fly the drone!
#### Adjusting parameters
You can adjust some of the drone's parameters (include PID coefficients) in QGroundControl app. In order to do that, go to the QGroundControl menu ⇒ *Vehicle Setup**Parameters*.
<img src="img/parameters.png" width="400">
#### CLI access
In addition to accessing the drone's command line interface (CLI) using the serial port, you can also access it with QGroundControl using Wi-Fi connection. To do that, go to the QGroundControl menu ⇒ *Vehicle Setup**Analyze Tools**MAVLink Console*.
<img src="img/cli.png" width="400">
> [!NOTE]
> If something goes wrong, go to the [Troubleshooting](troubleshooting.md) article.
### Firmware code structure
See [firmware overview](firmware.md) for more details.

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# Firmware overview
The firmware is a regular Arduino sketch, and follows the classic Arduino one-threaded design. The initialization code is in the `setup()` function, and the main loop is in the `loop()` function. The sketch includes multiple files, each responsible for a specific part of the system.
The firmware is a regular Arduino sketch, and it follows the classic Arduino one-threaded design. The initialization code is in the `setup()` function, and the main loop is in the `loop()` function. The sketch includes several files, each responsible for a specific subsystem.
## Dataflow
<img src="img/dataflow.svg" width=800 alt="Firmware dataflow diagram">
<img src="img/dataflow.svg" width=600 alt="Firmware dataflow diagram">
The main loop is running at 1000 Hz. All the dataflow is happening through global variables (for simplicity):
The main loop is running at 1000 Hz. All the dataflow goes through global variables (for simplicity):
* `t` *(double)* current step time, *s*.
* `t` *(float)* current step time, *s*.
* `dt` *(float)* — time delta between the current and previous steps, *s*.
* `gyro` *(Vector)* — data from the gyroscope, *rad/s*.
* `acc` *(Vector)* — acceleration data from the accelerometer, *m/s<sup>2</sup>*.
* `rates` *(Vector)* — filtered angular rates, *rad/s*.
* `attitude` *(Quaternion)* — estimated attitude (orientation) of drone.
* `controlRoll`, `controlPitch`, ... *(float[])* pilot's control inputs, range [-1, 1].
* `motors` *(float[])* motor outputs, range [0, 1].
* `controlRoll`, `controlPitch`, ... *(float[])* pilot control inputs, range [-1, 1].
* `motors` *(float[])* motor outputs, range [0, 1].
## Source files
Firmware source files are located in `flix` directory. The key files are:
Firmware source files are located in `flix` directory. The core files are:
* [`flix.ino`](../flix/flix.ino) — main entry point, Arduino sketch. Includes global variables definition and the main loop.
* [`flix.ino`](../flix/flix.ino) — Arduino sketch main file, entry point.Includes some global variable definitions and the main loop.
* [`imu.ino`](../flix/imu.ino) — reading data from the IMU sensor (gyroscope and accelerometer), IMU calibration.
* [`rc.ino`](../flix/rc.ino) — reading data from the RC receiver, RC calibration.
* [`estimate.ino`](../flix/estimate.ino) — drone's attitude estimation, complementary filter.
* [`control.ino`](../flix/control.ino) — drone's attitude and rates control, three-dimensional two-level cascade PID controller.
* [`motors.ino`](../flix/motors.ino) — PWM motor outputs control.
* [`estimate.ino`](../flix/estimate.ino) — attitude estimation, complementary filter.
* [`control.ino`](../flix/control.ino) — control subsystem, three-dimensional two-level cascade PID controller.
* [`motors.ino`](../flix/motors.ino) — PWM motor output control.
* [`mavlink.ino`](../flix/mavlink.ino) — interaction with QGroundControl or [pyflix](../tools/pyflix) via MAVLink protocol.
Utility files include:
Utility files:
* [`vector.h`](../flix/vector.h), [`quaternion.h`](../flix/quaternion.h) — project's vector and quaternion libraries implementation.
* [`pid.h`](../flix/pid.h) — generic PID controller implementation.
* [`lpf.h`](../flix/lpf.h) — generic low-pass filter implementation.
* [`vector.h`](../flix/vector.h), [`quaternion.h`](../flix/quaternion.h) — vector and quaternion libraries.
* [`pid.h`](../flix/pid.h) — generic PID controller.
* [`lpf.h`](../flix/lpf.h) — generic low-pass filter.
### Control subsystem
Pilot inputs are interpreted in `interpretControls()`, and then converted to the *control command*, which consists of the following:
* `attitudeTarget` *(Quaternion)* — target attitude of the drone.
* `ratesTarget` *(Vector)* — target angular rates, *rad/s*.
* `ratesExtra` *(Vector)* — additional (feed-forward) angular rates , used for yaw rate control in STAB mode, *rad/s*.
* `torqueTarget` *(Vector)* — target torque, range [-1, 1].
* `thrustTarget` *(float)* — collective thrust target, range [0, 1].
Control command is processed in `controlAttitude()`, `controlRates()`, `controlTorque()` functions. Each function may be skipped if the corresponding target is set to `NAN`.
<img src="img/control.svg" width=300 alt="Control subsystem diagram">
Armed state is stored in `armed` variable, and current mode is stored in `mode` variable.
## Building
See build instructions in [build.md](build.md).
See build instructions in [usage.md](usage.md).

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@@ -4,8 +4,9 @@
Do the following:
* **Check ESP32 core is installed**. Check if the version matches the one used in the [tutorial](build.md#firmware).
* **Check ESP32 core is installed**. Check if the version matches the one used in the [tutorial](usage.md#firmware).
* **Check libraries**. Install all the required libraries from the tutorial. Make sure there are no MPU9250 or other peripherals libraries that may conflict with the ones used in the tutorial.
* **Check the chosen board**. The correct board to choose in Arduino IDE for ESP32 Mini is *WEMOS D1 MINI ESP32*.
## The drone doesn't fly
@@ -14,7 +15,7 @@ Do the following:
* **Check the battery voltage**. Use a multimeter to measure the battery voltage. It should be in range of 3.7-4.2 V.
* **Check if there are some startup errors**. Connect the ESP32 to the computer and check the Serial Monitor output. Use the Reset button to make sure you see the whole ESP32 output.
* **Check the baudrate is correct**. If you see garbage characters in the Serial Monitor, make sure the baudrate is set to 115200.
* **Make sure correct IMU model is chosen**. If using ICM-20948 board, change `MPU9250` to `ICM20948` everywhere in the `imu.ino` file.
* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
* **Check if the CLI is working**. Perform `help` command in Serial Monitor. You should see the list of available commands. You can also access the CLI using QGroundControl (*Vehicle Setup* ⇒ *Analyze Tools**MAVLink Console*).
* **Configure QGroundControl correctly before connecting to the drone** if you use it to control the drone. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
* **If QGroundControl doesn't connect**, you might need to disable the firewall and/or VPN on your computer.
@@ -31,7 +32,6 @@ Do the following:
* `mfl` — should rotate front left motor (clockwise).
* `mrl` — should rotate rear left motor (counter-clockwise).
* `mrr` — should rotate rear right motor (clockwise).
* **Calibrate the RC** if you use it. Type `cr` command in Serial Monitor and follow the instructions.
* **Check the RC data** if you use it. Use `rc` command, `Control` should show correct values between -1 and 1, and between 0 and 1 for the throttle.
* **Check the remote control**. Using `rc` command, check the control values reflect your sticks movement. All the controls should change between -1 and 1, and throttle between 0 and 1.
* If using SBUS receiver, **calibrate the RC**. Type `cr` command in Serial Monitor and follow the instructions.
* **Check the IMU output using QGroundControl**. Connect to the drone using QGroundControl on your computer. Go to the *Analyze* tab, *MAVLINK Inspector*. Plot the data from the `SCALED_IMU` message. The gyroscope and accelerometer data should change according to the drone movement.
* **Check the gyroscope only attitude estimation**. Comment out `applyAcc();` line in `estimate.ino` and check if the attitude estimation in QGroundControl. It should be stable, but only drift very slowly.

252
docs/usage.md Normal file
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@@ -0,0 +1,252 @@
# Usage: build, setup and flight
To use Flix, you need to build the firmware and upload it to the ESP32 board. For simulation, you need to build and run the simulator.
For the start, clone the repository using git:
```bash
git clone https://github.com/okalachev/flix.git
cd flix
```
## Simulation
### Ubuntu
The latest version of Ubuntu supported by Gazebo 11 simulator is 20.04. If you have a newer version, consider using a virtual machine.
1. Install Arduino CLI:
```bash
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
```
2. Install Gazebo 11:
```bash
sudo sh -c 'echo "deb http://packages.osrfoundation.org/gazebo/ubuntu-stable `lsb_release -cs` main" > /etc/apt/sources.list.d/gazebo-stable.list'
wget https://packages.osrfoundation.org/gazebo.key -O - | sudo apt-key add -
sudo apt-get update
sudo apt-get install -y gazebo11 libgazebo11-dev
```
Set up your Gazebo environment variables:
```bash
echo "source /usr/share/gazebo/setup.sh" >> ~/.bashrc
source ~/.bashrc
```
3. Install SDL2 and other dependencies:
```bash
sudo apt-get update && sudo apt-get install build-essential libsdl2-dev
```
4. Add your user to the `input` group to enable joystick support (you need to re-login after this command):
```bash
sudo usermod -a -G input $USER
```
5. Run the simulation:
```bash
make simulator
```
### macOS
1. Install Homebrew package manager, if you don't have it installed:
```bash
/bin/bash -c "$(curl -fsSL https://raw.githubusercontent.com/Homebrew/install/HEAD/install.sh)"
```
2. Install Arduino CLI, Gazebo 11 and SDL2:
```bash
brew tap osrf/simulation
brew install arduino-cli
brew install gazebo11
brew install sdl2
```
Set up your Gazebo environment variables:
```bash
echo "source /opt/homebrew/share/gazebo/setup.sh" >> ~/.zshrc
source ~/.zshrc
```
3. Run the simulation:
```bash
make simulator
```
### Setup
#### Control with smartphone
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone. For **iOS**, use [QGroundControl build from TAJISOFT](https://apps.apple.com/ru/app/qgc-from-tajisoft/id1618653051).
2. Connect your smartphone to the same Wi-Fi network as the machine running the simulator.
3. If you're using a virtual machine, make sure that its network is set to the **bridged** mode with Wi-Fi adapter selected.
4. Run the simulation.
5. Open QGroundControl app. It should connect and begin showing the virtual drone's telemetry automatically.
6. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
7. Use the virtual joystick to fly the drone!
#### Control with USB remote control
1. Connect your USB remote control to the machine running the simulator.
2. Run the simulation.
3. Calibrate the RC using `cr` command in the command line interface.
4. Run the simulation again.
5. Use the USB remote control to fly the drone!
## Firmware
### Arduino IDE (Windows, Linux, macOS)
1. Install [Arduino IDE](https://www.arduino.cc/en/software) (version 2 is recommended).
2. Windows users might need to install [USB to UART bridge driver from Silicon Labs](https://www.silabs.com/developers/usb-to-uart-bridge-vcp-drivers).
3. Install ESP32 core, version 3.2.0. See the [official Espressif's instructions](https://docs.espressif.com/projects/arduino-esp32/en/latest/installing.html#installing-using-arduino-ide) on installing ESP32 Core in Arduino IDE.
4. Install the following libraries using [Library Manager](https://docs.arduino.cc/software/ide-v2/tutorials/ide-v2-installing-a-library):
* `FlixPeriph`, the latest version.
* `MAVLink`, version 2.0.16.
5. Clone the project using git or [download the source code as a ZIP archive](https://codeload.github.com/okalachev/flix/zip/refs/heads/master).
6. Open the downloaded Arduino sketch `flix/flix.ino` in Arduino IDE.
7. Connect your ESP32 board to the computer and choose correct board type in Arduino IDE (*WEMOS D1 MINI ESP32* for ESP32 Mini) and the port.
8. [Build and upload](https://docs.arduino.cc/software/ide-v2/tutorials/getting-started/ide-v2-uploading-a-sketch) the firmware using Arduino IDE.
### Command line (Windows, Linux, macOS)
1. [Install Arduino CLI](https://arduino.github.io/arduino-cli/installation/).
On Linux, use:
```bash
curl -fsSL https://raw.githubusercontent.com/arduino/arduino-cli/master/install.sh | BINDIR=~/.local/bin sh
```
2. Windows users might need to install [USB to UART bridge driver from Silicon Labs](https://www.silabs.com/developers/usb-to-uart-bridge-vcp-drivers).
3. Compile the firmware using `make`. Arduino dependencies will be installed automatically:
```bash
make
```
You can flash the firmware to the board using command:
```bash
make upload
```
You can also compile the firmware, upload it and start serial port monitoring using command:
```bash
make upload monitor
```
See other available Make commands in the [Makefile](../Makefile).
> [!TIP]
> You can test the firmware on a bare ESP32 board without connecting IMU and other peripherals. The Wi-Fi network `flix` should appear and all the basic functionality including CLI and QGroundControl connection should work.
### Setup
Before flight you need to calibrate the accelerometer:
1. Open Serial Monitor in Arduino IDE (or use `make monitor` command in the command line).
2. Type `ca` command there and follow the instructions.
#### Control with smartphone
1. Install [QGroundControl mobile app](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html#android) on your smartphone.
2. Power the drone using the battery.
3. Connect your smartphone to the appeared `flix` Wi-Fi network (password: `flixwifi`).
4. Open QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
5. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
6. Use the virtual joystick to fly the drone!
> [!TIP]
> Decrease `TILT_MAX` parameter when flying using the smartphone to make the controls less sensitive.
#### Control with remote control
Before flight using remote control, you need to calibrate it:
1. Open Serial Monitor in Arduino IDE (or use `make monitor` command in the command line).
2. Type `cr` command there and follow the instructions.
3. Use the remote control to fly the drone!
#### Control with USB remote control (Wi-Fi)
If your drone doesn't have RC receiver installed, you can use USB remote control and QGroundControl app to fly it.
1. Install [QGroundControl](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/getting_started/download_and_install.html) app on your computer.
2. Connect your USB remote control to the computer.
3. Power up the drone.
4. Connect your computer to the appeared `flix` Wi-Fi network (password: `flixwifi`).
5. Launch QGroundControl app. It should connect and begin showing the drone's telemetry automatically.
6. Go the the QGroundControl menu ⇒ *Vehicle Setup**Joystick*. Calibrate you USB remote control there.
7. Use the USB remote control to fly the drone!
> [!NOTE]
> If something goes wrong, go to the [Troubleshooting](troubleshooting.md) article.
## Flight
For both virtual sticks and a physical joystick, the default control scheme is left stick for throttle and yaw and right stick for pitch and roll:
<img src="img/controls.svg" width="300">
### Arming and disarming
To start the motors, you should **arm** the drone. To do that, move the left stick to the bottom right corner:
<img src="img/arming.svg" width="150">
After that, the motors **will start spinning** at low speed, indicating that the drone is armed and ready to fly.
When finished flying, **disarm** the drone, moving the left stick to the bottom left corner:
<img src="img/disarming.svg" width="150">
### Flight modes
Flight mode is changed using mode switch on the remote control or using the command line.
#### STAB
The default mode is *STAB*. In this mode, the drone stabilizes its attitude (orientation). The left stick controls throttle and yaw rate, the right stick controls pitch and roll angles.
> [!IMPORTANT]
> The drone doesn't stabilize its position, so slight drift is possible. The pilot should compensate it manually.
#### ACRO
In this mode, the pilot controls the angular rates. This control method is difficult to fly and mostly used in FPV racing.
#### MANUAL
Manual mode disables all the stabilization, and the pilot inputs are passed directly to the motors. This mode is intended for testing and demonstration purposes only, and basically the drone **cannot fly in this mode**.
#### AUTO
In this mode, the pilot inputs are ignored (except the mode switch, if configured). The drone can be controlled using [pyflix](../tools/pyflix/) Python library, or by modifying the firmware to implement the needed autonomous behavior.
If the pilot moves the control sticks, the drone will switch back to *STAB* mode.
## Adjusting parameters
You can adjust some of the drone's parameters (include PID coefficients) in QGroundControl app. In order to do that, go to the QGroundControl menu ⇒ *Vehicle Setup**Parameters*.
<img src="img/parameters.png" width="400">
## CLI access
In addition to accessing the drone's command line interface (CLI) using the serial port, you can also access it with QGroundControl using Wi-Fi connection. To do that, go to the QGroundControl menu ⇒ *Vehicle Setup**Analyze Tools**MAVLink Console*.
<img src="img/cli.png" width="400">

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@@ -4,6 +4,25 @@ This page contains user-built drones based on the Flix project. Publish your pro
---
## RoboCamp
Author: RoboCamp participants.<br>
Description: 3D-printed and wooden frames, ESP32 Mini, DC-DC buck-boost converters. BetaFPV LiteRadio 3 to control the drones via Wi-Fi connection.<br>
Features: altitude hold, obstacle avoidance, autonomous flight elements.<br>
Some of the designed model files: https://drive.google.com/drive/folders/18YHWGquKeIevzrMH4-OUT-zKXMETTEUu?usp=share_link.
RoboCamp took place in July 2025, Saint Petersburg, where 9 participants designed and built their own drones using the Flix project, and then modified the firmware to complete specific flight tasks.
See the detailed video about the event:
<a href="https://youtu.be/Wd3yaorjTx0"><img width=500 src="https://img.youtube.com/vi/Wd3yaorjTx0/sddefault.jpg"></a>
Built drones:
<img src="img/user/robocamp/1.jpg" width=500>
---
Author: chkroko.<br>
Description: the first Flix drone built with **brushless motors** (DShot interface).<br>
Features: SpeedyBee BLS 35A Mini V2 ESC, ESP32-S3 board, EMAX ECO 2 2207 1700kv motors, ICM20948V2 IMU, INA226 power monitor and Bluetooth gamepad for control.<br>

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@@ -8,10 +8,12 @@
#include "util.h"
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern float loopRate, dt;
extern double t;
extern const int ACRO, STAB, AUTO;
extern float t, dt, loopRate;
extern uint16_t channels[16];
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlArmed, controlMode;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
extern int mode;
extern bool armed;
const char* motd =
"\nWelcome to\n"
@@ -31,6 +33,9 @@ const char* motd =
"ps - show pitch/roll/yaw\n"
"psq - show attitude quaternion\n"
"imu - show IMU data\n"
"arm - arm the drone\n"
"disarm - disarm the drone\n"
"stab/acro/auto - set mode\n"
"rc - show RC data\n"
"mot - show motor output\n"
"log - dump in-RAM log\n"
@@ -54,7 +59,7 @@ void print(const char* format, ...) {
}
void pause(float duration) {
double start = t;
float start = t;
while (t - start < duration) {
step();
handleInput();
@@ -69,9 +74,10 @@ void doCommand(String str, bool echo = false) {
// parse command
String command, arg0, arg1;
splitString(str, command, arg0, arg1);
if (command.isEmpty()) return;
// echo command
if (echo && !command.isEmpty()) {
if (echo) {
print("> %s\n", str.c_str());
}
@@ -101,22 +107,30 @@ void doCommand(String str, bool echo = false) {
Vector a = attitude.toEuler();
print("roll: %f pitch: %f yaw: %f\n", degrees(a.x), degrees(a.y), degrees(a.z));
} else if (command == "psq") {
print("qx: %f qy: %f qz: %f qw: %f\n", attitude.x, attitude.y, attitude.z, attitude.w);
print("qw: %f qx: %f qy: %f qz: %f\n", attitude.w, attitude.x, attitude.y, attitude.z);
} else if (command == "imu") {
printIMUInfo();
print("gyro: %f %f %f\n", rates.x, rates.y, rates.z);
print("acc: %f %f %f\n", acc.x, acc.y, acc.z);
printIMUCalibration();
print("rate: %.0f\n", loopRate);
print("landed: %d\n", landed);
} else if (command == "arm") {
armed = true;
} else if (command == "disarm") {
armed = false;
} else if (command == "stab") {
mode = STAB;
} else if (command == "acro") {
mode = ACRO;
} else if (command == "auto") {
mode = AUTO;
} else if (command == "rc") {
print("channels: ");
for (int i = 0; i < 16; i++) {
print("%u ", channels[i]);
}
print("\nroll: %g pitch: %g yaw: %g throttle: %g armed: %g mode: %g\n",
controlRoll, controlPitch, controlYaw, controlThrottle, controlArmed, controlMode);
print("\nroll: %g pitch: %g yaw: %g throttle: %g mode: %g\n",
controlRoll, controlPitch, controlYaw, controlThrottle, controlMode);
print("mode: %s\n", getModeName());
print("armed: %d\n", armed);
} else if (command == "mot") {
print("front-right %g front-left %g rear-right %g rear-left %g\n",
motors[MOTOR_FRONT_RIGHT], motors[MOTOR_FRONT_LEFT], motors[MOTOR_REAR_RIGHT], motors[MOTOR_REAR_LEFT]);
@@ -157,8 +171,6 @@ void doCommand(String str, bool echo = false) {
attitude = Quaternion();
} else if (command == "reboot") {
ESP.restart();
} else if (command == "") {
// do nothing
} else {
print("Invalid command: %s\n", command.c_str());
}

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@@ -34,8 +34,8 @@
#define TILT_MAX radians(30)
#define RATES_D_LPF_ALPHA 0.2 // cutoff frequency ~ 40 Hz
enum { MANUAL, ACRO, STAB, USER } mode = STAB;
enum { YAW, YAW_RATE } yawMode = YAW;
const int MANUAL = 0, ACRO = 1, STAB = 2, AUTO = 3; // flight modes
int mode = STAB;
bool armed = false;
PID rollRatePID(ROLLRATE_P, ROLLRATE_I, ROLLRATE_D, ROLLRATE_I_LIM, RATES_D_LPF_ALPHA);
@@ -49,75 +49,57 @@ float tiltMax = TILT_MAX;
Quaternion attitudeTarget;
Vector ratesTarget;
Vector ratesExtra; // feedforward rates
Vector torqueTarget;
float thrustTarget;
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlArmed, controlMode;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
void control() {
interpretRC();
interpretControls();
failsafe();
if (mode == STAB) {
controlAttitude();
controlRate();
controlTorque();
} else if (mode == ACRO) {
controlRate();
controlTorque();
} else if (mode == MANUAL) {
controlTorque();
}
controlAttitude();
controlRates();
controlTorque();
}
void interpretRC() {
armed = controlThrottle >= 0.05 && controlArmed >= 0.5;
void interpretControls() {
// NOTE: put ACRO or MANUAL modes there if you want to use them
if (controlMode < 0.25) {
mode = STAB;
} else if (controlMode < 0.75) {
mode = STAB;
} else {
mode = STAB;
}
if (controlMode < 0.25) mode = STAB;
if (controlMode < 0.75) mode = STAB;
if (controlMode > 0.75) mode = STAB;
if (mode == AUTO) return; // pilot is not effective in AUTO mode
if (controlThrottle < 0.05 && controlYaw > 0.95) armed = true; // arm gesture
if (controlThrottle < 0.05 && controlYaw < -0.95) armed = false; // disarm gesture
thrustTarget = controlThrottle;
if (mode == ACRO) {
yawMode = YAW_RATE;
ratesTarget.x = controlRoll * maxRate.x;
ratesTarget.y = controlPitch* maxRate.y;
ratesTarget.z = -controlYaw * maxRate.z; // positive yaw stick means clockwise rotation in FLU
} else if (mode == STAB) {
yawMode = controlYaw == 0 ? YAW : YAW_RATE;
attitudeTarget = Quaternion::fromEuler(Vector(
controlRoll * tiltMax,
controlPitch * tiltMax,
attitudeTarget.getYaw()));
ratesTarget.z = -controlYaw * maxRate.z; // positive yaw stick means clockwise rotation in FLU
} else if (mode == MANUAL) {
// passthrough mode
yawMode = YAW_RATE;
torqueTarget = Vector(controlRoll, controlPitch, -controlYaw) * 0.01;
if (mode == STAB) {
float yawTarget = attitudeTarget.getYaw();
if (!armed || invalid(yawTarget) || controlYaw != 0) yawTarget = attitude.getYaw(); // reset yaw target
attitudeTarget = Quaternion::fromEuler(Vector(controlRoll * tiltMax, controlPitch * tiltMax, yawTarget));
ratesExtra = Vector(0, 0, -controlYaw * maxRate.z); // positive yaw stick means clockwise rotation in FLU
}
if (yawMode == YAW_RATE || !motorsActive()) {
// update yaw target as we don't have control over the yaw
attitudeTarget.setYaw(attitude.getYaw());
if (mode == ACRO) {
attitudeTarget.invalidate(); // skip attitude control
ratesTarget.x = controlRoll * maxRate.x;
ratesTarget.y = controlPitch * maxRate.y;
ratesTarget.z = -controlYaw * maxRate.z; // positive yaw stick means clockwise rotation in FLU
}
if (mode == MANUAL) { // passthrough mode
attitudeTarget.invalidate(); // skip attitude control
ratesTarget.invalidate(); // skip rate control
torqueTarget = Vector(controlRoll, controlPitch, -controlYaw) * 0.01;
}
}
void controlAttitude() {
if (!armed) {
rollPID.reset();
pitchPID.reset();
yawPID.reset();
return;
}
if (!armed || attitudeTarget.invalid() || thrustTarget < 0.1) return; // skip attitude control
const Vector up(0, 0, 1);
Vector upActual = Quaternion::rotateVector(up, attitude);
@@ -125,34 +107,38 @@ void controlAttitude() {
Vector error = Vector::rotationVectorBetween(upTarget, upActual);
ratesTarget.x = rollPID.update(error.x, dt);
ratesTarget.y = pitchPID.update(error.y, dt);
ratesTarget.x = rollPID.update(error.x) + ratesExtra.x;
ratesTarget.y = pitchPID.update(error.y) + ratesExtra.y;
if (yawMode == YAW) {
float yawError = wrapAngle(attitudeTarget.getYaw() - attitude.getYaw());
ratesTarget.z = yawPID.update(yawError, dt);
}
float yawError = wrapAngle(attitudeTarget.getYaw() - attitude.getYaw());
ratesTarget.z = yawPID.update(yawError) + ratesExtra.z;
}
void controlRate() {
if (!armed) {
rollRatePID.reset();
pitchRatePID.reset();
yawRatePID.reset();
return;
}
void controlRates() {
if (!armed || ratesTarget.invalid() || thrustTarget < 0.1) return; // skip rates control
Vector error = ratesTarget - rates;
// Calculate desired torque, where 0 - no torque, 1 - maximum possible torque
torqueTarget.x = rollRatePID.update(error.x, dt);
torqueTarget.y = pitchRatePID.update(error.y, dt);
torqueTarget.z = yawRatePID.update(error.z, dt);
torqueTarget.x = rollRatePID.update(error.x);
torqueTarget.y = pitchRatePID.update(error.y);
torqueTarget.z = yawRatePID.update(error.z);
}
void controlTorque() {
if (!torqueTarget.valid()) return; // skip torque control
if (!armed) {
memset(motors, 0, sizeof(motors));
memset(motors, 0, sizeof(motors)); // stop motors if disarmed
return;
}
if (thrustTarget < 0.1) {
motors[0] = 0.1; // idle thrust
motors[1] = 0.1;
motors[2] = 0.1;
motors[3] = 0.1;
return;
}
@@ -172,7 +158,7 @@ const char* getModeName() {
case MANUAL: return "MANUAL";
case ACRO: return "ACRO";
case STAB: return "STAB";
case USER: return "USER";
case AUTO: return "AUTO";
default: return "UNKNOWN";
}
}

View File

@@ -11,8 +11,6 @@
#define WEIGHT_ACC 0.003
#define RATES_LFP_ALPHA 0.2 // cutoff frequency ~ 40 Hz
LowPassFilter<Vector> ratesFilter(RATES_LFP_ALPHA);
void estimate() {
applyGyro();
applyAcc();
@@ -20,6 +18,7 @@ void estimate() {
void applyGyro() {
// filter gyro to get angular rates
static LowPassFilter<Vector> ratesFilter(RATES_LFP_ALPHA);
rates = ratesFilter.update(gyro);
// apply rates to attitude

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@@ -1,41 +0,0 @@
// Copyright (c) 2024 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Fail-safe functions
#define RC_LOSS_TIMEOUT 0.2
#define DESCEND_TIME 3.0 // time to descend from full throttle to zero
extern double controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw;
void failsafe() {
armingFailsafe();
rcLossFailsafe();
}
// Prevent arming without zero throttle input
void armingFailsafe() {
static double zeroThrottleTime;
static double armingTime;
if (!armed) armingTime = t; // stores the last time when the drone was disarmed, therefore contains arming time
if (controlTime > 0 && controlThrottle < 0.05) zeroThrottleTime = controlTime;
if (armingTime - zeroThrottleTime > 0.1) armed = false; // prevent arming if there was no zero throttle for 0.1 sec
}
// RC loss failsafe
void rcLossFailsafe() {
if (t - controlTime > RC_LOSS_TIMEOUT) {
descend();
}
}
// Smooth descend on RC lost
void descend() {
mode = STAB;
controlRoll = 0;
controlPitch = 0;
controlYaw = 0;
controlThrottle -= dt / DESCEND_TIME;
if (controlThrottle < 0) controlThrottle = 0;
}

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@@ -10,9 +10,10 @@
#define SERIAL_BAUDRATE 115200
#define WIFI_ENABLED 1
double t = NAN; // current step time, s
float t = NAN; // current step time, s
float dt; // time delta from previous step, s
float controlRoll, controlPitch, controlYaw, controlThrottle, controlArmed, controlMode; // pilot's inputs, range [-1, 1]
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
float controlMode = NAN;
Vector gyro; // gyroscope data
Vector acc; // accelerometer data, m/s/s
Vector rates; // filtered angular rates, rad/s

View File

@@ -4,11 +4,12 @@
// Work with the IMU sensor
#include <SPI.h>
#include <MPU9250.h>
#include <FlixPeriph.h>
#include "vector.h"
#include "lpf.h"
#include "util.h"
MPU9250 IMU(SPI);
MPU9250 imu(SPI);
Vector accBias;
Vector accScale(1, 1, 1);
@@ -16,22 +17,22 @@ Vector gyroBias;
void setupIMU() {
print("Setup IMU\n");
IMU.begin();
imu.begin();
configureIMU();
}
void configureIMU() {
IMU.setAccelRange(IMU.ACCEL_RANGE_4G);
IMU.setGyroRange(IMU.GYRO_RANGE_2000DPS);
IMU.setDLPF(IMU.DLPF_MAX);
IMU.setRate(IMU.RATE_1KHZ_APPROX);
IMU.setupInterrupt();
imu.setAccelRange(imu.ACCEL_RANGE_4G);
imu.setGyroRange(imu.GYRO_RANGE_2000DPS);
imu.setDLPF(imu.DLPF_MAX);
imu.setRate(imu.RATE_1KHZ_APPROX);
imu.setupInterrupt();
}
void readIMU() {
IMU.waitForData();
IMU.getGyro(gyro.x, gyro.y, gyro.z);
IMU.getAccel(acc.x, acc.y, acc.z);
imu.waitForData();
imu.getGyro(gyro.x, gyro.y, gyro.z);
imu.getAccel(acc.x, acc.y, acc.z);
calibrateGyroOnce();
// apply scale and bias
acc = (acc - accBias) / accScale;
@@ -49,9 +50,8 @@ void rotateIMU(Vector& data) {
}
void calibrateGyroOnce() {
static float landedTime = 0;
landedTime = landed ? landedTime + dt : 0;
if (landedTime < 2) return; // calibrate only if definitely stationary
static Delay landedDelay(2);
if (!landedDelay.update(landed)) return; // calibrate only if definitely stationary
static LowPassFilter<Vector> gyroCalibrationFilter(0.001);
gyroBias = gyroCalibrationFilter.update(gyro);
@@ -59,7 +59,7 @@ void calibrateGyroOnce() {
void calibrateAccel() {
print("Calibrating accelerometer\n");
IMU.setAccelRange(IMU.ACCEL_RANGE_2G); // the most sensitive mode
imu.setAccelRange(imu.ACCEL_RANGE_2G); // the most sensitive mode
print("1/6 Place level [8 sec]\n");
pause(8);
@@ -93,9 +93,9 @@ void calibrateAccelOnce() {
// Compute the average of the accelerometer readings
acc = Vector(0, 0, 0);
for (int i = 0; i < samples; i++) {
IMU.waitForData();
imu.waitForData();
Vector sample;
IMU.getAccel(sample.x, sample.y, sample.z);
imu.getAccel(sample.x, sample.y, sample.z);
acc = acc + sample;
}
acc = acc / samples;
@@ -119,7 +119,16 @@ void printIMUCalibration() {
}
void printIMUInfo() {
IMU.status() ? print("status: ERROR %d\n", IMU.status()) : print("status: OK\n");
print("model: %s\n", IMU.getModel());
print("who am I: 0x%02X\n", IMU.whoAmI());
imu.status() ? print("status: ERROR %d\n", imu.status()) : print("status: OK\n");
print("model: %s\n", imu.getModel());
print("who am I: 0x%02X\n", imu.whoAmI());
print("rate: %.0f\n", loopRate);
print("gyro: %f %f %f\n", rates.x, rates.y, rates.z);
print("acc: %f %f %f\n", acc.x, acc.y, acc.z);
imu.waitForData();
Vector rawGyro, rawAcc;
imu.getGyro(rawGyro.x, rawGyro.y, rawGyro.z);
imu.getAccel(rawAcc.x, rawAcc.y, rawAcc.z);
print("raw gyro: %f %f %f\n", rawGyro.x, rawGyro.y, rawGyro.z);
print("raw acc: %f %f %f\n", rawAcc.x, rawAcc.y, rawAcc.z);
}

View File

@@ -10,7 +10,6 @@
#define LOG_PERIOD 1.0 / LOG_RATE
#define LOG_SIZE LOG_DURATION * LOG_RATE
float tFloat;
Vector attitudeEuler;
Vector attitudeTargetEuler;
@@ -20,7 +19,7 @@ struct LogEntry {
};
LogEntry logEntries[] = {
{"t", &tFloat},
{"t", &t},
{"rates.x", &rates.x},
{"rates.y", &rates.y},
{"rates.z", &rates.z},
@@ -40,7 +39,6 @@ const int logColumns = sizeof(logEntries) / sizeof(logEntries[0]);
float logBuffer[LOG_SIZE][logColumns];
void prepareLogData() {
tFloat = t;
attitudeEuler = attitude.toEuler();
attitudeTargetEuler = attitudeTarget.toEuler();
}
@@ -48,7 +46,7 @@ void prepareLogData() {
void logData() {
if (!armed) return;
static int logPointer = 0;
static double logTime = 0;
static float logTime = 0;
if (t - logTime < LOG_PERIOD) return;
logTime = t;

View File

@@ -12,11 +12,11 @@
#define PERIOD_FAST 0.1
#define MAVLINK_CONTROL_YAW_DEAD_ZONE 0.1f
float mavlinkControlScale = 0.7;
bool mavlinkConnected = false;
String mavlinkPrintBuffer;
extern double controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlArmed, controlMode;
extern float controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
void processMavlink() {
sendMavlink();
@@ -26,8 +26,8 @@ void processMavlink() {
void sendMavlink() {
sendMavlinkPrint();
static double lastSlow = 0;
static double lastFast = 0;
static float lastSlow = 0;
static float lastFast = 0;
mavlink_message_t msg;
uint32_t time = t * 1000;
@@ -36,16 +36,20 @@ void sendMavlink() {
lastSlow = t;
mavlink_msg_heartbeat_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, MAV_TYPE_QUADROTOR, MAV_AUTOPILOT_GENERIC,
MAV_MODE_FLAG_MANUAL_INPUT_ENABLED | (armed * MAV_MODE_FLAG_SAFETY_ARMED) | ((mode == STAB) * MAV_MODE_FLAG_STABILIZE_ENABLED),
(armed ? MAV_MODE_FLAG_SAFETY_ARMED : 0) |
((mode == STAB) ? MAV_MODE_FLAG_STABILIZE_ENABLED : 0) |
((mode == AUTO) ? MAV_MODE_FLAG_AUTO_ENABLED : MAV_MODE_FLAG_MANUAL_INPUT_ENABLED),
mode, MAV_STATE_STANDBY);
sendMessage(&msg);
if (!mavlinkConnected) return; // send only heartbeat until connected
mavlink_msg_extended_sys_state_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg,
MAV_VTOL_STATE_UNDEFINED, landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR);
sendMessage(&msg);
}
if (t - lastFast >= PERIOD_FAST) {
if (t - lastFast >= PERIOD_FAST && mavlinkConnected) {
lastFast = t;
const float zeroQuat[] = {0, 0, 0, 0};
@@ -57,9 +61,9 @@ void sendMavlink() {
channels[0], channels[1], channels[2], channels[3], channels[4], channels[5], channels[6], channels[7], UINT8_MAX);
if (channels[0] != 0) sendMessage(&msg); // 0 means no RC input
float actuator[32];
memcpy(actuator, motors, sizeof(motors));
mavlink_msg_actuator_output_status_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time, 4, actuator);
float controls[8];
memcpy(controls, motors, sizeof(motors));
mavlink_msg_actuator_control_target_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time, 0, controls);
sendMessage(&msg);
mavlink_msg_scaled_imu_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, time,
@@ -79,6 +83,7 @@ void sendMessage(const void *msg) {
void receiveMavlink() {
uint8_t buf[MAVLINK_MAX_PACKET_LEN];
int len = receiveWiFi(buf, MAVLINK_MAX_PACKET_LEN);
if (len) mavlinkConnected = true;
// New packet, parse it
mavlink_message_t msg;
@@ -99,11 +104,10 @@ void handleMavlink(const void *_msg) {
if (m.target && m.target != SYSTEM_ID) return; // 0 is broadcast
controlThrottle = m.z / 1000.0f;
controlPitch = m.x / 1000.0f * mavlinkControlScale;
controlRoll = m.y / 1000.0f * mavlinkControlScale;
controlYaw = m.r / 1000.0f * mavlinkControlScale;
controlMode = 1; // STAB mode
controlArmed = 1; // armed
controlPitch = m.x / 1000.0f;
controlRoll = m.y / 1000.0f;
controlYaw = m.r / 1000.0f;
controlMode = NAN;
controlTime = t;
if (abs(controlYaw) < MAVLINK_CONTROL_YAW_DEAD_ZONE) controlYaw = 0;
@@ -174,24 +178,73 @@ void handleMavlink(const void *_msg) {
doCommand(data, true);
}
if (msg.msgid == MAVLINK_MSG_ID_SET_ATTITUDE_TARGET) {
if (mode != AUTO) return;
mavlink_set_attitude_target_t m;
mavlink_msg_set_attitude_target_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
// copy attitude, rates and thrust targets
ratesTarget.x = m.body_roll_rate;
ratesTarget.y = -m.body_pitch_rate; // convert to flu
ratesTarget.z = -m.body_yaw_rate;
attitudeTarget.w = m.q[0];
attitudeTarget.x = m.q[1];
attitudeTarget.y = -m.q[2];
attitudeTarget.z = -m.q[3];
thrustTarget = m.thrust;
ratesExtra = Vector(0, 0, 0);
if (m.type_mask & ATTITUDE_TARGET_TYPEMASK_ATTITUDE_IGNORE) attitudeTarget.invalidate();
armed = m.thrust > 0;
}
if (msg.msgid == MAVLINK_MSG_ID_SET_ACTUATOR_CONTROL_TARGET) {
if (mode != AUTO) return;
mavlink_set_actuator_control_target_t m;
mavlink_msg_set_actuator_control_target_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
attitudeTarget.invalidate();
ratesTarget.invalidate();
torqueTarget.invalidate();
memcpy(motors, m.controls, sizeof(motors)); // copy motor thrusts
armed = motors[0] > 0 || motors[1] > 0 || motors[2] > 0 || motors[3] > 0;
}
// Handle commands
if (msg.msgid == MAVLINK_MSG_ID_COMMAND_LONG) {
mavlink_command_long_t m;
mavlink_msg_command_long_decode(&msg, &m);
if (m.target_system && m.target_system != SYSTEM_ID) return;
mavlink_message_t ack;
mavlink_message_t response;
bool accepted = false;
if (m.command == MAV_CMD_REQUEST_MESSAGE && m.param1 == MAVLINK_MSG_ID_AUTOPILOT_VERSION) {
mavlink_msg_command_ack_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &ack, m.command, MAV_RESULT_ACCEPTED, UINT8_MAX, 0, msg.sysid, msg.compid);
sendMessage(&ack);
accepted = true;
mavlink_msg_autopilot_version_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &response,
MAV_PROTOCOL_CAPABILITY_PARAM_FLOAT | MAV_PROTOCOL_CAPABILITY_MAVLINK2, 1, 0, 1, 1, 0, 0, 0, 0, 0, 0, 0);
sendMessage(&response);
} else {
mavlink_msg_command_ack_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &ack, m.command, MAV_RESULT_UNSUPPORTED, UINT8_MAX, 0, msg.sysid, msg.compid);
sendMessage(&ack);
}
if (m.command == MAV_CMD_COMPONENT_ARM_DISARM) {
if (m.param1 && controlThrottle > 0.05) return; // don't arm if throttle is not low
accepted = true;
armed = m.param1 == 1;
}
if (m.command == MAV_CMD_DO_SET_MODE) {
if (m.param2 < 0 || m.param2 > AUTO) return; // incorrect mode
accepted = true;
mode = m.param2;
}
// send command ack
mavlink_message_t ack;
mavlink_msg_command_ack_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &ack, m.command, accepted ? MAV_RESULT_ACCEPTED : MAV_RESULT_UNSUPPORTED, UINT8_MAX, 0, msg.sysid, msg.compid);
sendMessage(&ack);
}
}

View File

@@ -25,30 +25,32 @@ const int MOTOR_FRONT_LEFT = 3;
void setupMotors() {
print("Setup Motors\n");
// configure pins
#ifdef ESP32
ledcAttach(MOTOR_0_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
ledcAttach(MOTOR_1_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
ledcAttach(MOTOR_2_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
ledcAttach(MOTOR_3_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
#else
analogWriteResolution(PWM_RESOLUTION);
analogWriteFrequency(PWM_FREQUENCY);
#endif
sendMotors();
print("Motors initialized\n");
}
int getDutyCycle(float value) {
value = constrain(value, 0, 1);
float pwm = mapff(value, 0, 1, PWM_MIN, PWM_MAX);
float pwm = mapf(value, 0, 1, PWM_MIN, PWM_MAX);
if (value == 0) pwm = PWM_STOP;
float duty = mapff(pwm, 0, 1000000 / PWM_FREQUENCY, 0, (1 << PWM_RESOLUTION) - 1);
float duty = mapf(pwm, 0, 1000000 / PWM_FREQUENCY, 0, (1 << PWM_RESOLUTION) - 1);
return round(duty);
}
void sendMotors() {
ledcWrite(MOTOR_0_PIN, getDutyCycle(motors[0]));
ledcWrite(MOTOR_1_PIN, getDutyCycle(motors[1]));
ledcWrite(MOTOR_2_PIN, getDutyCycle(motors[2]));
ledcWrite(MOTOR_3_PIN, getDutyCycle(motors[3]));
analogWrite(MOTOR_0_PIN, getDutyCycle(motors[0]));
analogWrite(MOTOR_1_PIN, getDutyCycle(motors[1]));
analogWrite(MOTOR_2_PIN, getDutyCycle(motors[2]));
analogWrite(MOTOR_3_PIN, getDutyCycle(motors[3]));
}
bool motorsActive() {

View File

@@ -8,7 +8,6 @@
extern float channelZero[16];
extern float channelMax[16];
extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
extern float mavlinkControlScale;
Preferences storage;
@@ -70,12 +69,7 @@ Parameter parameters[] = {
{"RC_PITCH", &pitchChannel},
{"RC_THROTTLE", &throttleChannel},
{"RC_YAW", &yawChannel},
{"RC_ARMED", &armedChannel},
{"RC_MODE", &modeChannel},
#if WIFI_ENABLED
// MAVLink
{"MAV_CTRL_SCALE", &mavlinkControlScale},
#endif
};
void setupParameters() {
@@ -124,7 +118,7 @@ bool setParameter(const char *name, const float value) {
}
void syncParameters() {
static double lastSync = 0;
static float lastSync = 0;
if (t - lastSync < 1) return; // sync once per second
if (motorsActive()) return; // don't use flash while flying, it may cause a delay
lastSync = t;

View File

@@ -9,40 +9,44 @@
class PID {
public:
float p = 0;
float i = 0;
float d = 0;
float windup = 0;
float p, i, d;
float windup;
float dtMax;
float derivative = 0;
float integral = 0;
LowPassFilter<float> lpf; // low pass filter for derivative term
PID(float p, float i, float d, float windup = 0, float dAlpha = 1) : p(p), i(i), d(d), windup(windup), lpf(dAlpha) {};
PID(float p, float i, float d, float windup = 0, float dAlpha = 1, float dtMax = 0.1) :
p(p), i(i), d(d), windup(windup), lpf(dAlpha), dtMax(dtMax) {}
float update(float error, float dt) {
integral += error * dt;
float update(float error) {
float dt = t - prevTime;
if (isfinite(prevError) && dt > 0) {
// calculate derivative if both dt and prevError are valid
derivative = (error - prevError) / dt;
// apply low pass filter to derivative
derivative = lpf.update(derivative);
if (dt > 0 && dt < dtMax) {
integral += error * dt;
derivative = lpf.update((error - prevError) / dt); // compute derivative and apply low-pass filter
} else {
integral = 0;
derivative = 0;
}
prevError = error;
prevTime = t;
return p * error + constrain(i * integral, -windup, windup) + d * derivative; // PID
}
void reset() {
prevError = NAN;
prevTime = NAN;
integral = 0;
derivative = 0;
lpf.reset();
}
private:
float prevError = NAN;
float prevTime = NAN;
};

View File

@@ -45,7 +45,7 @@ public:
cx * cy * sz - sx * sy * cz);
}
static Quaternion fromBetweenVectors(Vector u, Vector v) {
static Quaternion fromBetweenVectors(const Vector& u, const Vector& v) {
float dot = u.x * v.x + u.y * v.y + u.z * v.z;
float w1 = u.y * v.z - u.z * v.y;
float w2 = u.z * v.x - u.x * v.z;
@@ -64,6 +64,22 @@ public:
return isfinite(w) && isfinite(x) && isfinite(y) && isfinite(z);
}
bool valid() const {
return finite();
}
bool invalid() const {
return !valid();
}
void invalidate() {
w = NAN;
x = NAN;
y = NAN;
z = NAN;
}
float norm() const {
return sqrt(w * w + x * x + y * y + z * z);
}
@@ -116,29 +132,31 @@ public:
return euler;
}
float getRoll() const {
return toEuler().x;
}
float getPitch() const {
return toEuler().y;
}
float getYaw() const {
// https://github.com/ros/geometry2/blob/589caf083cae9d8fae7effdb910454b4681b9ec1/tf2/include/tf2/impl/utils.h#L122
float yaw;
float sqx = x * x;
float sqy = y * y;
float sqz = z * z;
float sqw = w * w;
double sarg = -2 * (x * z - w * y) / (sqx + sqy + sqz + sqw);
if (sarg <= -0.99999) {
yaw = -2 * atan2(y, x);
} else if (sarg >= 0.99999) {
yaw = 2 * atan2(y, x);
} else {
yaw = atan2(2 * (x * y + w * z), sqw + sqx - sqy - sqz);
}
return yaw;
return toEuler().z;
}
void setRoll(float roll) {
Vector euler = toEuler();
*this = Quaternion::fromEuler(Vector(roll, euler.y, euler.z));
}
void setPitch(float pitch) {
Vector euler = toEuler();
*this = Quaternion::fromEuler(Vector(euler.x, pitch, euler.z));
}
void setYaw(float yaw) {
// TODO: optimize?
Vector euler = toEuler();
euler.z = yaw;
(*this) = Quaternion::fromEuler(euler);
*this = Quaternion::fromEuler(Vector(euler.x, euler.y, yaw));
}
Quaternion operator * (const Quaternion& q) const {

View File

@@ -6,24 +6,24 @@
#include <SBUS.h>
#include "util.h"
SBUS RC(Serial2); // NOTE: Use RC(Serial2, 16, 17) if you use the old UART2 pins
SBUS rc(Serial2); // NOTE: Use RC(Serial2, 16, 17) if you use the old UART2 pins
uint16_t channels[16]; // raw rc channels
double controlTime; // time of the last controls update
float controlTime; // time of the last controls update
float channelZero[16]; // calibration zero values
float channelMax[16]; // calibration max values
// Channels mapping (using float to store in parameters):
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, armedChannel = NAN, modeChannel = NAN;
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
void setupRC() {
print("Setup RC\n");
RC.begin();
rc.begin();
}
bool readRC() {
if (RC.read()) {
SBUSData data = RC.data();
if (rc.read()) {
SBUSData data = rc.data();
for (int i = 0; i < 16; i++) channels[i] = data.ch[i]; // copy channels data
normalizeRC();
controlTime = t;
@@ -42,7 +42,6 @@ void normalizeRC() {
controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : NAN;
controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : NAN;
controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : NAN;
controlArmed = armedChannel >= 0 ? controls[(int)armedChannel] : 1; // assume armed by default
controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN;
}
@@ -50,16 +49,15 @@ void calibrateRC() {
uint16_t zero[16];
uint16_t center[16];
uint16_t max[16];
print("1/9 Calibrating RC: put all switches to default positions [3 sec]\n");
print("1/8 Calibrating RC: put all switches to default positions [3 sec]\n");
pause(3);
calibrateRCChannel(NULL, zero, zero, "2/9 Move sticks [3 sec]\n... ...\n... .o.\n.o. ...\n");
calibrateRCChannel(NULL, center, center, "3/9 Move sticks [3 sec]\n... ...\n.o. .o.\n... ...\n");
calibrateRCChannel(&throttleChannel, zero, max, "4/9 Move sticks [3 sec]\n.o. ...\n... .o.\n... ...\n");
calibrateRCChannel(&yawChannel, center, max, "5/9 Move sticks [3 sec]\n... ...\n..o .o.\n... ...\n");
calibrateRCChannel(&pitchChannel, zero, max, "6/9 Move sticks [3 sec]\n... .o.\n... ...\n.o. ...\n");
calibrateRCChannel(&rollChannel, zero, max, "7/9 Move sticks [3 sec]\n... ...\n... ..o\n.o. ...\n");
calibrateRCChannel(&armedChannel, zero, max, "8/9 Switch to armed [3 sec]\n");
calibrateRCChannel(&modeChannel, zero, max, "9/9 Disarm and switch mode to max [3 sec]\n");
calibrateRCChannel(NULL, zero, zero, "2/8 Move sticks [3 sec]\n... ...\n... .o.\n.o. ...\n");
calibrateRCChannel(NULL, center, center, "3/8 Move sticks [3 sec]\n... ...\n.o. .o.\n... ...\n");
calibrateRCChannel(&throttleChannel, zero, max, "4/8 Move sticks [3 sec]\n.o. ...\n... .o.\n... ...\n");
calibrateRCChannel(&yawChannel, center, max, "5/8 Move sticks [3 sec]\n... ...\n..o .o.\n... ...\n");
calibrateRCChannel(&pitchChannel, zero, max, "6/8 Move sticks [3 sec]\n... .o.\n... ...\n.o. ...\n");
calibrateRCChannel(&rollChannel, zero, max, "7/8 Move sticks [3 sec]\n... ...\n... ..o\n.o. ...\n");
calibrateRCChannel(&modeChannel, zero, max, "8/8 Put mode switch to max [3 sec]\n");
printRCCalibration();
}
@@ -94,6 +92,5 @@ void printRCCalibration() {
print("Pitch %-7g%-7g%-7g\n", pitchChannel, pitchChannel >= 0 ? channelZero[(int)pitchChannel] : NAN, pitchChannel >= 0 ? channelMax[(int)pitchChannel] : NAN);
print("Yaw %-7g%-7g%-7g\n", yawChannel, yawChannel >= 0 ? channelZero[(int)yawChannel] : NAN, yawChannel >= 0 ? channelMax[(int)yawChannel] : NAN);
print("Throttle %-7g%-7g%-7g\n", throttleChannel, throttleChannel >= 0 ? channelZero[(int)throttleChannel] : NAN, throttleChannel >= 0 ? channelMax[(int)throttleChannel] : NAN);
print("Armed %-7g%-7g%-7g\n", armedChannel, armedChannel >= 0 ? channelZero[(int)armedChannel] : NAN, armedChannel >= 0 ? channelMax[(int)armedChannel] : NAN);
print("Mode %-7g%-7g%-7g\n", modeChannel, modeChannel >= 0 ? channelZero[(int)modeChannel] : NAN, modeChannel >= 0 ? channelMax[(int)modeChannel] : NAN);
}

48
flix/safety.ino Normal file
View File

@@ -0,0 +1,48 @@
// Copyright (c) 2024 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Fail-safe functions
#define RC_LOSS_TIMEOUT 1
#define DESCEND_TIME 10
extern float controlTime;
extern float controlRoll, controlPitch, controlThrottle, controlYaw;
void failsafe() {
rcLossFailsafe();
autoFailsafe();
}
// RC loss failsafe
void rcLossFailsafe() {
if (controlTime == 0) return; // no RC at all
if (!armed) return;
if (t - controlTime > RC_LOSS_TIMEOUT) {
descend();
}
}
// Smooth descend on RC lost
void descend() {
mode = AUTO;
attitudeTarget = Quaternion();
thrustTarget -= dt / DESCEND_TIME;
if (thrustTarget < 0) {
thrustTarget = 0;
armed = false;
}
}
// Allow pilot to interrupt automatic flight
void autoFailsafe() {
static float roll, pitch, yaw, throttle;
if (roll != controlRoll || pitch != controlPitch || yaw != controlYaw || abs(throttle - controlThrottle) > 0.05) {
// controls changed
if (mode == AUTO) mode = STAB; // regain control by the pilot
}
roll = controlRoll;
pitch = controlPitch;
yaw = controlYaw;
throttle = controlThrottle;
}

View File

@@ -6,7 +6,7 @@
float loopRate; // Hz
void step() {
double now = micros() / 1000000.0;
float now = micros() / 1000000.0;
dt = now - t;
t = now;
@@ -18,7 +18,7 @@ void step() {
}
void computeLoopRate() {
static double windowStart = 0;
static float windowStart = 0;
static uint32_t rate = 0;
rate++;
if (t - windowStart >= 1) { // 1 second window

View File

@@ -6,17 +6,24 @@
#pragma once
#include <math.h>
#ifdef ESP32
#include <soc/soc.h>
#include <soc/rtc_cntl_reg.h>
#endif
const float ONE_G = 9.80665;
extern float t;
float mapf(long x, long in_min, long in_max, float out_min, float out_max) {
return (float)(x - in_min) * (out_max - out_min) / (float)(in_max - in_min) + out_min;
float mapf(float x, float in_min, float in_max, float out_min, float out_max) {
return (x - in_min) * (out_max - out_min) / (in_max - in_min) + out_min;
}
float mapff(float x, float in_min, float in_max, float out_min, float out_max) {
return (x - in_min) * (out_max - out_min) / (in_max - in_min) + out_min;
bool invalid(float x) {
return !isfinite(x);
}
bool valid(float x) {
return isfinite(x);
}
// Wrap angle to [-PI, PI)
@@ -32,7 +39,9 @@ float wrapAngle(float angle) {
// Disable reset on low voltage
void disableBrownOut() {
#ifdef ESP32
REG_CLR_BIT(RTC_CNTL_BROWN_OUT_REG, RTC_CNTL_BROWN_OUT_ENA);
#endif
}
// Trim and split string by spaces
@@ -44,3 +53,23 @@ void splitString(String& str, String& token0, String& token1, String& token2) {
token1 = strtok(NULL, " "); // String(NULL) creates empty string
token2 = strtok(NULL, "");
}
// Delay filter for boolean signals - ensures the signal is on for at least 'delay' seconds
class Delay {
public:
float delay;
float start = NAN;
Delay(float delay) : delay(delay) {}
bool update(bool on) {
if (!on) {
start = NAN;
return false;
}
if (isnan(start)) {
start = t;
}
return t - start >= delay;
}
};

View File

@@ -21,6 +21,21 @@ public:
return isfinite(x) && isfinite(y) && isfinite(z);
}
bool valid() const {
return finite();
}
bool invalid() const {
return !valid();
}
void invalidate() {
x = NAN;
y = NAN;
z = NAN;
}
float norm() const {
return sqrt(x * x + y * y + z * z);
}

View File

@@ -13,6 +13,7 @@
#define WIFI_PASSWORD "flixwifi"
#define WIFI_UDP_PORT 14550
#define WIFI_UDP_REMOTE_PORT 14550
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
WiFiUDP udp;
@@ -24,7 +25,7 @@ void setupWiFi() {
void sendWiFi(const uint8_t *buf, int len) {
if (WiFi.softAPIP() == IPAddress(0, 0, 0, 0) && WiFi.status() != WL_CONNECTED) return;
udp.beginPacket(WiFi.softAPBroadcastIP(), WIFI_UDP_REMOTE_PORT);
udp.beginPacket(udp.remoteIP() ? udp.remoteIP() : WIFI_UDP_REMOTE_ADDR, WIFI_UDP_REMOTE_PORT);
udp.write(buf, len);
udp.endPacket();
}

View File

@@ -1,7 +1,7 @@
cmake_minimum_required(VERSION 3.5 FATAL_ERROR)
project(flix_gazebo)
# === gazebo plugin
# Gazebo plugin
find_package(gazebo REQUIRED)
find_package(SDL2 REQUIRED)
include_directories(${GAZEBO_INCLUDE_DIRS})

View File

@@ -4,7 +4,7 @@
## Building and running
See [building and running instructions](../docs/build.md#simulation).
See [building and running instructions](../docs/usage.md#simulation).
## Code structure

View File

@@ -12,10 +12,11 @@
#define WIFI_ENABLED 1
double t = NAN;
float t = NAN;
float dt;
float motors[4];
float controlRoll, controlPitch, controlYaw, controlThrottle, controlArmed, controlMode;
float controlRoll, controlPitch, controlYaw, controlThrottle = NAN;
float controlMode = NAN;
Vector acc;
Vector gyro;
Vector rates;
@@ -28,9 +29,9 @@ void computeLoopRate();
void applyGyro();
void applyAcc();
void control();
void interpretRC();
void interpretControls();
void controlAttitude();
void controlRate();
void controlRates();
void controlTorque();
const char* getModeName();
void sendMotors();
@@ -54,9 +55,9 @@ void mavlinkPrint(const char* str);
void sendMavlinkPrint();
inline Quaternion fluToFrd(const Quaternion &q);
void failsafe();
void armingFailsafe();
void rcLossFailsafe();
void descend();
void autoFailsafe();
int parametersCount();
const char *getParameterName(int index);
float getParameter(int index);

View File

@@ -21,7 +21,7 @@
#include "cli.ino"
#include "control.ino"
#include "estimate.ino"
#include "failsafe.ino"
#include "safety.ino"
#include "log.ino"
#include "lpf.h"
#include "mavlink.ino"
@@ -59,6 +59,7 @@ public:
void OnReset() {
attitude = Quaternion(); // reset estimated attitude
armed = false;
__resetTime += __micros;
gzmsg << "Flix plugin reset" << endl;
}

View File

@@ -13,6 +13,7 @@
#define WIFI_UDP_PORT 14580
#define WIFI_UDP_REMOTE_PORT 14550
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
int wifiSocket;
@@ -35,7 +36,7 @@ void sendWiFi(const uint8_t *buf, int len) {
if (wifiSocket == 0) setupWiFi();
sockaddr_in addr; // remote address
addr.sin_family = AF_INET;
addr.sin_addr.s_addr = INADDR_BROADCAST; // send UDP broadcast
addr.sin_addr.s_addr = inet_addr(WIFI_UDP_REMOTE_ADDR);
addr.sin_port = htons(WIFI_UDP_REMOTE_PORT);
sendto(wifiSocket, buf, len, 0, (sockaddr *)&addr, sizeof(addr));
}

View File

@@ -49,6 +49,8 @@ for configuration in props['configurations']:
print('Check configuration', configuration['name'])
for include_path in configuration.get('includePath', []):
if include_path.startswith('/opt/') or include_path.startswith('/usr/'): # don't check non-Arduino libs
continue
check_path(include_path)
for forced_include in configuration.get('forcedInclude', []):

View File

@@ -59,6 +59,13 @@ flix.on('disconnected', lambda: print('Disconnected from Flix'))
flix.on('print', lambda text: print(f'Flix says: {text}'))
```
Unsubscribe from events using `off` method:
```python
flix.off('print') # unsubscribe from print events
flix.off(callback) # unsubscribe specific callback
```
You can also wait for specific events using `wait` method. This method returns the data associated with the event:
```python
@@ -66,13 +73,14 @@ gyro = flix.wait('gyro') # wait for gyroscope update
attitude = flix.wait('attitude', timeout=3) # wait for attitude update, raise TimeoutError after 3 seconds
```
The `value` argument specifies a condition for filtering events. It can be either an expected value or a callable:
The second argument (`value`) specifies a condition for filtering events. It can be either an expected value or a callable:
```python
flix.wait('armed', value=True) # wait until armed
flix.wait('armed', value=False) # wait until disarmed
flix.wait('motors', value=lambda motors: not any(motors)) # wait until all motors stop
flix.wait('attitude_euler', value=lambda att: att[0] > 0) # wait until roll angle is positive
flix.wait('armed', True) # wait until armed
flix.wait('armed', False) # wait until disarmed
flix.wait('mode', 'AUTO') # wait until flight mode is switched to AUTO
flix.wait('motors', lambda motors: not any(motors)) # wait until all motors stop
flix.wait('attitude_euler', lambda att: att[0] > 0) # wait until roll angle is positive
```
Full list of events:
@@ -107,7 +115,7 @@ Get and set firmware parameters using `get_param` and `set_param` methods:
```python
pitch_p = flix.get_param('PITCH_P') # get parameter value
flix.set_param('PITCH_P', 5) # set parameter value
flix.set_param('PITCH_P', 5) # set parameter value
```
Execute CLI commands using `cli` method. This method returns command response:
@@ -121,21 +129,65 @@ flix.cli('reboot') # reboot the drone
> [!TIP]
> Use `help` command to get the list of available commands.
You can arm and disarm the drone using `set_armed` method (warning: the drone will fall if disarmed in the air):
```python
flix.set_armed(True) # arm the drone
flix.set_armed(False) # disarm the drone
```
You can imitate pilot's controls using `set_controls` method:
```python
flix.set_controls(roll=0, pitch=0, yaw=0, throttle=0.6)
```
> [!WARNING]
> This method **is not intended for automatic flights**, only for adding support for a custom pilot input device.
### Automatic flight
The flight control feature is in development. List of methods intended for automatic flight control:
To perform automatic flight, switch the mode to *AUTO*, either from the remote control, or from the code:
* `set_position`
* `set_velocity`
* `set_attitude`
* `set_rates`
* `set_motors`
* `set_controls`
* `set_mode`
```python
flix.set_mode('AUTO')
```
In this mode you can set flight control targets. Setting attitude target:
```python
flix.set_attitude([0.1, 0.2, 0.3], 0.6) # set target roll, pitch, yaw and thrust
flix.set_attitude([1, 0, 0, 0], 0.6) # set target attitude quaternion and thrust
```
Setting angular rates target:
```python
flix.set_rates([0.1, 0.2, 0.3], 0.6) # set target roll rate, pitch rate, yaw rate and thrust
```
You also can control raw motors outputs directly:
```python
flix.set_motors([0.5, 0.5, 0.5, 0.5]) # set motors outputs in range [0, 1]
```
In *AUTO* mode, the drone will arm automatically if the thrust is greater than zero, and disarm if thrust is zero. Therefore, to disarm the drone, set thrust to zero:
```python
flix.set_attitude([0, 0, 0], 0) # disarm the drone
```
The following methods are in development and are not functional yet:
* `set_position` — set target position.
* `set_velocity` — set target velocity.
To exit from *AUTO* mode move control sticks and the drone will switch to *STAB* mode.
## Usage alongside QGroundControl
You can use the Flix library alongside the QGroundControl app, using a proxy mode. To do that:
You can use the Flix library alongside the QGroundControl app, using proxy mode. To do that:
1. Run proxy for `pyflix` and QGroundControl in background:
@@ -151,6 +203,8 @@ You can use the Flix library alongside the QGroundControl app, using a proxy mod
* *Port*: 14560
4. Restart QGroundControl.
<img src="../../docs/img/qgc-proxy.png" width="300">
Now you can run `pyflix` scripts and QGroundControl simultaneously.
## Tools
@@ -201,11 +255,11 @@ You can send values from the firmware like this (`mavlink.ino`):
```cpp
// Send float named value
mavlink_msg_named_value_float_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, t, "some_value", loopRate);
mavlink_msg_named_value_float_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, t, "loop_rate", loopRate);
sendMessage(&msg);
// Send vector named value
mavlink_msg_debug_vect_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, "some_vector", t, gyroBias.x, gyroBias.y, gyroBias.z);
mavlink_msg_debug_vect_pack(SYSTEM_ID, MAV_COMP_ID_AUTOPILOT1, &msg, "gyro_bias", t, gyroBias.x, gyroBias.y, gyroBias.z);
sendMessage(&msg);
```

View File

@@ -6,7 +6,7 @@
import os
import time
from queue import Queue, Empty
from typing import Literal, Optional, Callable, List, Dict, Any, Union
from typing import Optional, Callable, List, Dict, Any, Union, Sequence
import logging
import errno
from threading import Thread, Timer
@@ -36,10 +36,11 @@ class Flix:
system_id: int
messages: Dict[str, Dict[str, Any]] # MAVLink messages storage
values: Dict[Union[str, int], Union[float, List[float]]] = {} # named values
values: Dict[Union[str, int], Union[float, List[float]]] # named values
_connection_timeout = 3
_print_buffer: str = ''
_modes = ['MANUAL', 'ACRO', 'STAB', 'AUTO']
def __init__(self, system_id: int=1, wait_connection: bool=True):
if not (0 <= system_id < 256):
@@ -55,12 +56,11 @@ class Flix:
if e.errno != errno.EADDRINUSE:
raise
# Port busy - using proxy
logger.debug('Listening on port 14560 (proxy)')
logger.debug('Listening on port 14555 (proxy)')
self.connection: mavutil.mavfile = mavutil.mavlink_connection('udpin:0.0.0.0:14555', source_system=254) # type: ignore
self.connection.target_system = system_id
self.mavlink: mavlink.MAVLink = self.connection.mav
self._event_listeners: Dict[str, List[Callable[..., Any]]] = {}
self.messages = {}
self._disconnected_timer = Timer(0, self._disconnected)
self._reader_thread = Thread(target=self._read_mavlink, daemon=True)
self._reader_thread.start()
@@ -78,6 +78,8 @@ class Flix:
self.motors = [0, 0, 0, 0]
self.acc = [0, 0, 0]
self.gyro = [0, 0, 0]
self.messages = {}
self.values = {}
def on(self, event: str, callback: Callable):
event = event.lower()
@@ -85,10 +87,15 @@ class Flix:
self._event_listeners[event] = []
self._event_listeners[event].append(callback)
def off(self, callback: Callable):
for event in self._event_listeners:
if callback in self._event_listeners[event]:
self._event_listeners[event].remove(callback)
def off(self, event_or_callback: Union[str, Callable]):
if isinstance(event_or_callback, str):
event = event_or_callback.lower()
if event in self._event_listeners:
del self._event_listeners[event]
else:
for event in self._event_listeners:
if event_or_callback in self._event_listeners[event]:
self._event_listeners[event].remove(event_or_callback)
def _trigger(self, event: str, *args):
event = event.lower()
@@ -147,7 +154,7 @@ class Flix:
def _handle_mavlink_message(self, msg: mavlink.MAVLink_message):
if isinstance(msg, mavlink.MAVLink_heartbeat_message):
self.mode = ['MANUAL', 'ACRO', 'STAB', 'USER'][msg.custom_mode]
self.mode = self._modes[msg.custom_mode] if msg.custom_mode < len(self._modes) else f'UNKNOWN({msg.custom_mode})'
self.armed = msg.base_mode & mavlink.MAV_MODE_FLAG_SAFETY_ARMED != 0
self._trigger('mode', self.mode)
self._trigger('armed', self.armed)
@@ -168,6 +175,11 @@ class Flix:
msg.chan5_raw, msg.chan6_raw, msg.chan7_raw, msg.chan8_raw]
self._trigger('channels', self.channels)
if isinstance(msg, mavlink.MAVLink_actuator_control_target_message):
self.motors = msg.controls[:4] # type: ignore
self._trigger('motors', self.motors)
# TODO: to be removed: the old way of passing motor outputs
if isinstance(msg, mavlink.MAVLink_actuator_output_status_message):
self.motors = msg.actuator[:4] # type: ignore
self._trigger('motors', self.motors)
@@ -231,6 +243,19 @@ class Flix:
def _flu_to_mavlink(v: List[float]) -> List[float]:
return Flix._mavlink_to_flu(v)
def _command_send(self, command: int, params: Sequence[float]):
if len(params) != 7:
raise ValueError('Command must have 7 parameters')
for attempt in range(3):
try:
logger.debug(f'Send command {command} with params {params} (attempt #{attempt + 1})')
self.mavlink.command_long_send(self.system_id, 0, command, 0, *params) # type: ignore
self.wait('mavlink.COMMAND_ACK', value=lambda msg: msg.command == command and msg.result == mavlink.MAV_RESULT_ACCEPTED, timeout=0.1)
return
except TimeoutError:
continue
raise RuntimeError(f'Failed to send command {command} after 3 attempts')
def _connected(self):
# Reset disconnection timer
self._disconnected_timer.cancel()
@@ -275,6 +300,14 @@ class Flix:
continue
raise RuntimeError(f'Failed to set parameter {name} to {value} after 3 attempts')
def set_mode(self, mode: Union[str, int]):
if isinstance(mode, str):
mode = self._modes.index(mode.upper())
self._command_send(mavlink.MAV_CMD_DO_SET_MODE, (0, mode, 0, 0, 0, 0, 0))
def set_armed(self, armed: bool):
self._command_send(mavlink.MAV_CMD_COMPONENT_ARM_DISARM, (1 if armed else 0, 0, 0, 0, 0, 0, 0))
def set_position(self, position: List[float], yaw: Optional[float] = None, wait: bool = False, tolerance: float = 0.1):
raise NotImplementedError('Position control is not implemented yet')
@@ -282,17 +315,37 @@ class Flix:
raise NotImplementedError('Velocity control is not implemented yet')
def set_attitude(self, attitude: List[float], thrust: float):
raise NotImplementedError('Automatic flight is not implemented yet')
if len(attitude) == 3:
attitude = Quaternion([attitude[0], attitude[1], attitude[2]]).q # type: ignore
elif len(attitude) != 4:
raise ValueError('Attitude must be [roll, pitch, yaw] or [w, x, y, z] quaternion')
if not (0 <= thrust <= 1):
raise ValueError('Thrust must be in range [0, 1]')
attitude = self._flu_to_mavlink(attitude)
for _ in range(2): # duplicate to ensure delivery
self.mavlink.set_attitude_target_send(0, self.system_id, 0, 0,
[attitude[0], attitude[1], attitude[2], attitude[3]],
0, 0, 0, thrust)
def set_rates(self, rates: List[float], thrust: float):
raise NotImplementedError('Automatic flight is not implemented yet')
if len(rates) != 3:
raise ValueError('Rates must be [roll_rate, pitch_rate, yaw_rate]')
if not (0 <= thrust <= 1):
raise ValueError('Thrust must be in range [0, 1]')
rates = self._flu_to_mavlink(rates)
for _ in range(2): # duplicate to ensure delivery
self.mavlink.set_attitude_target_send(0, self.system_id, 0,
mavlink.ATTITUDE_TARGET_TYPEMASK_ATTITUDE_IGNORE,
[1, 0, 0, 0],
rates[0], rates[1], rates[2], thrust)
def set_motors(self, motors: List[float]):
if len(motors) != 4:
raise ValueError('motors must have 4 values')
if not all(0 <= m <= 1 for m in motors):
raise ValueError('motors must be in range [0, 1]')
raise NotImplementedError
for _ in range(2): # duplicate to ensure delivery
self.mavlink.set_actuator_control_target_send(int(time.time() * 1000000), 0, self.system_id, 0, motors + [0] * 4) # type: ignore
def set_controls(self, roll: float, pitch: float, yaw: float, throttle: float):
"""Send pilot's controls. Warning: not intended for automatic control"""
@@ -300,10 +353,7 @@ class Flix:
raise ValueError('roll, pitch, yaw must be in range [-1, 1]')
if not 0 <= throttle <= 1:
raise ValueError('throttle must be in range [0, 1]')
self.mavlink.manual_control_send(self.system_id, roll * 1000, pitch * 1000, yaw * 1000, throttle * 1000, 0) # type: ignore
def set_mode(self, mode: Literal['MANUAL', 'ACRO', 'STAB', 'USER']):
raise NotImplementedError('Setting mode is not implemented yet')
self.mavlink.manual_control_send(self.system_id, int(pitch * 1000), int(roll * 1000), int(throttle * 1000), int(yaw * 1000), 0) # type: ignore
def cli(self, cmd: str, wait_response: bool = True) -> str:
cmd = cmd.strip()
@@ -320,7 +370,9 @@ class Flix:
self.mavlink.serial_control_send(0, 0, 0, 0, len(cmd_bytes), cmd_bytes)
if not wait_response:
return ''
response = self.wait('print_full', timeout=0.1, value=lambda text: text.startswith(response_prefix))
timeout = 0.1
if cmd == 'log': timeout = 10 # log download may take more time
response = self.wait('print_full', timeout=timeout, value=lambda text: text.startswith(response_prefix))
return response[len(response_prefix):].strip()
except TimeoutError:
continue

View File

@@ -24,13 +24,16 @@ def main():
if addr in TARGETS: # packet from target
if source_addr is None:
continue
sock.sendto(data, source_addr)
try:
sock.sendto(data, source_addr)
packets += 1
except: pass
else: # packet from source
source_addr = addr
for target in TARGETS:
sock.sendto(data, target)
packets += 1
packets += 1
print(f'\rPackets: {packets}', end='')
if __name__ == '__main__':

View File

@@ -1,6 +1,6 @@
[project]
name = "pyflix"
version = "0.5"
version = "0.9"
description = "Python API for Flix drone"
authors = [{ name="Oleg Kalachev", email="okalachev@gmail.com" }]
license = "MIT"