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19 Commits
wifi-confi
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54
.vscode/c_cpp_properties.json
vendored
54
.vscode/c_cpp_properties.json
vendored
@@ -6,19 +6,18 @@
|
||||
"${workspaceFolder}/flix",
|
||||
"${workspaceFolder}/gazebo",
|
||||
"${workspaceFolder}/tools/**",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
|
||||
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/**",
|
||||
"~/.arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.3.6/libraries/**",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32",
|
||||
"~/.arduino15/packages/esp32/tools/esp32-libs/3.3.6/include/**",
|
||||
"~/Arduino/libraries/**",
|
||||
"/usr/include/gazebo-11/",
|
||||
"/usr/include/ignition/math6/"
|
||||
],
|
||||
"forcedInclude": [
|
||||
"${workspaceFolder}/.vscode/intellisense.h",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32/Arduino.h",
|
||||
"~/.arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32/pins_arduino.h",
|
||||
"${workspaceFolder}/flix/cli.ino",
|
||||
"${workspaceFolder}/flix/control.ino",
|
||||
"${workspaceFolder}/flix/estimate.ino",
|
||||
@@ -31,9 +30,10 @@
|
||||
"${workspaceFolder}/flix/rc.ino",
|
||||
"${workspaceFolder}/flix/time.ino",
|
||||
"${workspaceFolder}/flix/wifi.ino",
|
||||
"${workspaceFolder}/flix/parameters.ino"
|
||||
"${workspaceFolder}/flix/parameters.ino",
|
||||
"${workspaceFolder}/flix/safety.ino"
|
||||
],
|
||||
"compilerPath": "~/.arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++",
|
||||
"compilerPath": "~/.arduino15/packages/esp32/tools/esp-x32/2511/bin/xtensa-esp32-elf-g++",
|
||||
"cStandard": "c11",
|
||||
"cppStandard": "c++17",
|
||||
"defines": [
|
||||
@@ -53,19 +53,18 @@
|
||||
"name": "Mac",
|
||||
"includePath": [
|
||||
"${workspaceFolder}/flix",
|
||||
"~/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",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.6/libraries/**",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32",
|
||||
"~/Library/Arduino15/packages/esp32/tools/esp32-libs/3.3.6/include/**",
|
||||
"~/Documents/Arduino/libraries/**",
|
||||
"/opt/homebrew/include/gazebo-11/",
|
||||
"/opt/homebrew/include/ignition/math6/"
|
||||
],
|
||||
"forcedInclude": [
|
||||
"${workspaceFolder}/.vscode/intellisense.h",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32/Arduino.h",
|
||||
"~/Library/Arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32/pins_arduino.h",
|
||||
"${workspaceFolder}/flix/flix.ino",
|
||||
"${workspaceFolder}/flix/cli.ino",
|
||||
"${workspaceFolder}/flix/control.ino",
|
||||
@@ -78,9 +77,10 @@
|
||||
"${workspaceFolder}/flix/rc.ino",
|
||||
"${workspaceFolder}/flix/time.ino",
|
||||
"${workspaceFolder}/flix/wifi.ino",
|
||||
"${workspaceFolder}/flix/parameters.ino"
|
||||
"${workspaceFolder}/flix/parameters.ino",
|
||||
"${workspaceFolder}/flix/safety.ino"
|
||||
],
|
||||
"compilerPath": "~/Library/Arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++",
|
||||
"compilerPath": "~/Library/Arduino15/packages/esp32/tools/esp-x32/2511/bin/xtensa-esp32-elf-g++",
|
||||
"cStandard": "c11",
|
||||
"cppStandard": "c++17",
|
||||
"defines": [
|
||||
@@ -103,17 +103,16 @@
|
||||
"${workspaceFolder}/flix",
|
||||
"${workspaceFolder}/gazebo",
|
||||
"${workspaceFolder}/tools/**",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/libraries/**",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/**",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/tools/esp32-arduino-libs/idf-release_v5.4-2f7dcd86-v1/esp32/dio_qspi/include",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.6/libraries/**",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/tools/esp32-libs/3.3.6/include/**",
|
||||
"~/Documents/Arduino/libraries/**"
|
||||
],
|
||||
"forcedInclude": [
|
||||
"${workspaceFolder}/.vscode/intellisense.h",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/cores/esp32/Arduino.h",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.2.0/variants/d1_mini32/pins_arduino.h",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.6/cores/esp32/Arduino.h",
|
||||
"~/AppData/Local/Arduino15/packages/esp32/hardware/esp32/3.3.6/variants/d1_mini32/pins_arduino.h",
|
||||
"${workspaceFolder}/flix/cli.ino",
|
||||
"${workspaceFolder}/flix/control.ino",
|
||||
"${workspaceFolder}/flix/estimate.ino",
|
||||
@@ -126,9 +125,10 @@
|
||||
"${workspaceFolder}/flix/rc.ino",
|
||||
"${workspaceFolder}/flix/time.ino",
|
||||
"${workspaceFolder}/flix/wifi.ino",
|
||||
"${workspaceFolder}/flix/parameters.ino"
|
||||
"${workspaceFolder}/flix/parameters.ino",
|
||||
"${workspaceFolder}/flix/safety.ino"
|
||||
],
|
||||
"compilerPath": "~/AppData/Local/Arduino15/packages/esp32/tools/esp-x32/2411/bin/xtensa-esp32-elf-g++.exe",
|
||||
"compilerPath": "~/AppData/Local/Arduino15/packages/esp32/tools/esp-x32/2511/bin/xtensa-esp32-elf-g++.exe",
|
||||
"cStandard": "c11",
|
||||
"cppStandard": "c++17",
|
||||
"defines": [
|
||||
|
||||
4
Makefile
4
Makefile
@@ -13,10 +13,10 @@ monitor:
|
||||
|
||||
dependencies .dependencies:
|
||||
arduino-cli core update-index --config-file arduino-cli.yaml
|
||||
arduino-cli core install esp32:esp32@3.2.0 --config-file arduino-cli.yaml
|
||||
arduino-cli core install esp32:esp32@3.3.6 --config-file arduino-cli.yaml
|
||||
arduino-cli lib update-index
|
||||
arduino-cli lib install "FlixPeriph"
|
||||
arduino-cli lib install "MAVLink"@2.0.16
|
||||
arduino-cli lib install "MAVLink"@2.0.25
|
||||
touch .dependencies
|
||||
|
||||
gazebo/build cmake: gazebo/CMakeLists.txt
|
||||
|
||||
@@ -138,10 +138,10 @@ You can see a user-contributed [variant of complete circuit diagram](https://mir
|
||||
|
||||
|Motor|Position|Direction|Prop type|Motor wires|GPIO|
|
||||
|-|-|-|-|-|-|
|
||||
|Motor 0|Rear left|Counter-clockwise|B|Black & White|GPIO12 (*TDI*)|
|
||||
|Motor 1|Rear right|Clockwise|A|Blue & Red|GPIO13 (*TCK*)|
|
||||
|Motor 2|Front right|Counter-clockwise|B|Black & White|GPIO14 (*TMS*)|
|
||||
|Motor 3|Front left|Clockwise|A|Blue & Red|GPIO15 (*TD0*)|
|
||||
|Motor 0|Rear left|Counter-clockwise|B|Black & White|GPIO12 *(TDI)*|
|
||||
|Motor 1|Rear right|Clockwise|A|Blue & Red|GPIO13 *(TCK)*|
|
||||
|Motor 2|Front right|Counter-clockwise|B|Black & White|GPIO14 *(TMS)*|
|
||||
|Motor 3|Front left|Clockwise|A|Blue & Red|GPIO15 *(TD0)*|
|
||||
|
||||
Clockwise motors have blue & red wires and correspond to propeller type A (marked on the propeller).
|
||||
Counter-clockwise motors have black & white wires correspond to propeller type B.
|
||||
|
||||
@@ -41,10 +41,10 @@ Motors connection table:
|
||||
|
||||
|Motor|Position|Direction|Prop type|Motor wires|GPIO|
|
||||
|-|-|-|-|-|-|
|
||||
|Motor 0|Rear left|Counter-clockwise|B|Black & White|GPIO12 (*TDI*)|
|
||||
|Motor 1|Rear right|Clockwise|A|Blue & Red|GPIO13 (*TCK*)|
|
||||
|Motor 2|Front right|Counter-clockwise|B|Black & White|GPIO14 (*TMS*)|
|
||||
|Motor 3|Front left|Clockwise|A|Blue & Red|GPIO15 (*TD0*)|
|
||||
|Motor 0|Rear left|Counter-clockwise|B|Black & White|GPIO12 *(TDI)*|
|
||||
|Motor 1|Rear right|Clockwise|A|Blue & Red|GPIO13 *(TCK)*|
|
||||
|Motor 2|Front right|Counter-clockwise|B|Black & White|GPIO14 *(TMS)*|
|
||||
|Motor 3|Front left|Clockwise|A|Blue & Red|GPIO15 *(TD0)*|
|
||||
|
||||
## Motors tightening
|
||||
|
||||
|
||||
@@ -110,7 +110,7 @@ float angle = Vector::angleBetween(a, b); // 1.57 (90 градусов)
|
||||
|
||||
#### Скалярное произведение
|
||||
|
||||
Скалярное произведение векторов (*dot product*) — это произведение длин двух векторов на косинус угла между ними. В математике оно обозначается знаком `·` или слитным написанием векторов. Интуитивно, результат скалярного произведения показывает, насколько два вектора *сонаправлены*.
|
||||
Скалярное произведение векторов *(dot product)* — это произведение длин двух векторов на косинус угла между ними. В математике оно обозначается знаком `·` или слитным написанием векторов. Интуитивно, результат скалярного произведения показывает, насколько два вектора *сонаправлены*.
|
||||
|
||||
В Flix используется статический метод `Vector::dot()`:
|
||||
|
||||
@@ -124,7 +124,7 @@ float dotProduct = Vector::dot(a, b); // 32
|
||||
|
||||
#### Векторное произведение
|
||||
|
||||
Векторное произведение (*cross product*) позволяет найти вектор, перпендикулярный двум другим векторам. В математике оно обозначается знаком `×`, а в прошивке используется статический метод `Vector::cross()`:
|
||||
Векторное произведение *(cross product)* позволяет найти вектор, перпендикулярный двум другим векторам. В математике оно обозначается знаком `×`, а в прошивке используется статический метод `Vector::cross()`:
|
||||
|
||||
```cpp
|
||||
Vector a(1, 2, 3);
|
||||
@@ -144,9 +144,9 @@ Vector crossProduct = Vector::cross(a, b); // -3, 6, -3
|
||||
|
||||
В прошивке углы Эйлера сохраняются в обычный объект `Vector` (хоть и, строго говоря, не являются вектором):
|
||||
|
||||
* Угол по крену (*roll*) — `vector.x`.
|
||||
* Угол по тангажу (*pitch*) — `vector.y`.
|
||||
* Угол по рысканию (*yaw*) — `vector.z`.
|
||||
* Угол по крену *(roll)* — `vector.x`.
|
||||
* Угол по тангажу *(pitch)* — `vector.y`.
|
||||
* Угол по рысканию *(yaw)* — `vector.z`.
|
||||
|
||||
Особенности углов Эйлера:
|
||||
|
||||
@@ -162,8 +162,8 @@ Vector crossProduct = Vector::cross(a, b); // -3, 6, -3
|
||||
|
||||
Помимо углов Эйлера, любую ориентацию в трехмерном пространстве можно представить в виде вращения вокруг некоторой оси на некоторый угол. В геометрии это доказывается, как **теорема вращения Эйлера**. В таком представлении ориентация задается двумя величинами:
|
||||
|
||||
* **Ось вращения** (*axis*) — единичный вектор, определяющий ось вращения.
|
||||
* **Угол поворота** (*angle* или *θ*) — угол, на который нужно повернуть объект вокруг этой оси.
|
||||
* **Ось вращения** *(axis)* — единичный вектор, определяющий ось вращения.
|
||||
* **Угол поворота** *(angle* или *θ)* — угол, на который нужно повернуть объект вокруг этой оси.
|
||||
|
||||
В Flix ось вращения задается объектом `Vector`, а угол поворота — числом типа `float` в радианах:
|
||||
|
||||
@@ -177,7 +177,7 @@ float angle = radians(45);
|
||||
|
||||
### Вектор вращения
|
||||
|
||||
Если умножить вектор *axis* на угол поворота *θ*, то получится **вектор вращения** (*rotation vector*). Этот вектор играет важную роль в алгоритмах управления ориентацией летательного аппарата.
|
||||
Если умножить вектор *axis* на угол поворота *θ*, то получится **вектор вращения** *(rotation vector)*. Этот вектор играет важную роль в алгоритмах управления ориентацией летательного аппарата.
|
||||
|
||||
Вектор вращения обладает замечательным свойством: если угловые скорости объекта (в собственной системе координат) в каждый момент времени совпадают с компонентами этого вектора, то за единичное время объект придет к заданной этим вектором ориентации. Это свойство позволяет использовать вектор вращения для управления ориентацией объекта посредством управления угловыми скоростями.
|
||||
|
||||
@@ -198,7 +198,7 @@ Vector rotation = radians(45) * Vector(1, 2, 3);
|
||||
<a href="https://github.com/okalachev/flix/blob/master/flix/quaternion.h"><code>quaternion.h</code></a>.<br>
|
||||
</div>
|
||||
|
||||
Вектор вращения удобен, но еще удобнее использовать **кватернион**. В Flix кватернионы задаются объектами `Quaternion` из библиотеки `quaternion.h`. Кватернион состоит из четырех значений: *w*, *x*, *y*, *z* и рассчитывается из вектора оси вращения (*axis*) и угла поворота (*θ*) по формуле:
|
||||
Вектор вращения удобен, но еще удобнее использовать **кватернион**. В Flix кватернионы задаются объектами `Quaternion` из библиотеки `quaternion.h`. Кватернион состоит из четырех значений: *w*, *x*, *y*, *z* и рассчитывается из вектора оси вращения *(axis)* и угла поворота *(θ)* по формуле:
|
||||
|
||||
\\[ q = \left( \begin{array}{c} w \\\\ x \\\\ y \\\\ z \end{array} \right) = \left( \begin{array}{c} \cos\left(\frac{\theta}{2}\right) \\\\ axis\_x \cdot \sin\left(\frac{\theta}{2}\right) \\\\ axis\_y \cdot \sin\left(\frac{\theta}{2}\right) \\\\ axis\_z \cdot \sin\left(\frac{\theta}{2}\right) \end{array} \right) \\]
|
||||
|
||||
|
||||
@@ -177,7 +177,7 @@ imu.setDLPF(imu.DLPF_MAX);
|
||||
|
||||
## Калибровка гироскопа
|
||||
|
||||
Как и любое измерительное устройство, гироскоп вносит искажения в измерения. Наиболее простая модель этих искажений делит их на статические смещения (*bias*) и случайный шум (*noise*):
|
||||
Как и любое измерительное устройство, гироскоп вносит искажения в измерения. Наиболее простая модель этих искажений делит их на статические смещения *(bias)* и случайный шум *(noise)*:
|
||||
|
||||
\\[ gyro_{xyz}=rates_{xyz}+bias_{xyz}+noise \\]
|
||||
|
||||
|
||||
BIN
docs/img/user/arkymatsekh/1.jpg
Normal file
BIN
docs/img/user/arkymatsekh/1.jpg
Normal file
Binary file not shown.
|
After Width: | Height: | Size: 62 KiB |
BIN
docs/img/user/arkymatsekh/2.jpg
Normal file
BIN
docs/img/user/arkymatsekh/2.jpg
Normal file
Binary file not shown.
|
After Width: | Height: | Size: 48 KiB |
BIN
docs/img/user/arkymatsekh/3.jpg
Normal file
BIN
docs/img/user/arkymatsekh/3.jpg
Normal file
Binary file not shown.
|
After Width: | Height: | Size: 50 KiB |
BIN
docs/img/user/arkymatsekh/video.jpg
Normal file
BIN
docs/img/user/arkymatsekh/video.jpg
Normal file
Binary file not shown.
|
After Width: | Height: | Size: 17 KiB |
@@ -13,10 +13,10 @@ Do the following:
|
||||
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 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 startup output.
|
||||
* **Check the baudrate is correct**. If you see garbage characters in the Serial Monitor, make sure the baudrate is set to 115200.
|
||||
* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
|
||||
* **Check if the 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*).
|
||||
* **Check if the console is working**. Perform `help` command in Serial Monitor. You should see the list of available commands. You can also access the console using QGroundControl *(Vehicle Setup* ⇒ *Analyze Tools* ⇒ *MAVLink Console)*.
|
||||
* **Configure QGroundControl correctly before connecting to the drone** if you use it to control the drone. Go to the settings and enable *Virtual Joystick*. *Auto-Center Throttle* setting **should be disabled**.
|
||||
* **If QGroundControl doesn't connect**, you might need to disable the firewall and/or VPN on your computer.
|
||||
* **Check the IMU is working**. Perform `imu` command and check its output:
|
||||
|
||||
@@ -20,10 +20,10 @@ You can build and upload the firmware using either **Arduino IDE** (easier for b
|
||||
|
||||
1. Install [Arduino IDE](https://www.arduino.cc/en/software) (version 2 is recommended).
|
||||
2. *Windows users might need to install [USB to UART bridge driver from Silicon Labs](https://www.silabs.com/developers/usb-to-uart-bridge-vcp-drivers).*
|
||||
3. Install ESP32 core, version 3.2.0. 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.
|
||||
3. Install ESP32 core, version 3.3.6. See the [official Espressif's instructions](https://docs.espressif.com/projects/arduino-esp32/en/latest/installing.html#installing-using-arduino-ide) on installing ESP32 Core in Arduino IDE.
|
||||
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.
|
||||
* `MAVLink`, version 2.0.25.
|
||||
5. Open the `flix/flix.ino` sketch from downloaded firmware sources in Arduino IDE.
|
||||
6. Connect your ESP32 board to the computer and choose correct board type in Arduino IDE (*WEMOS D1 MINI ESP32* for ESP32 Mini) and the port.
|
||||
7. [Build and upload](https://docs.arduino.cc/software/ide-v2/tutorials/getting-started/ide-v2-uploading-a-sketch) the firmware using Arduino IDE.
|
||||
@@ -108,7 +108,7 @@ The drone is configured using parameters. To access and modify them, go to the Q
|
||||
|
||||
<img src="img/parameters.png" width="400">
|
||||
|
||||
You can also work with parameters using `p` command in the console.
|
||||
You can also work with parameters using `p` command in the console. Parameter names are case-insensitive.
|
||||
|
||||
### Define IMU orientation
|
||||
|
||||
@@ -134,6 +134,20 @@ Before flight you need to calibrate the accelerometer:
|
||||
1. Access the console using QGroundControl (recommended) or Serial Monitor.
|
||||
2. Type `ca` command there and follow the instructions.
|
||||
|
||||
### Setup motors
|
||||
|
||||
If using non-default motor pins, set the pin numbers using the parameters: `MOTOR_PIN_FL`, `MOTOR_PIN_FR`, `MOTOR_PIN_RL`, `MOTOR_PIN_RR` (front-left, front-right, rear-left, rear-right respectively).
|
||||
|
||||
If using brushless motors and ESCs:
|
||||
|
||||
1. Set the appropriate PWM using the parameters: `MOT_PWM_STOP`, `MOT_PWM_MIN`, and `MOT_PWM_MAX` (1000, 1000, and 2000 is typical).
|
||||
2. Decrease the PWM frequency using the `MOT_PWM_FREQ` parameter (400 is typical).
|
||||
|
||||
Reboot the drone to apply the changes.
|
||||
|
||||
> [!CAUTION]
|
||||
> **Remove the props when configuring the motors!** If improperly configured, you may not be able to stop them.
|
||||
|
||||
### Check everything works
|
||||
|
||||
1. Check the IMU is working: perform `imu` command and check its output:
|
||||
@@ -250,8 +264,8 @@ You can configure the Wi-Fi using parameters and console commands.
|
||||
The Wi-Fi mode is chosen using `WIFI_MODE` parameter in QGroundControl or in the console:
|
||||
|
||||
* `0` — Wi-Fi is disabled.
|
||||
* `1` — Access Point mode (*AP*) — the drone creates a Wi-Fi network.
|
||||
* `2` — Client mode (*STA*) — the drone connects to an existing Wi-Fi network.
|
||||
* `1` — Access Point mode *(AP)* — the drone creates a Wi-Fi network.
|
||||
* `2` — Client mode *(STA)* — the drone connects to an existing Wi-Fi network.
|
||||
* `3` — *ESP-NOW (not implemented yet)*.
|
||||
|
||||
> [!WARNING]
|
||||
@@ -271,6 +285,12 @@ ap my-flix-ssid mypassword123
|
||||
p WIFI_MODE 1
|
||||
```
|
||||
|
||||
Disabling Wi-Fi:
|
||||
|
||||
```
|
||||
p WIFI_MODE 0
|
||||
```
|
||||
|
||||
## Flight log
|
||||
|
||||
After the flight, you can download the flight log for analysis wirelessly. Use the following command on your computer for that:
|
||||
|
||||
11
docs/user.md
11
docs/user.md
@@ -4,6 +4,17 @@ This page contains user-built drones based on the Flix project. Publish your pro
|
||||
|
||||
---
|
||||
|
||||
Author: **Arkadiy "Arky" Matsekh**, Foucault Dynamics, Gold Coast, Australia.<br>
|
||||
The drone was built for the University of Queensland industry-led Master's capstone project.
|
||||
|
||||
**Flight video:**
|
||||
|
||||
<a href="https://drive.google.com/file/d/1NNYSVXBY-w0JjCo07D8-PgnVq3ca9plj/view?usp=sharing"><img height=300 src="img/user/arkymatsekh/video.jpg"></a>
|
||||
|
||||
<img src="img/user/arkymatsekh/1.jpg" height=150> <img src="img/user/arkymatsekh/2.jpg" height=150> <img src="img/user/arkymatsekh/3.jpg" height=150>
|
||||
|
||||
---
|
||||
|
||||
Author: [goldarte](https://t.me/goldarte).<br>
|
||||
|
||||
<img src="img/user/goldarte/1.jpg" height=150> <img src="img/user/goldarte/2.jpg" height=150>
|
||||
|
||||
@@ -6,6 +6,7 @@
|
||||
#include "pid.h"
|
||||
#include "vector.h"
|
||||
#include "util.h"
|
||||
#include "lpf.h"
|
||||
|
||||
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
|
||||
extern const int RAW, ACRO, STAB, AUTO;
|
||||
@@ -14,6 +15,7 @@ extern uint16_t channels[16];
|
||||
extern float controlTime;
|
||||
extern int mode;
|
||||
extern bool armed;
|
||||
extern LowPassFilter<Vector> gyroBiasFilter;
|
||||
|
||||
const char* motd =
|
||||
"\nWelcome to\n"
|
||||
@@ -44,6 +46,7 @@ const char* motd =
|
||||
"log [dump] - print log header [and data]\n"
|
||||
"cr - calibrate RC\n"
|
||||
"ca - calibrate accel\n"
|
||||
"cl - calibrate level\n"
|
||||
"mfr, mfl, mrr, mrl - test motor (remove props)\n"
|
||||
"sys - show system info\n"
|
||||
"reset - reset drone's state\n"
|
||||
@@ -92,7 +95,7 @@ void doCommand(String str, bool echo = false) {
|
||||
} else if (command == "p") {
|
||||
bool success = setParameter(arg0.c_str(), arg1.toFloat());
|
||||
if (success) {
|
||||
print("%s = %g\n", arg0.c_str(), arg1.toFloat());
|
||||
print("%s = %g\n", arg0.c_str(), getParameter(arg0.c_str()));
|
||||
} else {
|
||||
print("Parameter not found: %s\n", arg0.c_str());
|
||||
}
|
||||
@@ -149,6 +152,8 @@ void doCommand(String str, bool echo = false) {
|
||||
calibrateRC();
|
||||
} else if (command == "ca") {
|
||||
calibrateAccel();
|
||||
} else if (command == "cl") {
|
||||
calibrateLevel();
|
||||
} else if (command == "mfr") {
|
||||
testMotor(MOTOR_FRONT_RIGHT);
|
||||
} else if (command == "mfl") {
|
||||
@@ -178,6 +183,7 @@ void doCommand(String str, bool echo = false) {
|
||||
#endif
|
||||
} else if (command == "reset") {
|
||||
attitude = Quaternion();
|
||||
gyroBiasFilter.reset();
|
||||
} else if (command == "reboot") {
|
||||
ESP.restart();
|
||||
} else {
|
||||
|
||||
@@ -52,6 +52,7 @@ PID pitchPID(PITCH_P, PITCH_I, PITCH_D);
|
||||
PID yawPID(YAW_P, 0, 0);
|
||||
Vector maxRate(ROLLRATE_MAX, PITCHRATE_MAX, YAWRATE_MAX);
|
||||
float tiltMax = TILT_MAX;
|
||||
int flightModes[] = {STAB, STAB, STAB}; // map for rc mode switch
|
||||
|
||||
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
|
||||
@@ -65,9 +66,9 @@ void control() {
|
||||
}
|
||||
|
||||
void interpretControls() {
|
||||
if (controlMode < 0.25) mode = STAB;
|
||||
if (controlMode < 0.75) mode = STAB;
|
||||
if (controlMode > 0.75) mode = STAB;
|
||||
if (controlMode < 0.25) mode = flightModes[0];
|
||||
else if (controlMode < 0.75) mode = flightModes[1];
|
||||
else if (controlMode > 0.75) mode = flightModes[2];
|
||||
|
||||
if (mode == AUTO) return; // pilot is not effective in AUTO mode
|
||||
|
||||
|
||||
@@ -7,7 +7,6 @@
|
||||
#include "quaternion.h"
|
||||
#include "util.h"
|
||||
|
||||
|
||||
extern float t, dt;
|
||||
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
|
||||
extern Vector gyro, acc;
|
||||
|
||||
12
flix/imu.ino
12
flix/imu.ino
@@ -19,6 +19,8 @@ Vector acc; // accelerometer output, m/s/s
|
||||
Vector accBias;
|
||||
Vector accScale(1, 1, 1);
|
||||
|
||||
LowPassFilter<Vector> gyroBiasFilter(0.001);
|
||||
|
||||
void setupIMU() {
|
||||
print("Setup IMU\n");
|
||||
imu.begin();
|
||||
@@ -50,8 +52,6 @@ void readIMU() {
|
||||
void calibrateGyroOnce() {
|
||||
static Delay landedDelay(2);
|
||||
if (!landedDelay.update(landed)) return; // calibrate only if definitely stationary
|
||||
|
||||
static LowPassFilter<Vector> gyroBiasFilter(0.001);
|
||||
gyroBias = gyroBiasFilter.update(gyro);
|
||||
}
|
||||
|
||||
@@ -110,6 +110,14 @@ void calibrateAccelOnce() {
|
||||
accBias = (accMax + accMin) / 2;
|
||||
}
|
||||
|
||||
void calibrateLevel() {
|
||||
print("Place perfectly level [1 sec]\n");
|
||||
pause(1);
|
||||
Quaternion correction = Quaternion::fromBetweenVectors(Quaternion::rotateVector(Vector(0, 0, 1), attitude), Vector(0, 0, 1));
|
||||
imuRotation = Quaternion::rotate(correction, Quaternion::fromEuler(imuRotation)).toEuler();
|
||||
print("✓ Done: %.3f %.3f %.3f\n", degrees(imuRotation.x), degrees(imuRotation.y), degrees(imuRotation.z));
|
||||
}
|
||||
|
||||
void printIMUCalibration() {
|
||||
print("gyro bias: %f %f %f\n", gyroBias.x, gyroBias.y, gyroBias.z);
|
||||
print("accel bias: %f %f %f\n", accBias.x, accBias.y, accBias.z);
|
||||
|
||||
14
flix/lpf.h
14
flix/lpf.h
@@ -14,15 +14,6 @@ public:
|
||||
LowPassFilter(float alpha): alpha(alpha) {};
|
||||
|
||||
T update(const T input) {
|
||||
if (alpha == 1) { // filter disabled
|
||||
return input;
|
||||
}
|
||||
|
||||
if (!initialized) {
|
||||
output = input;
|
||||
initialized = true;
|
||||
}
|
||||
|
||||
return output += alpha * (input - output);
|
||||
}
|
||||
|
||||
@@ -31,9 +22,6 @@ public:
|
||||
}
|
||||
|
||||
void reset() {
|
||||
initialized = false;
|
||||
output = T(); // set to zero
|
||||
}
|
||||
|
||||
private:
|
||||
bool initialized = false;
|
||||
};
|
||||
|
||||
@@ -142,7 +142,7 @@ void handleMavlink(const void *_msg) {
|
||||
// send ack
|
||||
mavlink_message_t msg;
|
||||
mavlink_msg_param_value_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
|
||||
m.param_id, m.param_value, MAV_PARAM_TYPE_REAL32, parametersCount(), 0); // index is unknown
|
||||
m.param_id, getParameter(name), MAV_PARAM_TYPE_REAL32, parametersCount(), 0); // index is unknown
|
||||
sendMessage(&msg);
|
||||
}
|
||||
|
||||
|
||||
@@ -1,24 +1,19 @@
|
||||
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
|
||||
// Repository: https://github.com/okalachev/flix
|
||||
|
||||
// Motors output control using MOSFETs
|
||||
// In case of using ESCs, change PWM_STOP, PWM_MIN and PWM_MAX to appropriate values in μs, decrease PWM_FREQUENCY (to 400)
|
||||
// PWM control for motors
|
||||
|
||||
#include "util.h"
|
||||
|
||||
#define MOTOR_0_PIN 12 // rear left
|
||||
#define MOTOR_1_PIN 13 // rear right
|
||||
#define MOTOR_2_PIN 14 // front right
|
||||
#define MOTOR_3_PIN 15 // front left
|
||||
|
||||
#define PWM_FREQUENCY 78000
|
||||
#define PWM_RESOLUTION 10
|
||||
#define PWM_STOP 0
|
||||
#define PWM_MIN 0
|
||||
#define PWM_MAX 1000000 / PWM_FREQUENCY
|
||||
|
||||
float motors[4]; // normalized motor thrusts in range [0..1]
|
||||
|
||||
int motorPins[4] = {12, 13, 14, 15}; // default pin numbers
|
||||
int pwmFrequency = 78000;
|
||||
int pwmResolution = 10;
|
||||
int pwmStop = 0;
|
||||
int pwmMin = 0;
|
||||
int pwmMax = -1; // -1 means duty cycle mode
|
||||
|
||||
const int MOTOR_REAR_LEFT = 0;
|
||||
const int MOTOR_REAR_RIGHT = 1;
|
||||
const int MOTOR_FRONT_RIGHT = 2;
|
||||
@@ -26,30 +21,30 @@ const int MOTOR_FRONT_LEFT = 3;
|
||||
|
||||
void setupMotors() {
|
||||
print("Setup Motors\n");
|
||||
|
||||
// configure pins
|
||||
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);
|
||||
|
||||
for (int i = 0; i < 4; i++) {
|
||||
ledcAttach(motorPins[i], pwmFrequency, pwmResolution);
|
||||
}
|
||||
sendMotors();
|
||||
print("Motors initialized\n");
|
||||
}
|
||||
|
||||
int getDutyCycle(float value) {
|
||||
value = constrain(value, 0, 1);
|
||||
float pwm = mapf(value, 0, 1, PWM_MIN, PWM_MAX);
|
||||
if (value == 0) pwm = PWM_STOP;
|
||||
float duty = mapf(pwm, 0, 1000000 / PWM_FREQUENCY, 0, (1 << PWM_RESOLUTION) - 1);
|
||||
return round(duty);
|
||||
void sendMotors() {
|
||||
for (int i = 0; i < 4; i++) {
|
||||
ledcWrite(motorPins[i], getDutyCycle(motors[i]));
|
||||
}
|
||||
}
|
||||
|
||||
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]));
|
||||
int getDutyCycle(float value) {
|
||||
value = constrain(value, 0, 1);
|
||||
if (pwmMax >= 0) { // pwm mode
|
||||
float pwm = mapf(value, 0, 1, pwmMin, pwmMax);
|
||||
if (value == 0) pwm = pwmStop;
|
||||
float duty = mapf(pwm, 0, 1000000 / pwmFrequency, 0, (1 << pwmResolution) - 1);
|
||||
return round(duty);
|
||||
} else { // duty cycle mode
|
||||
return round(value * ((1 << pwmResolution) - 1));
|
||||
}
|
||||
}
|
||||
|
||||
bool motorsActive() {
|
||||
|
||||
@@ -10,6 +10,7 @@ extern float channelZero[16];
|
||||
extern float channelMax[16];
|
||||
extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
|
||||
extern int wifiMode, udpLocalPort, udpRemotePort;
|
||||
extern float rcLossTimeout, descendTime;
|
||||
|
||||
Preferences storage;
|
||||
|
||||
@@ -48,6 +49,9 @@ Parameter parameters[] = {
|
||||
{"CTL_R_RATE_MAX", &maxRate.x},
|
||||
{"CTL_Y_RATE_MAX", &maxRate.z},
|
||||
{"CTL_TILT_MAX", &tiltMax},
|
||||
{"CTL_FLT_MODE_0", &flightModes[0]},
|
||||
{"CTL_FLT_MODE_1", &flightModes[1]},
|
||||
{"CTL_FLT_MODE_2", &flightModes[2]},
|
||||
// imu
|
||||
{"IMU_ROT_ROLL", &imuRotation.x},
|
||||
{"IMU_ROT_PITCH", &imuRotation.y},
|
||||
@@ -58,9 +62,20 @@ Parameter parameters[] = {
|
||||
{"IMU_ACC_SCALE_X", &accScale.x},
|
||||
{"IMU_ACC_SCALE_Y", &accScale.y},
|
||||
{"IMU_ACC_SCALE_Z", &accScale.z},
|
||||
{"IMU_GYRO_BIAS_A", &gyroBiasFilter.alpha},
|
||||
// estimate
|
||||
{"EST_ACC_WEIGHT", &accWeight},
|
||||
{"EST_RATES_LPF_A", &ratesFilter.alpha},
|
||||
// motors
|
||||
{"MOT_PIN_FL", &motorPins[MOTOR_FRONT_LEFT]},
|
||||
{"MOT_PIN_FR", &motorPins[MOTOR_FRONT_RIGHT]},
|
||||
{"MOT_PIN_RL", &motorPins[MOTOR_REAR_LEFT]},
|
||||
{"MOT_PIN_RR", &motorPins[MOTOR_REAR_RIGHT]},
|
||||
{"MOT_PWM_FREQ", &pwmFrequency},
|
||||
{"MOT_PWM_RES", &pwmResolution},
|
||||
{"MOT_PWM_STOP", &pwmStop},
|
||||
{"MOT_PWM_MIN", &pwmMin},
|
||||
{"MOT_PWM_MAX", &pwmMax},
|
||||
// rc
|
||||
{"RC_ZERO_0", &channelZero[0]},
|
||||
{"RC_ZERO_1", &channelZero[1]},
|
||||
@@ -91,6 +106,9 @@ Parameter parameters[] = {
|
||||
{"MAV_SYS_ID", &mavlinkSysId},
|
||||
{"MAV_RATE_SLOW", &telemetrySlow.rate},
|
||||
{"MAV_RATE_FAST", &telemetryFast.rate},
|
||||
// safety
|
||||
{"SF_RC_LOSS_TIME", &rcLossTimeout},
|
||||
{"SF_DESCEND_TIME", &descendTime},
|
||||
};
|
||||
|
||||
void setupParameters() {
|
||||
@@ -121,7 +139,7 @@ float getParameter(int index) {
|
||||
|
||||
float getParameter(const char *name) {
|
||||
for (auto ¶meter : parameters) {
|
||||
if (strcmp(parameter.name, name) == 0) {
|
||||
if (strcasecmp(parameter.name, name) == 0) {
|
||||
return parameter.getValue();
|
||||
}
|
||||
}
|
||||
@@ -130,7 +148,7 @@ float getParameter(const char *name) {
|
||||
|
||||
bool setParameter(const char *name, const float value) {
|
||||
for (auto ¶meter : parameters) {
|
||||
if (strcmp(parameter.name, name) == 0) {
|
||||
if (strcasecmp(parameter.name, name) == 0) {
|
||||
if (parameter.integer && !isfinite(value)) return false; // can't set integer to NaN or Inf
|
||||
parameter.setValue(value);
|
||||
return true;
|
||||
|
||||
@@ -13,10 +13,10 @@ float channelZero[16]; // calibration zero values
|
||||
float channelMax[16]; // calibration max values
|
||||
|
||||
float controlRoll, controlPitch, controlYaw, controlThrottle; // pilot's inputs, range [-1, 1]
|
||||
float controlMode = NAN; //
|
||||
float controlTime; // time of the last controls update (0 when no RC)
|
||||
float controlMode = NAN;
|
||||
float controlTime = NAN; // time of the last controls update
|
||||
|
||||
// Channels mapping (using float to store in parameters):
|
||||
// Channels mapping (nan means not assigned):
|
||||
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
|
||||
|
||||
void setupRC() {
|
||||
|
||||
@@ -3,12 +3,12 @@
|
||||
|
||||
// Fail-safe functions
|
||||
|
||||
#define RC_LOSS_TIMEOUT 1
|
||||
#define DESCEND_TIME 10
|
||||
|
||||
extern float controlTime;
|
||||
extern float controlRoll, controlPitch, controlThrottle, controlYaw;
|
||||
|
||||
float rcLossTimeout = 1;
|
||||
float descendTime = 10;
|
||||
|
||||
void failsafe() {
|
||||
rcLossFailsafe();
|
||||
autoFailsafe();
|
||||
@@ -16,9 +16,8 @@ void failsafe() {
|
||||
|
||||
// RC loss failsafe
|
||||
void rcLossFailsafe() {
|
||||
if (controlTime == 0) return; // no RC at all
|
||||
if (!armed) return;
|
||||
if (t - controlTime > RC_LOSS_TIMEOUT) {
|
||||
if (t - controlTime > rcLossTimeout) {
|
||||
descend();
|
||||
}
|
||||
}
|
||||
@@ -27,7 +26,7 @@ void rcLossFailsafe() {
|
||||
void descend() {
|
||||
mode = AUTO;
|
||||
attitudeTarget = Quaternion();
|
||||
thrustTarget -= dt / DESCEND_TIME;
|
||||
thrustTarget -= dt / descendTime;
|
||||
if (thrustTarget < 0) {
|
||||
thrustTarget = 0;
|
||||
armed = false;
|
||||
|
||||
@@ -1,7 +1,7 @@
|
||||
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
|
||||
// Repository: https://github.com/okalachev/flix
|
||||
|
||||
// Wi-Fi connectivity
|
||||
// Wi-Fi communication
|
||||
|
||||
#include <WiFi.h>
|
||||
#include <WiFiAP.h>
|
||||
|
||||
@@ -9,6 +9,7 @@
|
||||
#include "quaternion.h"
|
||||
#include "Arduino.h"
|
||||
#include "wifi.h"
|
||||
#include "lpf.h"
|
||||
|
||||
extern float t, dt;
|
||||
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
|
||||
@@ -19,6 +20,7 @@ extern float motors[4];
|
||||
|
||||
Vector gyro, acc, imuRotation;
|
||||
Vector accBias, gyroBias, accScale(1, 1, 1);
|
||||
LowPassFilter<Vector> gyroBiasFilter(0);
|
||||
|
||||
// declarations
|
||||
void step();
|
||||
@@ -32,6 +34,7 @@ void controlRates();
|
||||
void controlTorque();
|
||||
const char* getModeName();
|
||||
void sendMotors();
|
||||
int getDutyCycle(float value);
|
||||
bool motorsActive();
|
||||
void testMotor(int n);
|
||||
void print(const char* format, ...);
|
||||
@@ -68,6 +71,7 @@ void resetParameters();
|
||||
void setLED(bool on) {};
|
||||
void calibrateGyro() { print("Skip gyro calibrating\n"); };
|
||||
void calibrateAccel() { print("Skip accel calibrating\n"); };
|
||||
void calibrateLevel() { print("Skip level calibrating\n"); };
|
||||
void printIMUCalibration() { print("cal: N/A\n"); };
|
||||
void printIMUInfo() {};
|
||||
void printWiFiInfo() {};
|
||||
|
||||
@@ -11,9 +11,10 @@
|
||||
#include <sys/poll.h>
|
||||
#include <gazebo/gazebo.hh>
|
||||
|
||||
#define WIFI_UDP_PORT 14580
|
||||
#define WIFI_UDP_REMOTE_PORT 14550
|
||||
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
|
||||
int wifiMode = 1; // mock
|
||||
int udpLocalPort = 14580;
|
||||
int udpRemotePort = 14550;
|
||||
const char *udpRemoteIP = "255.255.255.255";
|
||||
|
||||
int wifiSocket;
|
||||
|
||||
@@ -22,22 +23,22 @@ void setupWiFi() {
|
||||
sockaddr_in addr; // local address
|
||||
addr.sin_family = AF_INET;
|
||||
addr.sin_addr.s_addr = INADDR_ANY;
|
||||
addr.sin_port = htons(WIFI_UDP_PORT);
|
||||
addr.sin_port = htons(udpLocalPort);
|
||||
if (bind(wifiSocket, (sockaddr *)&addr, sizeof(addr))) {
|
||||
gzerr << "Failed to bind WiFi UDP socket on port " << WIFI_UDP_PORT << std::endl;
|
||||
gzerr << "Failed to bind WiFi UDP socket on port " << udpLocalPort << std::endl;
|
||||
return;
|
||||
}
|
||||
int broadcast = 1;
|
||||
setsockopt(wifiSocket, SOL_SOCKET, SO_BROADCAST, &broadcast, sizeof(broadcast)); // enable broadcast
|
||||
gzmsg << "WiFi UDP socket initialized on port " << WIFI_UDP_PORT << " (remote port " << WIFI_UDP_REMOTE_PORT << ")" << std::endl;
|
||||
gzmsg << "WiFi UDP socket initialized on port " << udpLocalPort << " (remote port " << udpRemotePort << ")" << std::endl;
|
||||
}
|
||||
|
||||
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 = inet_addr(WIFI_UDP_REMOTE_ADDR);
|
||||
addr.sin_port = htons(WIFI_UDP_REMOTE_PORT);
|
||||
addr.sin_addr.s_addr = inet_addr(udpRemoteIP);
|
||||
addr.sin_port = htons(udpRemotePort);
|
||||
sendto(wifiSocket, buf, len, 0, (sockaddr *)&addr, sizeof(addr));
|
||||
}
|
||||
|
||||
|
||||
@@ -13,7 +13,7 @@ lines = []
|
||||
|
||||
print('Downloading log...')
|
||||
count = 0
|
||||
dev.write('log\n'.encode())
|
||||
dev.write('log dump\n'.encode())
|
||||
while True:
|
||||
line = dev.readline()
|
||||
if not line:
|
||||
|
||||
@@ -43,6 +43,7 @@ records = [record for record in records if record[0] != 0]
|
||||
|
||||
print(f'Received records: {len(records)}')
|
||||
|
||||
os.makedirs(f'{DIR}/log', exist_ok=True)
|
||||
log = open(f'{DIR}/log/{datetime.datetime.now().isoformat()}.csv', 'wb')
|
||||
log.write(header.encode() + b'\n')
|
||||
for record in records:
|
||||
|
||||
@@ -92,17 +92,17 @@ Full list of events:
|
||||
|-----|-----------|----------------|
|
||||
|`connected`|Connected to the drone||
|
||||
|`disconnected`|Connection is lost||
|
||||
|`armed`|Armed state update|Armed state (*bool*)|
|
||||
|`mode`|Flight mode update|Flight mode (*str*)|
|
||||
|`landed`|Landed state update|Landed state (*bool*)|
|
||||
|`armed`|Armed state update|Armed state *(bool)*|
|
||||
|`mode`|Flight mode update|Flight mode *(str)*|
|
||||
|`landed`|Landed state update|Landed state *(bool)*|
|
||||
|`print`|The drone prints text to the console|Text|
|
||||
|`attitude`|Attitude update|Attitude quaternion (*list*)|
|
||||
|`attitude_euler`|Attitude update|Euler angles (*list*)|
|
||||
|`rates`|Angular rates update|Angular rates (*list*)|
|
||||
|`channels`|Raw RC channels update|Raw RC channels (*list*)|
|
||||
|`motors`|Motor outputs update|Motor outputs (*list*)|
|
||||
|`acc`|Accelerometer update|Accelerometer output (*list*)|
|
||||
|`gyro`|Gyroscope update|Gyroscope output (*list*)|
|
||||
|`attitude`|Attitude update|Attitude quaternion *(list)*|
|
||||
|`attitude_euler`|Attitude update|Euler angles *(list)*|
|
||||
|`rates`|Angular rates update|Angular rates *(list)*|
|
||||
|`channels`|Raw RC channels update|Raw RC channels *(list)*|
|
||||
|`motors`|Motor outputs update|Motor outputs *(list)*|
|
||||
|`acc`|Accelerometer update|Accelerometer output *(list)*|
|
||||
|`gyro`|Gyroscope update|Gyroscope output *(list)*|
|
||||
|`mavlink`|Received MAVLink message|Message object|
|
||||
|`mavlink.<message_name>`|Received specific MAVLink message|Message object|
|
||||
|`mavlink.<message_id>`|Received specific MAVLink message|Message object|
|
||||
@@ -277,7 +277,3 @@ logger = logging.getLogger('flix')
|
||||
logger.setLevel(logging.DEBUG) # be more verbose
|
||||
logger.setLevel(logging.WARNING) # be less verbose
|
||||
```
|
||||
|
||||
## Stability
|
||||
|
||||
The library is in development stage. The API is not stable.
|
||||
|
||||
Reference in New Issue
Block a user