28 Commits
Author SHA1 Message Date
Oleg Kalachev 142cb9af01 Position control draft 2026-08-01 20:13:48 +03:00
Oleg Kalachev 74b082957e Add threshold for rc sticks move for quitting auto mode 2026-07-21 10:58:22 +03:00
Oleg Kalachev 4582942919 Minor docs update 2026-07-21 10:51:50 +03:00
Oleg Kalachev df14a5678f Don't send discovery message if encrypting is disabled in espnow 2026-07-20 19:01:38 +03:00
Oleg Kalachev 81721abf91 Disable log as it may crash the program 2026-07-20 10:16:30 +03:00
Oleg Kalachev 1276d220a6 Add tilt disarm failsafe 2026-07-18 21:35:13 +03:00
Oleg Kalachev 79c7e282cb Fix esp-now proxy 2026-07-18 14:25:19 +03:00
Oleg Kalachev f031cf3046 Fix printing espnow channel number in wifi command 2026-07-18 14:16:33 +03:00
Oleg Kalachev 60f389a289 Fix espnow proxy 2026-07-18 11:35:20 +03:00
Oleg Kalachev 5c24ce113d Minor docs update 2026-07-18 00:45:19 +03:00
Oleg Kalachev b58c2e7c7a Add auto channel search to espnow-proxy 2026-07-18 00:03:18 +03:00
Oleg Kalachev 2137730a8d Make espnow-proxy output more obvious 2026-07-18 00:03:01 +03:00
Oleg Kalachev 309d2d2e29 Add espnow-proxy build to ci 2026-07-17 23:42:28 +03:00
Oleg Kalachev 0c91ccfab5 Use STA interface in ESP-NOW proxy 2026-07-17 23:39:21 +03:00
Oleg Kalachev 26d53d4ce1 Docs fix 2026-07-17 17:18:07 +03:00
Oleg Kalachev 0366b24ff3 Minor docs fix 2026-07-17 17:06:22 +03:00
Oleg Kalachev 3de4e9ab9a Add info on uploading the firmware to ESP32-S3 Super Mini 2026-07-17 17:04:45 +03:00
Oleg Kalachev f1e024b19a Add instructions on how to set pin numbers for imu 2026-07-17 14:13:02 +03:00
Oleg Kalachev d9be26c5be Disable gyro notch filter by default 2026-07-16 23:21:17 +03:00
Oleg Kalachev f8a4cbfee1 Fix in docs 2026-07-16 17:48:16 +03:00
Oleg Kalachev 658040e652 Merge branch 'master' into robolager2026 2026-07-16 16:54:47 +03:00
Oleg Kalachev 70459df8dd Disable swarming in espnow proxy by default 2026-07-16 11:30:10 +03:00
Oleg Kalachev 61213bb8a1 Unset default motor pins (for safety) 2026-07-15 20:19:02 +03:00
Oleg Kalachev 8917849711 Remove unneeded declaration from the sim 2026-07-15 18:40:51 +03:00
Oleg Kalachev 1cdc7a8641 Fix rc in simulator
Virtual rc is disabled if rxRxPin < 0
2026-07-15 18:40:35 +03:00
Oleg Kalachev d64bf24c6d Add alicanerus' build 2026-07-08 22:29:33 +03:00
Oleg Kalachev fabd5e072d Fixes in the docs 2026-07-04 21:40:39 +03:00
Oleg Kalachev 1ae85ff118 Add argument to motor testing commands for specifying thrust 2026-07-02 22:22:33 +03:00
19 changed files with 239 additions and 72 deletions
+1 -1
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@@ -84,7 +84,7 @@ Additional articles:
|*Boost converter (optional, for more stable power supply)*|*5V output*|<img src="docs/img/buck-boost.jpg" width=100>|1| |*Boost converter (optional, for more stable power supply)*|*5V output*|<img src="docs/img/buck-boost.jpg" width=100>|1|
|Motor|8520 3.7V brushed motor.<br>Motor with exact 3.7V voltage is needed, not ranged working voltage (3.7V — 6V).<br>Make sure the motor shaft diameter and propeller hole diameter match!|<img src="docs/img/motor.jpeg" width=100>|4| |Motor|8520 3.7V brushed motor.<br>Motor with exact 3.7V voltage is needed, not ranged working voltage (3.7V — 6V).<br>Make sure the motor shaft diameter and propeller hole diameter match!|<img src="docs/img/motor.jpeg" width=100>|4|
|Propeller|55 mm or 65 mm|<img src="docs/img/prop.jpg" width=100>|4| |Propeller|55 mm or 65 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| |MOSFET (transistor)|UMW 100N03A or [analog](https://t.me/opensourcequadcopter/33).<br>Warning: don't use KIA 100N03A or other manufacturers, they might not work!|<img src="docs/img/100n03a.jpg" width=100>|4|
|Pull-down resistor<br>Voltage measurement resistor|10 kΩ|<img src="docs/img/resistor10k.jpg" width=100>|6| |Pull-down resistor<br>Voltage measurement resistor|10 kΩ|<img src="docs/img/resistor10k.jpg" width=100>|6|
|3.7V Li-Po battery|LW 952540 (or any compatible by the size).<br>Make sure the battery has enough discharge rate — 25C or more!|<img src="docs/img/battery.jpg" width=100>|1| |3.7V Li-Po battery|LW 952540 (or any compatible by the size).<br>Make sure the battery has enough discharge rate — 25C or more!|<img src="docs/img/battery.jpg" width=100>|1|
|Battery connector cable|MX2.0 2P female|<img src="docs/img/mx.png" width=100>|1| |Battery connector cable|MX2.0 2P female|<img src="docs/img/mx.png" width=100>|1|
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+33 -17
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@@ -25,7 +25,7 @@ You can build and upload the firmware using either **Arduino IDE** (easier for b
* `FlixPeriph`, the latest version. * `FlixPeriph`, the latest version.
* `MAVLink`, version 2.0.25. * `MAVLink`, version 2.0.25.
5. Open the `flix/flix.ino` sketch from downloaded firmware sources in Arduino IDE. 5. Open the `flix/flix.ino` sketch from downloaded firmware sources in Arduino IDE.
6. Connect your ESP32 board to the computer and choose correct board type in Arduino IDE (*WEMOS D1 MINI ESP32* for ESP32 Mini) and the port. 6. Connect your ESP32 board to the computer and choose correct board type in Arduino IDE (*WEMOS D1 MINI ESP32* for ESP32 Mini, *ESP32S3 Dev Module* for ESP32-S3 Super Mini) and the port.
7. Set *Tools**Core Debug Level* to *Error* to see the errors in the serial console. Set *Tools**USB CDC on Boot* to *Enabled* for ESP32-S3/ESP32-C3 boards. 7. Set *Tools**Core Debug Level* to *Error* to see the errors in the serial console. Set *Tools**USB CDC on Boot* to *Enabled* for ESP32-S3/ESP32-C3 boards.
8. [Build and upload](https://docs.arduino.cc/software/ide-v2/tutorials/getting-started/ide-v2-uploading-a-sketch) the firmware using Arduino IDE. 8. [Build and upload](https://docs.arduino.cc/software/ide-v2/tutorials/getting-started/ide-v2-uploading-a-sketch) the firmware using Arduino IDE.
@@ -71,6 +71,32 @@ See other available Make commands in [Makefile](../Makefile).
## Before first flight ## Before first flight
### Choose the IMU model
In case if using different IMU model than MPU9250, change `imu` variable declaration in the `imu.ino`:
```cpp
ICM20948 imu(SPI); // For ICM-20948 via SPI
// or
MPU6050 imu(Wire); // For MPU-6050 via I2C
```
If using non-default SPI pins, pass SCK, MISO, and MOSI pin numbers to `SPI.begin` call and SS pin to `imu` constructor like that:
```cpp
ICM20948(SPI, <SS>);
// ...
SPI.begin(<SCK>, <MISO>, <MOSI>);
imu.begin();
```
If using non-default I2C pins, pass SDA and SCL pin numbers to `Wire.setPins` call like that:
```cpp
Wire.begin(<SDA>, <SCL>);
imu.begin();
```
### Connect using QGroundControl ### Connect using QGroundControl
QGroundControl is a ground control station software that can be used to monitor and control the drone. QGroundControl is a ground control station software that can be used to monitor and control the drone.
@@ -96,7 +122,7 @@ To access the console using serial port:
To access the console using QGroundControl: To access the console using QGroundControl:
1. Connect to the drone using QGroundControl app. 1. Connect to the drone using QGroundControl app.
2. Go to the QGroundControl menu ⇒ *Vehicle Setup* ⇒ *Analyze Tools* ⇒ *MAVLink Console*. 2. Go to the QGroundControl menu ⇒ *Analyze Tools* ⇒ *MAVLink Console*.
<img src="img/cli.png" width="400"> <img src="img/cli.png" width="400">
@@ -111,19 +137,6 @@ The drone is configured using parameters. To access and modify them, go to the Q
You can also work with parameters using `p` command in the console. Parameter names are case-insensitive. You can also work with parameters using `p` command in the console. Parameter names are case-insensitive.
### Configure the IMU
1. Configure the following parameters for the used IMU:
* `IMU_MODEL` — IMU model (0 for disabled, 1 for MPU-9250/MPU-6500¹, 2 for ICM-20948, 3 for MPU-6050, 4 for ICM-40609-D).
* `IMU_BUS` — communication bus (0 for SPI, 1 for I²C).
* `IMU_PIN_SCK`, `IMU_PIN_MISO`, `IMU_PIN_MOSI`, `IMU_PIN_CS` — SPI pin numbers.
* `IMU_PIN_SCL`, `IMU_PIN_SDA` — I²C pin numbers.
* `IMU_PIN_INT` — IMU data ready pin number (-1 if not used).
2. Reboot the drone.
3. Check the IMU is working using `imu` command in the console (see details below).
¹ — not to be confused with MPU-6050.
### Define IMU orientation ### Define IMU orientation
The IMU orientation (relative to the drone's axes) is defined using the parameters: `IMU_ROT_ROLL`, `IMU_ROT_PITCH`, and `IMU_ROT_YAW`. The IMU orientation (relative to the drone's axes) is defined using the parameters: `IMU_ROT_ROLL`, `IMU_ROT_PITCH`, and `IMU_ROT_YAW`.
@@ -337,7 +350,7 @@ To setup ESP-NOW communication:
1. Flash the second ESP32 board with ESP-NOW proxy sketch: [`tools/espnow-proxy/espnow-proxy.ino`](../tools/espnow-proxy/espnow-proxy.ino). Use Arduino IDE or command line: `make upload_proxy`. 1. Flash the second ESP32 board with ESP-NOW proxy sketch: [`tools/espnow-proxy/espnow-proxy.ino`](../tools/espnow-proxy/espnow-proxy.ino). Use Arduino IDE or command line: `make upload_proxy`.
2. Open Serial Monitor or use `make monitor` command. The ESP32 will print its MAC address and generated encryption key, for example: 2. Open Serial Monitor in Arduino IDE or use `make monitor` command. The ESP32 will print its MAC address and generated encryption key, for example:
``` ```
espnow 7a:c8:e3:eb:bf:e9 &PiuSysxP9+$L&5E espnow 7a:c8:e3:eb:bf:e9 &PiuSysxP9+$L&5E
@@ -356,7 +369,10 @@ To setup ESP-NOW communication:
* Type: Serial. * Type: Serial.
* Serial Port: choose the port of the proxy ESP32 board, e. g. `/dev/cu.usbserial-0001`. * Serial Port: choose the port of the proxy ESP32 board, e. g. `/dev/cu.usbserial-0001`.
* Baud Rate: 115200. * Baud Rate: 115200.
5. Click *Save*. QGroundControl should connect to the drone using ESP-NOW and begin showing the telemetry. 5. Click *Save*, click *Connect*. QGroundControl should connect to the drone using ESP-NOW and begin showing the telemetry.
> [!TIP]
> Make sure Arduino IDE is not running when using ESP-NOW proxy board, as it may block it.
## Flight log ## Flight log
+9
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@@ -4,6 +4,15 @@ This page contains user-built drones based on the Flix project. Publish your pro
--- ---
Author: Alican Erüst.<br>
Description: QX95 mm frame, 55 mm propellers, 3.7 V 25C 1050 mAh LiPo battery, MPU6050 IMU, Logitech F310 gamepad controller, with a total quadcopter weight of 66 g.
<img src="img/user/alicanerus/1.jpg" height=200> <img src="img/user/alicanerus/2.jpg" height=200> <img src="img/user/alicanerus/3.jpg" height=200>
[Flight video](https://drive.google.com/file/d/1k0WeWTKnCAfaugkX7LcmNxsUuq79RL8Z/view?usp=sharing).
---
Author: [Неруш Михаил](https://t.me/NerushMV).<br> Author: [Неруш Михаил](https://t.me/NerushMV).<br>
Description: custom frame made of 4 mm plywood, 8520 brushed motors, 75 mm propellers, MPU-6500. FlySky FS-i6X with ESP32-based adapter for ESP-NOW communication (using PPM output).<br> Description: custom frame made of 4 mm plywood, 8520 brushed motors, 75 mm propellers, MPU-6500. FlySky FS-i6X with ESP32-based adapter for ESP-NOW communication (using PPM output).<br>
Sources and materials: [link](https://drive.google.com/drive/folders/1uWiDcuorLrtVs_IIR7Y13omij-7Q1nx8). Sources and materials: [link](https://drive.google.com/drive/folders/1uWiDcuorLrtVs_IIR7Y13omij-7Q1nx8).
+8 -6
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@@ -9,7 +9,7 @@
#include "filter.h" #include "filter.h"
extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT; extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern const int RAW, ACRO, STAB, AUTO; extern const int RAW, ACRO, STAB, AUTO, POS;
extern const int W_AP, W_STA, W_ESPNOW; extern const int W_AP, W_STA, W_ESPNOW;
extern float t, dt, loopRate; extern float t, dt, loopRate;
extern uint16_t channels[16]; extern uint16_t channels[16];
@@ -50,8 +50,8 @@ const char* motd =
"sta <ssid> <password> - configure Wi-Fi client mode\n" "sta <ssid> <password> - configure Wi-Fi client mode\n"
"espnow <mac> [<key>] - configure ESP-NOW peer\n" "espnow <mac> [<key>] - configure ESP-NOW peer\n"
"mot - show motor output\n" "mot - show motor output\n"
"mfr/mfl/mrr/mrl [<thrust>] - test motor (remove props)\n"
"log [dump] - print log header [and data]\n" "log [dump] - print log header [and data]\n"
"mfr, mfl, mrr, mrl - test motor (remove props)\n"
"log - show log info\n" "log - show log info\n"
"log header - show log header\n" "log header - show log header\n"
"log reset - reset log\n" "log reset - reset log\n"
@@ -134,6 +134,8 @@ void doCommand(String str, bool echo = false) {
mode = ACRO; mode = ACRO;
} else if (command == "auto") { } else if (command == "auto") {
mode = AUTO; mode = AUTO;
} else if (command == "pos") {
mode = POS;
} else if (command == "rc") { } else if (command == "rc") {
print("channels: "); print("channels: ");
for (int i = 0; i < 16; i++) { for (int i = 0; i < 16; i++) {
@@ -176,13 +178,13 @@ void doCommand(String str, bool echo = false) {
} else if (command == "ca") { } else if (command == "ca") {
calibrateAccel(); calibrateAccel();
} else if (command == "mfr") { } else if (command == "mfr") {
testMotor(MOTOR_FRONT_RIGHT); testMotor(MOTOR_FRONT_RIGHT, arg0.isEmpty() ? 0.2 : arg0.toFloat());
} else if (command == "mfl") { } else if (command == "mfl") {
testMotor(MOTOR_FRONT_LEFT); testMotor(MOTOR_FRONT_LEFT, arg0.isEmpty() ? 0.2 : arg0.toFloat());
} else if (command == "mrr") { } else if (command == "mrr") {
testMotor(MOTOR_REAR_RIGHT); testMotor(MOTOR_REAR_RIGHT, arg0.isEmpty() ? 0.2 : arg0.toFloat());
} else if (command == "mrl") { } else if (command == "mrl") {
testMotor(MOTOR_REAR_LEFT); testMotor(MOTOR_REAR_LEFT, arg0.isEmpty() ? 0.2 : arg0.toFloat());
} else if (command == "sys") { } else if (command == "sys") {
#ifdef ESP32 #ifdef ESP32
print("Chip: %s\n", ESP.getChipModel()); print("Chip: %s\n", ESP.getChipModel());
+14 -2
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@@ -34,7 +34,7 @@
#define TILT_MAX radians(30) #define TILT_MAX radians(30)
#define RATES_D_LPF_ALPHA 0.2 // cutoff frequency ~ 40 Hz #define RATES_D_LPF_ALPHA 0.2 // cutoff frequency ~ 40 Hz
const int RAW = 0, ACRO = 1, STAB = 2, AUTO = 3; // flight modes const int RAW = 0, ACRO = 1, STAB = 2, AUTO = 3, POS = 4;
int mode = STAB; int mode = STAB;
bool armed = false; bool armed = false;
@@ -56,6 +56,7 @@ 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 const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode; extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
extern Vector position, positionTarget;
void control() { void control() {
interpretControls(); interpretControls();
@@ -79,7 +80,18 @@ void interpretControls() {
thrustTarget = controlThrottle; thrustTarget = controlThrottle;
if (mode == STAB) { if (mode == POS) {
if (controlRoll != 0 || controlPitch != 0) {
positionTarget.x = NAN;
positionTarget.y = NAN;
} else if (invalid(positionTarget.x) || invalid(positionTarget.y)) {
// reset position target
positionTarget.x = position.x;
positionTarget.y = position.y;
}
}
if (mode == STAB || (mode == POS && invalid(positionTarget.x))) {
float yawTarget = attitudeTarget.getYaw(); float yawTarget = attitudeTarget.getYaw();
if (!armed || invalid(yawTarget) || controlYaw != 0) yawTarget = attitude.getYaw(); // reset yaw target if (!armed || invalid(yawTarget) || controlYaw != 0) yawTarget = attitude.getYaw(); // reset yaw target
attitudeTarget = Quaternion::fromEuler(Vector(controlRoll * tiltMax, controlPitch * tiltMax, yawTarget)); attitudeTarget = Quaternion::fromEuler(Vector(controlRoll * tiltMax, controlPitch * tiltMax, yawTarget));
+2 -1
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@@ -15,7 +15,7 @@ bool landed;
float accWeight = 0.003; float accWeight = 0.003;
float levelWeight = 0.0002; float levelWeight = 0.0002;
LowPassFilter<Vector> ratesFilter(0.2); // cutoff frequency ~ 40 Hz LowPassFilter<Vector> ratesFilter(0.2); // cutoff frequency ~ 40 Hz
NotchFilter<Vector> ratesNotch(382, 40); NotchFilter<Vector> ratesNotch(382, 0);
void setupEstimate() { void setupEstimate() {
print("Setup estimation\n"); print("Setup estimation\n");
@@ -26,6 +26,7 @@ void estimate() {
applyGyro(); applyGyro();
applyAcc(); applyAcc();
applyLevel(); applyLevel();
estimatePosition();
} }
void applyGyro() { void applyGyro() {
+2 -15
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@@ -4,16 +4,12 @@
// Work with the IMU sensor // Work with the IMU sensor
#include <SPI.h> #include <SPI.h>
#include <Wire.h>
#include <FlixPeriph.h> #include <FlixPeriph.h>
#include "vector.h" #include "vector.h"
#include "filter.h" #include "filter.h"
#include "util.h" #include "util.h"
IMU imu; MPU9250 imu(SPI);
int imuModel = 1, imuBus = 0;
int imuSckPin = SCK, imuMisoPin = MISO, imuMosiPin = MOSI, imuCsPin = -1, imuIntPin = -1;
int imuSdaPin = SDA, imuSclPin = SCL;
Vector imuRotation(0, 0, PI / 2); // imu orientation as Euler angles Vector imuRotation(0, 0, PI / 2); // imu orientation as Euler angles
Vector gyro; // gyroscope output, rad/s Vector gyro; // gyroscope output, rad/s
@@ -27,15 +23,7 @@ LowPassFilter<Vector> gyroBiasFilter(0.001);
void setupIMU() { void setupIMU() {
print("Setup IMU\n"); print("Setup IMU\n");
if (imuBus == 0 && imuCsPin > 0) { imu.begin();
// SPI connection
SPI.begin(imuSckPin, imuMisoPin, imuMosiPin);
imu.begin((IMU::Model)imuModel, SPI, imuCsPin, imuIntPin);
} else if (imuBus == 1) {
// I2C connection
Wire.setPins(imuSdaPin, imuSclPin);
imu.begin((IMU::Model)imuModel, Wire, imuIntPin);
}
configureIMU(); configureIMU();
} }
@@ -137,7 +125,6 @@ void printIMUInfo() {
print("model: %s\n", imu.getModel()); print("model: %s\n", imu.getModel());
print("who am I: 0x%02X\n", imu.whoAmI()); print("who am I: 0x%02X\n", imu.whoAmI());
print("rate: %.0f\n", loopRate); print("rate: %.0f\n", loopRate);
print("interrupt mode: %s\n", imuIntPin != -1 ? "pin" : "timer");
print("temperature: %.1f °C\n", imu.getTemp()); print("temperature: %.1f °C\n", imu.getTemp());
print("gyro: %f %f %f\n", gyro.x, gyro.y, gyro.z); print("gyro: %f %f %f\n", gyro.x, gyro.y, gyro.z);
print("acc: %f %f %f\n", acc.x, acc.y, acc.z); print("acc: %f %f %f\n", acc.x, acc.y, acc.z);
+6 -1
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@@ -6,7 +6,7 @@
#include "vector.h" #include "vector.h"
#include "util.h" #include "util.h"
int logMemory = 0; // 0 - RAM, 1 - PSRAM, -1 - disabled int logMemory = -1; // 0 - RAM, 1 - PSRAM, -1 - disabled
float logUsage = 0.5; // fraction of free memory to use for log float logUsage = 0.5; // fraction of free memory to use for log
struct LogValue { struct LogValue {
@@ -68,6 +68,11 @@ LogTopic logTopics[] = {
{"attitude.pitch", []() { return attitude.getPitch(); }}, {"attitude.pitch", []() { return attitude.getPitch(); }},
{"attitude.yaw", []() { return attitude.getYaw(); }}), {"attitude.yaw", []() { return attitude.getYaw(); }}),
LogTopic(50,
{"position.x", &position.x},
{"position.y", &position.y},
{"position.z", &position.z}),
// rc // rc
LogTopic(10, LogTopic(10,
{"controlTime", &controlTime, false}, // trigger value {"controlTime", &controlTime, false}, // trigger value
+7
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@@ -196,6 +196,13 @@ void handleMavlink(const void *_msg) {
sendMessage(&msg); sendMessage(&msg);
} }
if (msg.msgid == MAVLINK_MSG_ID_VISION_POSITION_ESTIMATE) {
mavlink_vision_position_estimate_t m;
mavlink_msg_vision_position_estimate_decode(&msg, &m);
Vector pos(m.x, m.y, m.z);
correctPosition(pos);
}
if (msg.msgid == MAVLINK_MSG_ID_MISSION_REQUEST_LIST) { // handle to make qgc happy if (msg.msgid == MAVLINK_MSG_ID_MISSION_REQUEST_LIST) { // handle to make qgc happy
mavlink_mission_request_list_t m; mavlink_mission_request_list_t m;
mavlink_msg_mission_request_list_decode(&msg, &m); mavlink_msg_mission_request_list_decode(&msg, &m);
+3 -3
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@@ -7,7 +7,7 @@
float motors[4]; // normalized motor thrusts in range [0..1] float motors[4]; // normalized motor thrusts in range [0..1]
int motorPins[4] = {12, 13, 14, 15}; // default pin numbers int motorPins[4] = {-1, -1, -1, -1}; // default pin numbers
int pwmFrequency = 78000; int pwmFrequency = 78000;
int pwmResolution = 10; int pwmResolution = 10;
int pwmStop = 0; int pwmStop = 0;
@@ -51,9 +51,9 @@ bool motorsActive() {
return motors[0] != 0 || motors[1] != 0 || motors[2] != 0 || motors[3] != 0; return motors[0] != 0 || motors[1] != 0 || motors[2] != 0 || motors[3] != 0;
} }
void testMotor(int n) { void testMotor(int n, float thrust) {
print("Testing motor %d\n", n); print("Testing motor %d\n", n);
motors[n] = 0.2; motors[n] = thrust;
delay(50); // ESP32 may need to wait until the end of the current cycle to change duty https://github.com/espressif/arduino-esp32/issues/5306 delay(50); // ESP32 may need to wait until the end of the current cycle to change duty https://github.com/espressif/arduino-esp32/issues/5306
sendMotors(); sendMotors();
pause(3); pause(3);
+10 -8
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@@ -5,14 +5,16 @@
#include <Preferences.h> #include <Preferences.h>
#include "util.h" #include "util.h"
#include "pid.h"
extern int channelZero[16], channelMax[16]; extern int channelZero[16], channelMax[16];
extern int rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel; extern int rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
extern int rcRxPin, voltagePin; extern int rcRxPin, voltagePin;
extern int wifiMode, wifiLongRange, udpLocalPort, udpRemotePort, espnowChannel; extern int wifiMode, wifiLongRange, udpLocalPort, udpRemotePort, espnowChannel;
extern float rcLossTimeout, descendTime; extern float rcLossTimeout, descendTime, disarmTilt;
extern float voltageScale; extern float voltageScale;
extern LowPassFilter<float> voltageFilter; extern LowPassFilter<float> voltageFilter;
extern PID posX_PID, posY_PID;
Preferences storage; Preferences storage;
@@ -59,14 +61,13 @@ Parameter parameters[] = {
{"CTL_FLT_MODE_0", &flightModes[0]}, {"CTL_FLT_MODE_0", &flightModes[0]},
{"CTL_FLT_MODE_1", &flightModes[1]}, {"CTL_FLT_MODE_1", &flightModes[1]},
{"CTL_FLT_MODE_2", &flightModes[2]}, {"CTL_FLT_MODE_2", &flightModes[2]},
// position
{"POS_XY_P", &posX_PID.p, setupPosition},
{"POS_XY_I", &posX_PID.i, setupPosition},
{"POS_XY_D", &posX_PID.d, setupPosition},
{"POS_XY_WU", &posX_PID.windup, setupPosition},
{"POS_XY_D_A", &posX_PID.lpf.alpha, setupPosition},
// imu // imu
{"IMU_MODEL", &imuModel},
{"IMU_BUS", &imuBus},
{"IMU_PIN_SCK", &imuSckPin},
{"IMU_PIN_MISO", &imuMisoPin},
{"IMU_PIN_MOSI", &imuMosiPin},
{"IMU_PIN_CS", &imuCsPin},
{"IMU_PIN_INT", &imuIntPin},
{"IMU_ROT_ROLL", &imuRotation.x}, {"IMU_ROT_ROLL", &imuRotation.x},
{"IMU_ROT_PITCH", &imuRotation.y}, {"IMU_ROT_PITCH", &imuRotation.y},
{"IMU_ROT_YAW", &imuRotation.z}, {"IMU_ROT_YAW", &imuRotation.z},
@@ -153,6 +154,7 @@ Parameter parameters[] = {
// safety // safety
{"SF_RC_LOSS_TIME", &rcLossTimeout}, {"SF_RC_LOSS_TIME", &rcLossTimeout},
{"SF_DESCEND_TIME", &descendTime}, {"SF_DESCEND_TIME", &descendTime},
{"SF_DISARM_TILT", &disarmTilt}
}; };
void setupParameters() { void setupParameters() {
+95
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@@ -0,0 +1,95 @@
#include "vector.h"
#include "quaternion.h"
#include "pid.h"
#include "util.h"
float mass = 0.065;
float motorThrust = 0.031 * ONE_G;
float positionWeight = 0.9;
float velocityWeight = 0.9;
PID velX_PID(1.0, 0.0, 0.02);
PID velY_PID(1.0, 0.0, 0.02);
PID velZ_PID(1.0, 0.0, 0.02);
// PID posX_PID(1.0, 0.0, 0.0);
// PID posY_PID(1.0, 0.0, 0.0);
// PID posZ_PID(1.0, 0.0, 0.0);
PID posX_PID(0.1, 0.0, 0.0);
PID posY_PID(0.1, 0.0, 0.0);
PID posZ_PID(0.1, 0.0, 0.0);
Vector acceleration;
Vector velocity;
Vector position;
Vector velocityTarget(NAN, NAN, NAN);
Vector positionTarget(NAN, NAN, NAN);
extern Quaternion attitudeTarget;
extern float thrustTarget;
void setupPosition() {
// TODO: posY_PID = posX_PID;
// posX_PID.copy(posY_PID);
posY_PID.p = posX_PID.p;
posY_PID.i = posX_PID.i;
posY_PID.d = posX_PID.d;
}
void estimatePosition() {
acceleration = Quaternion::rotateVector(acceleration, attitude) + Vector(0, 0, -ONE_G);
velocity += acceleration * dt;
position += velocity * dt;
}
void correctPosition(Vector& pos) {
// position += (pos - position) * positionWeight;
position = pos;
// positionUpdated = true;
if (invalid(positionTarget.x) || invalid(positionTarget.y)) return;
attitudeTarget.setPitch(posX_PID.update(positionTarget.x - position.x));
attitudeTarget.setRoll(posY_PID.update(positionTarget.y - position.y));
}
void correctVelocity(Vector& vel) {
velocity += (vel - velocity) * velocityWeight;
}
void controlVelocity() {
Vector accelerationTarget(
velX_PID.update(velocityTarget.x - velocity.x),
velY_PID.update(velocityTarget.y - velocity.y),
velZ_PID.update(velocityTarget.z - velocity.z)
);
Vector thrustVector = (accelerationTarget + Vector(0, 0, ONE_G)) * mass;
const Vector up(0, 0, 1);
attitudeTarget = Quaternion::fromBetweenVectors(up, thrustVector);
float maxThrust = motorThrust * 4; // 4 motors
thrustTarget = thrustVector.norm() / maxThrust;
}
void controlPosition() {
if (positionTarget.invalid()) return;
velocityTarget = Vector(
posX_PID.update(positionTarget.x - position.x),
posY_PID.update(positionTarget.y - position.y),
posZ_PID.update(positionTarget.z - position.z)
);
controlVelocity();
}
void controlPositionSimple() {
if (positionTarget.invalid()) return;
// straight attitude target control
attitudeTarget.setPitch(posX_PID.update(positionTarget.x - position.x));
attitudeTarget.setRoll(posY_PID.update(positionTarget.y - position.y));
}
+15 -1
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@@ -8,10 +8,12 @@ extern float controlRoll, controlPitch, controlThrottle, controlYaw;
float rcLossTimeout = 1; float rcLossTimeout = 1;
float descendTime = 10; float descendTime = 10;
float disarmTilt = radians(120);
void failsafe() { void failsafe() {
rcLossFailsafe(); rcLossFailsafe();
autoFailsafe(); autoFailsafe();
tiltFailsafe();
} }
// RC loss failsafe // RC loss failsafe
@@ -36,7 +38,7 @@ void descend() {
// Allow pilot to interrupt automatic flight // Allow pilot to interrupt automatic flight
void autoFailsafe() { void autoFailsafe() {
static float roll, pitch, yaw, throttle; static float roll, pitch, yaw, throttle;
if (roll != controlRoll || pitch != controlPitch || yaw != controlYaw || abs(throttle - controlThrottle) > 0.05) { if (abs(roll - controlRoll) > 0.05 || abs(pitch - controlPitch) > 0.05 || abs(yaw - controlYaw) > 0.05 || abs(throttle - controlThrottle) > 0.05) {
// controls changed and mode switch is not configured // controls changed and mode switch is not configured
if (mode == AUTO && invalid(controlMode)) mode = STAB; // regain control by the pilot if (mode == AUTO && invalid(controlMode)) mode = STAB; // regain control by the pilot
} }
@@ -45,3 +47,15 @@ void autoFailsafe() {
yaw = controlYaw; yaw = controlYaw;
throttle = controlThrottle; throttle = controlThrottle;
} }
// Disarm if tilted too much
void tiltFailsafe() {
if (!armed) return;
if (mode != STAB) return;
Vector up = Quaternion::rotateVector(Vector(0, 0, 1), attitude);
float tilt = acos(up.z);
if (disarmTilt && tilt > disarmTilt) {
armed = false;
}
}
+2 -2
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@@ -58,7 +58,7 @@ void sendWiFi(const uint8_t *buf, int len) {
espnow.write(buf, len); espnow.write(buf, len);
static Rate discovery(2); static Rate discovery(2);
if (discovery) espnowBroadcast.write((const uint8_t *)"flix", 4); // broadcast message to help finding this device if (espnow.isEncrypted() && discovery) espnowBroadcast.write((const uint8_t *)"flix", 4); // broadcast message to help finding this device
return; return;
} }
@@ -89,7 +89,7 @@ void printWiFiInfo() {
print("MAC: %s\n", WiFi.softAPmacAddress().c_str()); print("MAC: %s\n", WiFi.softAPmacAddress().c_str());
print("Peer MAC: %s\n", MacAddress(espnow.addr()).toString().c_str()); print("Peer MAC: %s\n", MacAddress(espnow.addr()).toString().c_str());
print("Encrypted: %d\n", espnow.isEncrypted()); print("Encrypted: %d\n", espnow.isEncrypted());
print("Channel: %d\n", espnow.getChannel()); print("Channel: %d\n", WiFi.channel());
print("Lost packets: %d\n", espnow.lost); print("Lost packets: %d\n", espnow.lost);
} else if (WiFi.getMode() == WIFI_MODE_AP) { } else if (WiFi.getMode() == WIFI_MODE_AP) {
print("Mode: Access Point (AP)\n"); print("Mode: Access Point (AP)\n");
+2 -5
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@@ -21,10 +21,6 @@ extern float motors[4];
Vector gyro, acc, imuRotation; Vector gyro, acc, imuRotation;
Vector accBias, gyroBias, accScale(1, 1, 1); Vector accBias, gyroBias, accScale(1, 1, 1);
LowPassFilter<Vector> gyroBiasFilter(0); LowPassFilter<Vector> gyroBiasFilter(0);
int imuModel = 1, imuBus = 0;
int imuSckPin = 0, imuMisoPin = 0, imuMosiPin = 0, imuCsPin = -1, imuIntPin = -1;
int imuSdaPin = 0, imuSclPin = 0;
int rgbPin = -1, rgbNum = 1;
// declarations // declarations
void step(); void step();
@@ -42,7 +38,7 @@ const char* getModeName();
void sendMotors(); void sendMotors();
int getDutyCycle(float value); int getDutyCycle(float value);
bool motorsActive(); bool motorsActive();
void testMotor(int n); void testMotor(int, float);
void print(const char* format, ...); void print(const char* format, ...);
void pause(float duration); void pause(float duration);
void doCommand(String str, bool echo); void doCommand(String str, bool echo);
@@ -76,6 +72,7 @@ void failsafe();
void rcLossFailsafe(); void rcLossFailsafe();
void descend(); void descend();
void autoFailsafe(); void autoFailsafe();
void tiltFailsafe();
int parametersCount(); int parametersCount();
const char *getParameterName(int index); const char *getParameterName(int index);
float getParameter(int index); float getParameter(int index);
+30 -10
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@@ -11,18 +11,22 @@
#include <Preferences.h> #include <Preferences.h>
#include "../../flix/util.h" #include "../../flix/util.h"
const int CHANNEL = 6; const bool DISABLE_SWARM = true;
const int CHANNEL = -1; // -1 means auto search
char key[ESP_NOW_KEY_LEN + 1] = {0}; // with trailing null char key[ESP_NOW_KEY_LEN + 1] = {0}; // with trailing null
Preferences storage; Preferences storage;
std::vector<ESPNOWSerial *> peers; std::vector<ESPNOWSerial *> peers;
bool stop = false;
void onNewPeer(const esp_now_recv_info_t *info, const uint8_t *data, int len, void *arg) { void onNewPeer(const esp_now_recv_info_t *info, const uint8_t *data, int len, void *arg) {
if (len != 4 || memcmp(data, "flix", 4) != 0) return; // check if discovery message if (len != 4 || memcmp(data, "flix", 4) != 0) return; // check if discovery message
if (stop) return;
Serial.printf("New peer: " MACSTR "\n", MAC2STR(info->src_addr)); Serial.printf("New peer: " MACSTR "\n", MAC2STR(info->src_addr));
ESPNOWSerial *link = new ESPNOWSerial(info->src_addr, CHANNEL, WIFI_IF_AP); ESPNOWSerial *link = new ESPNOWSerial(info->src_addr, WiFi.channel(), WIFI_IF_STA);
link->begin(); link->begin();
link->setKey((const uint8_t *)key); link->setKey((const uint8_t *)key);
peers.push_back(link); peers.push_back(link);
@@ -30,9 +34,8 @@ void onNewPeer(const esp_now_recv_info_t *info, const uint8_t *data, int len, vo
void setup() { void setup() {
Serial.begin(115200); Serial.begin(115200);
WiFi.mode(WIFI_AP); WiFi.mode(WIFI_STA);
WiFi.setSleep(false); WiFi.setSleep(false);
WiFi.setChannel(CHANNEL);
ESP_NOW.onNewPeer(onNewPeer, NULL); ESP_NOW.onNewPeer(onNewPeer, NULL);
ESP_NOW.begin(); ESP_NOW.begin();
@@ -43,12 +46,6 @@ void setup() {
storage.putString("key", key); storage.putString("key", key);
} }
strcpy(key, storage.getString("key").c_str()); strcpy(key, storage.getString("key").c_str());
// Discover the first peer
while (peers.empty()) {
Serial.printf("espnow %s %s\n", WiFi.softAPmacAddress().c_str(), key);
delay(500);
}
} }
void generateRandomKey() { void generateRandomKey() {
@@ -61,6 +58,20 @@ void generateRandomKey() {
void loop() { void loop() {
uint8_t buf[5000]; uint8_t buf[5000];
static int channelIndex = 0;
static const int channels[] = {6, 11, 1, 2, 6, 11, 3, 4, 5, 6, 1, 11, 8, 6, 9, 10, 11, 6, 1, 12, 13}; // 6, 1 and 11 are most common
static unsigned long last = 0;
if (!stop && millis() - last > 500) {
// Change search channel
last = millis();
channelIndex = (channelIndex + 1) % (sizeof(channels) / sizeof(channels[0]));
int channel = CHANNEL < 0 ? channels[channelIndex] : CHANNEL;
Serial.printf("Run on Flix: espnow %s %s\n", WiFi.STA.macAddress().c_str(), key);
Serial.printf("Searching channel %d\n", channel);
WiFi.setChannel(channel);
}
// Send from Serial to ESP-NOW // Send from Serial to ESP-NOW
while (Serial.available() > 0) { while (Serial.available() > 0) {
int b = Serial.read(); int b = Serial.read();
@@ -81,6 +92,15 @@ void loop() {
// Send from ESP-NOW to Serial // Send from ESP-NOW to Serial
for (ESPNOWSerial *link : peers) { for (ESPNOWSerial *link : peers) {
int len = link->read(buf, sizeof(buf)); int len = link->read(buf, sizeof(buf));
if (!stop) {
for (int i = 0; i < len; i++) {
if (buf[i] == MAVLINK_STX) {
// Got MAVLink message, stop discovery
Serial.printf("Received MAVLink from " MACSTR "\n", MAC2STR(link->addr()));
if (DISABLE_SWARM) stop = true;
}
}
}
if (len > 0) { if (len > 0) {
Serial.write(buf, len); Serial.write(buf, len);
} }