6 Commits

Author SHA1 Message Date
Oleg Kalachev
f8f746b0cd Add level calibration 2026-01-30 07:49:26 +03:00
Oleg Kalachev
3dde380bb7 Add parameters for list of modes bound to rc switch
Parameters: CTL_FLT_MODE_0, CTL_FLT_MODE_1, CTL_FLT_MODE_2.
Also fix a bug with incorrect choosing the mode from controlMode.
2026-01-27 16:38:20 +03:00
Oleg Kalachev
377b21429b Fix error when launching the sim
Also make the parameters WIFI_LOC_PORT and WIFI_REM_PORT work in the sim.
2026-01-27 16:32:52 +03:00
Oleg Kalachev
1ac443d6f8 Add a build by Arky Matsekh 2026-01-27 15:17:58 +03:00
Oleg Kalachev
964c0f7bc1 Make setting parameter in console printing actual parameter value.
In some cases, it would not be equal to the requested value.
2026-01-27 09:28:01 +03:00
Oleg Kalachev
40bdaacedb Make motor subsystem configurable using parameters
Motor pins: MOT_PIN_FL, MOT_PIN_FR, MOT_PIN_RL, MOT_PIN_RR.
PWM configuration: MOT_PWM_FREQ, MOT_PWM_RES, MOT_PWM_STOP, MOT_PWM_MIN, MOT_PWM_MAX.
MOT_PWM_MAX = -1 chooses duty cycle mode for brushed motors (default).
2026-01-27 08:40:52 +03:00
13 changed files with 92 additions and 42 deletions

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@@ -134,6 +134,20 @@ Before flight you need to calibrate the accelerometer:
1. Access the console using QGroundControl (recommended) or Serial Monitor. 1. Access the console using QGroundControl (recommended) or Serial Monitor.
2. Type `ca` command there and follow the instructions. 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 ### Check everything works
1. Check the IMU is working: perform `imu` command and check its output: 1. Check the IMU is working: perform `imu` command and check its output:

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@@ -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> 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> <img src="img/user/goldarte/1.jpg" height=150> <img src="img/user/goldarte/2.jpg" height=150>

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@@ -46,6 +46,7 @@ const char* motd =
"log [dump] - print log header [and data]\n" "log [dump] - print log header [and data]\n"
"cr - calibrate RC\n" "cr - calibrate RC\n"
"ca - calibrate accel\n" "ca - calibrate accel\n"
"cl - calibrate level\n"
"mfr, mfl, mrr, mrl - test motor (remove props)\n" "mfr, mfl, mrr, mrl - test motor (remove props)\n"
"sys - show system info\n" "sys - show system info\n"
"reset - reset drone's state\n" "reset - reset drone's state\n"
@@ -94,7 +95,7 @@ void doCommand(String str, bool echo = false) {
} else if (command == "p") { } else if (command == "p") {
bool success = setParameter(arg0.c_str(), arg1.toFloat()); bool success = setParameter(arg0.c_str(), arg1.toFloat());
if (success) { if (success) {
print("%s = %g\n", arg0.c_str(), arg1.toFloat()); print("%s = %g\n", arg0.c_str(), getParameter(arg0.c_str()));
} else { } else {
print("Parameter not found: %s\n", arg0.c_str()); print("Parameter not found: %s\n", arg0.c_str());
} }
@@ -151,6 +152,8 @@ void doCommand(String str, bool echo = false) {
calibrateRC(); calibrateRC();
} else if (command == "ca") { } else if (command == "ca") {
calibrateAccel(); calibrateAccel();
} else if (command == "cl") {
calibrateLevel();
} else if (command == "mfr") { } else if (command == "mfr") {
testMotor(MOTOR_FRONT_RIGHT); testMotor(MOTOR_FRONT_RIGHT);
} else if (command == "mfl") { } else if (command == "mfl") {

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@@ -52,6 +52,7 @@ PID pitchPID(PITCH_P, PITCH_I, PITCH_D);
PID yawPID(YAW_P, 0, 0); PID yawPID(YAW_P, 0, 0);
Vector maxRate(ROLLRATE_MAX, PITCHRATE_MAX, YAWRATE_MAX); Vector maxRate(ROLLRATE_MAX, PITCHRATE_MAX, YAWRATE_MAX);
float tiltMax = TILT_MAX; float tiltMax = TILT_MAX;
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;
@@ -65,9 +66,9 @@ void control() {
} }
void interpretControls() { void interpretControls() {
if (controlMode < 0.25) mode = STAB; if (controlMode < 0.25) mode = flightModes[0];
if (controlMode < 0.75) mode = STAB; else if (controlMode < 0.75) mode = flightModes[1];
if (controlMode > 0.75) mode = STAB; else if (controlMode > 0.75) mode = flightModes[2];
if (mode == AUTO) return; // pilot is not effective in AUTO mode if (mode == AUTO) return; // pilot is not effective in AUTO mode

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@@ -110,6 +110,14 @@ void calibrateAccelOnce() {
accBias = (accMax + accMin) / 2; accBias = (accMax + accMin) / 2;
} }
void calibrateLevel() {
print("Place perfectly level [1 sec]\n");
pause(1);
Quaternion correction = Quaternion::fromBetweenVectors(Quaternion::rotateVector(Vector(0, 0, 1), attitude), Vector(0, 0, 1));
imuRotation = Quaternion::rotate(correction, Quaternion::fromEuler(imuRotation)).toEuler();
print("✓ Done: %.3f %.3f %.3f\n", degrees(imuRotation.x), degrees(imuRotation.y), degrees(imuRotation.z));
}
void printIMUCalibration() { void printIMUCalibration() {
print("gyro bias: %f %f %f\n", gyroBias.x, gyroBias.y, gyroBias.z); print("gyro bias: %f %f %f\n", gyroBias.x, gyroBias.y, gyroBias.z);
print("accel bias: %f %f %f\n", accBias.x, accBias.y, accBias.z); print("accel bias: %f %f %f\n", accBias.x, accBias.y, accBias.z);

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@@ -1,24 +1,19 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com> // Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix // Repository: https://github.com/okalachev/flix
// Motors output control using MOSFETs // PWM control for motors
// In case of using ESCs, change PWM_STOP, PWM_MIN and PWM_MAX to appropriate values in μs, decrease PWM_FREQUENCY (to 400)
#include "util.h" #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] 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_LEFT = 0;
const int MOTOR_REAR_RIGHT = 1; const int MOTOR_REAR_RIGHT = 1;
const int MOTOR_FRONT_RIGHT = 2; const int MOTOR_FRONT_RIGHT = 2;
@@ -26,30 +21,30 @@ const int MOTOR_FRONT_LEFT = 3;
void setupMotors() { void setupMotors() {
print("Setup Motors\n"); print("Setup Motors\n");
// configure pins // configure pins
ledcAttach(MOTOR_0_PIN, PWM_FREQUENCY, PWM_RESOLUTION); for (int i = 0; i < 4; i++) {
ledcAttach(MOTOR_1_PIN, PWM_FREQUENCY, PWM_RESOLUTION); ledcAttach(motorPins[i], pwmFrequency, pwmResolution);
ledcAttach(MOTOR_2_PIN, PWM_FREQUENCY, PWM_RESOLUTION); }
ledcAttach(MOTOR_3_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
sendMotors(); sendMotors();
print("Motors initialized\n"); print("Motors initialized\n");
} }
int getDutyCycle(float value) { void sendMotors() {
value = constrain(value, 0, 1); for (int i = 0; i < 4; i++) {
float pwm = mapf(value, 0, 1, PWM_MIN, PWM_MAX); ledcWrite(motorPins[i], getDutyCycle(motors[i]));
if (value == 0) pwm = PWM_STOP; }
float duty = mapf(pwm, 0, 1000000 / PWM_FREQUENCY, 0, (1 << PWM_RESOLUTION) - 1);
return round(duty);
} }
void sendMotors() { int getDutyCycle(float value) {
ledcWrite(MOTOR_0_PIN, getDutyCycle(motors[0])); value = constrain(value, 0, 1);
ledcWrite(MOTOR_1_PIN, getDutyCycle(motors[1])); if (pwmMax >= 0) { // pwm mode
ledcWrite(MOTOR_2_PIN, getDutyCycle(motors[2])); float pwm = mapf(value, 0, 1, pwmMin, pwmMax);
ledcWrite(MOTOR_3_PIN, getDutyCycle(motors[3])); 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() { bool motorsActive() {

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@@ -49,6 +49,9 @@ Parameter parameters[] = {
{"CTL_R_RATE_MAX", &maxRate.x}, {"CTL_R_RATE_MAX", &maxRate.x},
{"CTL_Y_RATE_MAX", &maxRate.z}, {"CTL_Y_RATE_MAX", &maxRate.z},
{"CTL_TILT_MAX", &tiltMax}, {"CTL_TILT_MAX", &tiltMax},
{"CTL_FLT_MODE_0", &flightModes[0]},
{"CTL_FLT_MODE_1", &flightModes[1]},
{"CTL_FLT_MODE_2", &flightModes[2]},
// imu // imu
{"IMU_ROT_ROLL", &imuRotation.x}, {"IMU_ROT_ROLL", &imuRotation.x},
{"IMU_ROT_PITCH", &imuRotation.y}, {"IMU_ROT_PITCH", &imuRotation.y},
@@ -63,6 +66,16 @@ Parameter parameters[] = {
// estimate // estimate
{"EST_ACC_WEIGHT", &accWeight}, {"EST_ACC_WEIGHT", &accWeight},
{"EST_RATES_LPF_A", &ratesFilter.alpha}, {"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
{"RC_ZERO_0", &channelZero[0]}, {"RC_ZERO_0", &channelZero[0]},
{"RC_ZERO_1", &channelZero[1]}, {"RC_ZERO_1", &channelZero[1]},

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@@ -9,6 +9,7 @@
#include "quaternion.h" #include "quaternion.h"
#include "Arduino.h" #include "Arduino.h"
#include "wifi.h" #include "wifi.h"
#include "lpf.h"
extern float t, dt; extern float t, dt;
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode; extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
@@ -19,6 +20,7 @@ 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);
// declarations // declarations
void step(); void step();
@@ -32,6 +34,7 @@ void controlRates();
void controlTorque(); void controlTorque();
const char* getModeName(); const char* getModeName();
void sendMotors(); void sendMotors();
int getDutyCycle(float value);
bool motorsActive(); bool motorsActive();
void testMotor(int n); void testMotor(int n);
void print(const char* format, ...); void print(const char* format, ...);
@@ -68,6 +71,7 @@ void resetParameters();
void setLED(bool on) {}; void setLED(bool on) {};
void calibrateGyro() { print("Skip gyro calibrating\n"); }; void calibrateGyro() { print("Skip gyro calibrating\n"); };
void calibrateAccel() { print("Skip accel calibrating\n"); }; void calibrateAccel() { print("Skip accel calibrating\n"); };
void calibrateLevel() { print("Skip level calibrating\n"); };
void printIMUCalibration() { print("cal: N/A\n"); }; void printIMUCalibration() { print("cal: N/A\n"); };
void printIMUInfo() {}; void printIMUInfo() {};
void printWiFiInfo() {}; void printWiFiInfo() {};

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@@ -11,9 +11,10 @@
#include <sys/poll.h> #include <sys/poll.h>
#include <gazebo/gazebo.hh> #include <gazebo/gazebo.hh>
#define WIFI_UDP_PORT 14580 int wifiMode = 1; // mock
#define WIFI_UDP_REMOTE_PORT 14550 int udpLocalPort = 14580;
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255" int udpRemotePort = 14550;
const char *udpRemoteIP = "255.255.255.255";
int wifiSocket; int wifiSocket;
@@ -22,22 +23,22 @@ void setupWiFi() {
sockaddr_in addr; // local address sockaddr_in addr; // local address
addr.sin_family = AF_INET; addr.sin_family = AF_INET;
addr.sin_addr.s_addr = INADDR_ANY; 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))) { 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; return;
} }
int broadcast = 1; int broadcast = 1;
setsockopt(wifiSocket, SOL_SOCKET, SO_BROADCAST, &broadcast, sizeof(broadcast)); // enable broadcast 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) { void sendWiFi(const uint8_t *buf, int len) {
if (wifiSocket == 0) setupWiFi(); if (wifiSocket == 0) setupWiFi();
sockaddr_in addr; // remote address sockaddr_in addr; // remote address
addr.sin_family = AF_INET; addr.sin_family = AF_INET;
addr.sin_addr.s_addr = inet_addr(WIFI_UDP_REMOTE_ADDR); addr.sin_addr.s_addr = inet_addr(udpRemoteIP);
addr.sin_port = htons(WIFI_UDP_REMOTE_PORT); addr.sin_port = htons(udpRemotePort);
sendto(wifiSocket, buf, len, 0, (sockaddr *)&addr, sizeof(addr)); sendto(wifiSocket, buf, len, 0, (sockaddr *)&addr, sizeof(addr));
} }