1 Commits

Author SHA1 Message Date
Oleg Kalachev
6c41f65ef9 Apply motors configuration without reboot 2026-01-27 09:56:39 +03:00
12 changed files with 19 additions and 31 deletions

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@@ -143,8 +143,6 @@ 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.

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@@ -4,17 +4,6 @@ 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>

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@@ -52,7 +52,6 @@ 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;
@@ -66,9 +65,9 @@ void control() {
}
void interpretControls() {
if (controlMode < 0.25) mode = flightModes[0];
else if (controlMode < 0.75) mode = flightModes[1];
else if (controlMode > 0.75) mode = flightModes[2];
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

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@@ -24,6 +24,7 @@ void setupMotors() {
// configure pins
for (int i = 0; i < 4; i++) {
ledcAttach(motorPins[i], pwmFrequency, pwmResolution);
pwmFrequency = ledcChangeFrequency(motorPins[i], pwmFrequency, pwmResolution); // if re-initializing
}
sendMotors();
print("Motors initialized\n");

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@@ -49,9 +49,6 @@ 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},
@@ -123,6 +120,11 @@ void setupParameters() {
}
}
void afterParameterChange(String name, const float value) {
if (name == "MOT_PWM_FREQ" || name == "MOT_PWM_RES") setupMotors();
if (name == "MOT_PIN_FL" || name == "MOT_PIN_FR" || name == "MOT_PIN_RL" || name == "MOT_PIN_RR") setupMotors();
}
int parametersCount() {
return sizeof(parameters) / sizeof(parameters[0]);
}
@@ -151,6 +153,7 @@ bool setParameter(const char *name, const float value) {
if (strcasecmp(parameter.name, name) == 0) {
if (parameter.integer && !isfinite(value)) return false; // can't set integer to NaN or Inf
parameter.setValue(value);
afterParameterChange(name, value);
return true;
}
}

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@@ -165,6 +165,7 @@ void delay(uint32_t ms) {
bool ledcAttach(uint8_t pin, uint32_t freq, uint8_t resolution) { return true; }
bool ledcWrite(uint8_t pin, uint32_t duty) { return true; }
uint32_t ledcChangeFrequency(uint8_t pin, uint32_t freq, uint8_t resolution) { return freq; }
unsigned long __micros;
unsigned long __resetTime = 0;

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@@ -9,7 +9,6 @@
#include "quaternion.h"
#include "Arduino.h"
#include "wifi.h"
#include "lpf.h"
extern float t, dt;
extern float controlRoll, controlPitch, controlYaw, controlThrottle, controlMode;
@@ -20,7 +19,6 @@ extern float motors[4];
Vector gyro, acc, imuRotation;
Vector accBias, gyroBias, accScale(1, 1, 1);
LowPassFilter<Vector> gyroBiasFilter(0);
// declarations
void step();

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@@ -11,10 +11,9 @@
#include <sys/poll.h>
#include <gazebo/gazebo.hh>
int wifiMode = 1; // mock
int udpLocalPort = 14580;
int udpRemotePort = 14550;
const char *udpRemoteIP = "255.255.255.255";
#define WIFI_UDP_PORT 14580
#define WIFI_UDP_REMOTE_PORT 14550
#define WIFI_UDP_REMOTE_ADDR "255.255.255.255"
int wifiSocket;
@@ -23,22 +22,22 @@ void setupWiFi() {
sockaddr_in addr; // local address
addr.sin_family = AF_INET;
addr.sin_addr.s_addr = INADDR_ANY;
addr.sin_port = htons(udpLocalPort);
addr.sin_port = htons(WIFI_UDP_PORT);
if (bind(wifiSocket, (sockaddr *)&addr, sizeof(addr))) {
gzerr << "Failed to bind WiFi UDP socket on port " << udpLocalPort << std::endl;
gzerr << "Failed to bind WiFi UDP socket on port " << WIFI_UDP_PORT << std::endl;
return;
}
int broadcast = 1;
setsockopt(wifiSocket, SOL_SOCKET, SO_BROADCAST, &broadcast, sizeof(broadcast)); // enable broadcast
gzmsg << "WiFi UDP socket initialized on port " << udpLocalPort << " (remote port " << udpRemotePort << ")" << std::endl;
gzmsg << "WiFi UDP socket initialized on port " << WIFI_UDP_PORT << " (remote port " << WIFI_UDP_REMOTE_PORT << ")" << 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(udpRemoteIP);
addr.sin_port = htons(udpRemotePort);
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));
}