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BIN
docs/img/user/arkymatsekh/1.jpg
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docs/img/user/arkymatsekh/2.jpg
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docs/img/user/arkymatsekh/3.jpg
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docs/img/user/arkymatsekh/video.jpg
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@@ -134,6 +134,20 @@ Before flight you need to calibrate the accelerometer:
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1. Access the console using QGroundControl (recommended) or Serial Monitor.
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1. Access the console using QGroundControl (recommended) or Serial Monitor.
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2. Type `ca` command there and follow the instructions.
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2. Type `ca` command there and follow the instructions.
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### Setup motors
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||||||
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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).
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||||||
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If using brushless motors and ESCs:
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1. Set the appropriate PWM using the parameters: `MOT_PWM_STOP`, `MOT_PWM_MIN`, and `MOT_PWM_MAX` (1000, 1000, and 2000 is typical).
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2. Decrease the PWM frequency using the `MOT_PWM_FREQ` parameter (400 is typical).
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Reboot the drone to apply the changes.
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> [!CAUTION]
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> **Remove the props when configuring the motors!** If improperly configured, you may not be able to stop them.
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### Check everything works
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### Check everything works
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1. Check the IMU is working: perform `imu` command and check its output:
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1. Check the IMU is working: perform `imu` command and check its output:
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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
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---
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---
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Author: **Arkadiy "Arky" Matsekh**, Foucault Dynamics, Gold Coast, Australia.<br>
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The drone was built for the University of Queensland industry-led Master's capstone project.
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**Flight video:**
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<a href="https://drive.google.com/file/d/1NNYSVXBY-w0JjCo07D8-PgnVq3ca9plj/view?usp=sharing"><img height=300 src="img/user/arkymatsekh/video.jpg"></a>
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<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>
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---
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Author: [goldarte](https://t.me/goldarte).<br>
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Author: [goldarte](https://t.me/goldarte).<br>
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<img src="img/user/goldarte/1.jpg" height=150> <img src="img/user/goldarte/2.jpg" height=150>
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<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 =
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"log [dump] - print log header [and data]\n"
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"log [dump] - print log header [and data]\n"
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"cr - calibrate RC\n"
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"cr - calibrate RC\n"
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"ca - calibrate accel\n"
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"ca - calibrate accel\n"
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"cl - calibrate level\n"
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"mfr, mfl, mrr, mrl - test motor (remove props)\n"
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"mfr, mfl, mrr, mrl - test motor (remove props)\n"
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"sys - show system info\n"
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"sys - show system info\n"
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"reset - reset drone's state\n"
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"reset - reset drone's state\n"
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@@ -94,7 +95,7 @@ void doCommand(String str, bool echo = false) {
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} else if (command == "p") {
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} else if (command == "p") {
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bool success = setParameter(arg0.c_str(), arg1.toFloat());
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bool success = setParameter(arg0.c_str(), arg1.toFloat());
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if (success) {
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if (success) {
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print("%s = %g\n", arg0.c_str(), arg1.toFloat());
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print("%s = %g\n", arg0.c_str(), getParameter(arg0.c_str()));
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} else {
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} else {
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print("Parameter not found: %s\n", arg0.c_str());
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print("Parameter not found: %s\n", arg0.c_str());
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}
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}
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@@ -151,6 +152,8 @@ void doCommand(String str, bool echo = false) {
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calibrateRC();
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calibrateRC();
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} else if (command == "ca") {
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} else if (command == "ca") {
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calibrateAccel();
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calibrateAccel();
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} else if (command == "cl") {
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calibrateLevel();
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} else if (command == "mfr") {
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} else if (command == "mfr") {
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testMotor(MOTOR_FRONT_RIGHT);
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testMotor(MOTOR_FRONT_RIGHT);
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} else if (command == "mfl") {
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} else if (command == "mfl") {
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@@ -52,6 +52,7 @@ PID pitchPID(PITCH_P, PITCH_I, PITCH_D);
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PID yawPID(YAW_P, 0, 0);
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PID yawPID(YAW_P, 0, 0);
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Vector maxRate(ROLLRATE_MAX, PITCHRATE_MAX, YAWRATE_MAX);
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Vector maxRate(ROLLRATE_MAX, PITCHRATE_MAX, YAWRATE_MAX);
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float tiltMax = TILT_MAX;
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float tiltMax = TILT_MAX;
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int flightModes[] = {STAB, STAB, STAB}; // map for rc mode switch
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extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
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extern const int MOTOR_REAR_LEFT, MOTOR_REAR_RIGHT, MOTOR_FRONT_RIGHT, MOTOR_FRONT_LEFT;
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extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
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extern float controlRoll, controlPitch, controlThrottle, controlYaw, controlMode;
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@@ -65,9 +66,9 @@ void control() {
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}
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}
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||||||
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||||||
void interpretControls() {
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void interpretControls() {
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if (controlMode < 0.25) mode = STAB;
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if (controlMode < 0.25) mode = flightModes[0];
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if (controlMode < 0.75) mode = STAB;
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else if (controlMode < 0.75) mode = flightModes[1];
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if (controlMode > 0.75) mode = STAB;
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else if (controlMode > 0.75) mode = flightModes[2];
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if (mode == AUTO) return; // pilot is not effective in AUTO mode
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if (mode == AUTO) return; // pilot is not effective in AUTO mode
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|||||||
@@ -110,6 +110,14 @@ void calibrateAccelOnce() {
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accBias = (accMax + accMin) / 2;
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accBias = (accMax + accMin) / 2;
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}
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}
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void calibrateLevel() {
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print("Place perfectly level [1 sec]\n");
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pause(1);
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Quaternion correction = Quaternion::fromBetweenVectors(Quaternion::rotateVector(Vector(0, 0, 1), attitude), Vector(0, 0, 1));
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imuRotation = Quaternion::rotate(correction, Quaternion::fromEuler(imuRotation)).toEuler();
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print("✓ Done: %.3f %.3f %.3f\n", degrees(imuRotation.x), degrees(imuRotation.y), degrees(imuRotation.z));
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}
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void printIMUCalibration() {
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void printIMUCalibration() {
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print("gyro bias: %f %f %f\n", gyroBias.x, gyroBias.y, gyroBias.z);
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print("gyro bias: %f %f %f\n", gyroBias.x, gyroBias.y, gyroBias.z);
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print("accel bias: %f %f %f\n", accBias.x, accBias.y, accBias.z);
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print("accel bias: %f %f %f\n", accBias.x, accBias.y, accBias.z);
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@@ -1,24 +1,19 @@
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// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
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// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
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// Repository: https://github.com/okalachev/flix
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// Repository: https://github.com/okalachev/flix
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// Motors output control using MOSFETs
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// PWM control for motors
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// In case of using ESCs, change PWM_STOP, PWM_MIN and PWM_MAX to appropriate values in μs, decrease PWM_FREQUENCY (to 400)
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#include "util.h"
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#include "util.h"
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#define MOTOR_0_PIN 12 // rear left
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#define MOTOR_1_PIN 13 // rear right
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#define MOTOR_2_PIN 14 // front right
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#define MOTOR_3_PIN 15 // front left
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#define PWM_FREQUENCY 78000
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#define PWM_RESOLUTION 10
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#define PWM_STOP 0
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#define PWM_MIN 0
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#define PWM_MAX 1000000 / PWM_FREQUENCY
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||||||
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float motors[4]; // normalized motor thrusts in range [0..1]
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float motors[4]; // normalized motor thrusts in range [0..1]
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int motorPins[4] = {12, 13, 14, 15}; // default pin numbers
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int pwmFrequency = 78000;
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int pwmResolution = 10;
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int pwmStop = 0;
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int pwmMin = 0;
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||||||
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int pwmMax = -1; // -1 means duty cycle mode
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||||||
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||||||
const int MOTOR_REAR_LEFT = 0;
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const int MOTOR_REAR_LEFT = 0;
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const int MOTOR_REAR_RIGHT = 1;
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const int MOTOR_REAR_RIGHT = 1;
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const int MOTOR_FRONT_RIGHT = 2;
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const int MOTOR_FRONT_RIGHT = 2;
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@@ -26,30 +21,30 @@ const int MOTOR_FRONT_LEFT = 3;
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void setupMotors() {
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void setupMotors() {
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print("Setup Motors\n");
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print("Setup Motors\n");
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// configure pins
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// configure pins
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ledcAttach(MOTOR_0_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
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for (int i = 0; i < 4; i++) {
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ledcAttach(MOTOR_1_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
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ledcAttach(motorPins[i], pwmFrequency, pwmResolution);
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ledcAttach(MOTOR_2_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
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}
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ledcAttach(MOTOR_3_PIN, PWM_FREQUENCY, PWM_RESOLUTION);
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sendMotors();
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sendMotors();
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print("Motors initialized\n");
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print("Motors initialized\n");
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}
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}
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int getDutyCycle(float value) {
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void sendMotors() {
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value = constrain(value, 0, 1);
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for (int i = 0; i < 4; i++) {
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float pwm = mapf(value, 0, 1, PWM_MIN, PWM_MAX);
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ledcWrite(motorPins[i], getDutyCycle(motors[i]));
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if (value == 0) pwm = PWM_STOP;
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}
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float duty = mapf(pwm, 0, 1000000 / PWM_FREQUENCY, 0, (1 << PWM_RESOLUTION) - 1);
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return round(duty);
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}
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}
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void sendMotors() {
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int getDutyCycle(float value) {
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ledcWrite(MOTOR_0_PIN, getDutyCycle(motors[0]));
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value = constrain(value, 0, 1);
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ledcWrite(MOTOR_1_PIN, getDutyCycle(motors[1]));
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if (pwmMax >= 0) { // pwm mode
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ledcWrite(MOTOR_2_PIN, getDutyCycle(motors[2]));
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float pwm = mapf(value, 0, 1, pwmMin, pwmMax);
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ledcWrite(MOTOR_3_PIN, getDutyCycle(motors[3]));
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if (value == 0) pwm = pwmStop;
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float duty = mapf(pwm, 0, 1000000 / pwmFrequency, 0, (1 << pwmResolution) - 1);
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return round(duty);
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} else { // duty cycle mode
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return round(value * ((1 << pwmResolution) - 1));
|
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|
}
|
||||||
}
|
}
|
||||||
|
|
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bool motorsActive() {
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bool motorsActive() {
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@@ -49,6 +49,9 @@ Parameter parameters[] = {
|
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{"CTL_R_RATE_MAX", &maxRate.x},
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{"CTL_R_RATE_MAX", &maxRate.x},
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{"CTL_Y_RATE_MAX", &maxRate.z},
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{"CTL_Y_RATE_MAX", &maxRate.z},
|
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{"CTL_TILT_MAX", &tiltMax},
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{"CTL_TILT_MAX", &tiltMax},
|
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|
{"CTL_FLT_MODE_0", &flightModes[0]},
|
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|
{"CTL_FLT_MODE_1", &flightModes[1]},
|
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|
{"CTL_FLT_MODE_2", &flightModes[2]},
|
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// imu
|
// imu
|
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{"IMU_ROT_ROLL", &imuRotation.x},
|
{"IMU_ROT_ROLL", &imuRotation.x},
|
||||||
{"IMU_ROT_PITCH", &imuRotation.y},
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{"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]},
|
||||||
|
|||||||
@@ -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() {};
|
||||||
|
|||||||
@@ -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));
|
||||||
}
|
}
|
||||||
|
|
||||||
|
|||||||
Reference in New Issue
Block a user