1 Commits

Author SHA1 Message Date
Oleg Kalachev
6c41f65ef9 Apply motors configuration without reboot 2026-01-27 09:56:39 +03:00
21 changed files with 69 additions and 103 deletions

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@@ -143,34 +143,30 @@ 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.
### Important: check everything works
### Check everything works
1. Check the IMU is working: perform `imu` command in the console and check the output:
1. Check the IMU is working: perform `imu` command and check its output:
* The `status` field should be `OK`.
* The `rate` field should be about 1000 (Hz).
* The `accel` and `gyro` fields should change as you move the drone.
* The `accel bias` and `accel scale` fields should contain calibration parameters (not zeros and ones).
* The `gyro bias` field should contain estimated gyro bias (not zeros).
* The `landed` field should be `1` when the drone is still on the ground and `0` when you lift it up.
2. Check the attitude estimation: connect to the drone using QGroundControl, rotate the drone in different orientations and check if the attitude estimation shown in QGroundControl is correct. Compare your attitude indicator (in the *large vertical* mode) to the video:
<a href="https://youtu.be/yVRN23-GISU"><img width=300 src="https://i3.ytimg.com/vi/yVRN23-GISU/maxresdefault.jpg"></a>
3. Perform motor tests. Use the following commands **— remove the propellers before running the tests!**
3. Perform motor tests in the console. Use the following commands **— remove the propellers before running the tests!**
* `mfr` — rotate front right motor (counter-clockwise).
* `mfl` — rotate front left motor (clockwise).
* `mrl` — rotate rear left motor (counter-clockwise).
* `mrr` — rotate rear right motor (clockwise).
* `mfr` — should rotate front right motor (counter-clockwise).
* `mfl` — should rotate front left motor (clockwise).
* `mrl` — should rotate rear left motor (counter-clockwise).
* `mrr` — should rotate rear right motor (clockwise).
Make sure rotation directions and propeller types match the following diagram:
Rotation diagram:
<img src="img/motors.svg" width=200>
@@ -236,11 +232,11 @@ When finished flying, **disarm** the drone, moving the left stick to the bottom
### Flight modes
Flight mode is changed using mode switch on the remote control (if configured) or using the console commands. The main flight mode is *STAB*.
Flight mode is changed using mode switch on the remote control or using the command line.
#### STAB
In this mode, the drone stabilizes its attitude (orientation). The left stick controls throttle and yaw rate, the right stick controls pitch and roll angles.
The default mode is *STAB*. In this mode, the drone stabilizes its attitude (orientation). The left stick controls throttle and yaw rate, the right stick controls pitch and roll angles.
> [!IMPORTANT]
> The drone doesn't stabilize its position, so slight drift is possible. The pilot should compensate it manually.
@@ -255,7 +251,7 @@ In this mode, the pilot controls the angular rates. This control method is diffi
#### AUTO
In this mode, the pilot inputs are ignored (except the mode switch). The drone can be controlled using [pyflix](../tools/pyflix/) Python library, or by modifying the firmware to implement the needed behavior.
In this mode, the pilot inputs are ignored (except the mode switch, if configured). The drone can be controlled using [pyflix](../tools/pyflix/) Python library, or by modifying the firmware to implement the needed autonomous behavior.
If the pilot moves the control sticks, the drone will switch back to *STAB* mode.

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@@ -4,33 +4,6 @@ This page contains user-built drones based on the Flix project. Publish your pro
---
Author: [FanBy0ru](https://https://github.com/FanBy0ru).<br>
Description: custom 3D-printed frame.<br>
Frame STLs and flight validation: https://cults3d.com/en/3d-model/gadget/armature-pour-flix-drone.
<img src="img/user/fanby0ru/1.jpg" height=200> <img src="img/user/fanby0ru/2.jpg" height=200>
---
Author: Ivan44 Phalko.<br>
Description: custom PCB, cusom test bench.<br>
[Flight validation](https://drive.google.com/file/d/17DNDJ1gPmCmDRAwjedCbJ9RXAyqMqqcX/view?usp=sharing).
<img src="img/user/phalko/1.jpg" height=200> <img src="img/user/phalko/2.jpg" height=200> <img src="img/user/phalko/3.jpg" height=200>
---
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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@@ -1,7 +1,7 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Attitude estimation using gyro and accelerometer
// Attitude estimation from gyro and accelerometer
#include "quaternion.h"
#include "vector.h"

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@@ -21,8 +21,8 @@ void setup() {
disableBrownOut();
setupParameters();
setupLED();
setLED(true);
setupMotors();
setLED(true);
setupWiFi();
setupIMU();
setupRC();

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@@ -8,13 +8,12 @@
extern float controlTime;
bool mavlinkConnected = false;
String mavlinkPrintBuffer;
int mavlinkSysId = 1;
Rate telemetryFast(10);
Rate telemetrySlow(2);
bool mavlinkConnected = false;
String mavlinkPrintBuffer;
void processMavlink() {
sendMavlink();
receiveMavlink();
@@ -42,9 +41,9 @@ void sendMavlink() {
}
if (telemetryFast && mavlinkConnected) {
const float offset[] = {0, 0, 0, 0};
const float zeroQuat[] = {0, 0, 0, 0};
mavlink_msg_attitude_quaternion_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
time, attitude.w, attitude.x, -attitude.y, -attitude.z, rates.x, -rates.y, -rates.z, offset); // convert to frd
time, attitude.w, attitude.x, -attitude.y, -attitude.z, rates.x, -rates.y, -rates.z, zeroQuat); // convert to frd
sendMessage(&msg);
mavlink_msg_rc_channels_raw_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, controlTime * 1000, 0,

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

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@@ -6,22 +6,21 @@
#include <Preferences.h>
#include "util.h"
extern int channelZero[16];
extern int channelMax[16];
extern int rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
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;
struct Parameter {
const char *name; // max length is 15
const char *name; // max length is 15 (Preferences key limit)
bool integer;
union { float *f; int *i; }; // pointer to the variable
union { float *f; int *i; }; // pointer to variable
float cache; // what's stored in flash
void (*callback)(); // called after parameter change
Parameter(const char *name, float *variable, void (*callback)() = nullptr) : name(name), integer(false), f(variable), callback(callback) {};
Parameter(const char *name, int *variable, void (*callback)() = nullptr) : name(name), integer(true), i(variable), callback(callback) {};
Parameter(const char *name, float *variable) : name(name), integer(false), f(variable) {};
Parameter(const char *name, int *variable) : name(name), integer(true), i(variable) {};
float getValue() const { return integer ? *i : *f; };
void setValue(const float value) { if (integer) *i = value; else *f = value; };
};
@@ -50,9 +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},
@@ -68,12 +64,12 @@ Parameter parameters[] = {
{"EST_ACC_WEIGHT", &accWeight},
{"EST_RATES_LPF_A", &ratesFilter.alpha},
// motors
{"MOT_PIN_FL", &motorPins[MOTOR_FRONT_LEFT], setupMotors},
{"MOT_PIN_FR", &motorPins[MOTOR_FRONT_RIGHT], setupMotors},
{"MOT_PIN_RL", &motorPins[MOTOR_REAR_LEFT], setupMotors},
{"MOT_PIN_RR", &motorPins[MOTOR_REAR_RIGHT], setupMotors},
{"MOT_PWM_FREQ", &pwmFrequency, setupMotors},
{"MOT_PWM_RES", &pwmResolution, setupMotors},
{"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},
@@ -113,8 +109,7 @@ Parameter parameters[] = {
};
void setupParameters() {
print("Setup parameters\n");
storage.begin("flix");
storage.begin("flix", false);
// Read parameters from storage
for (auto &parameter : parameters) {
if (!storage.isKey(parameter.name)) {
@@ -125,6 +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]);
}
@@ -153,7 +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);
if (parameter.callback) parameter.callback();
afterParameterChange(name, value);
return true;
}
}
@@ -167,7 +167,8 @@ void syncParameters() {
for (auto &parameter : parameters) {
if (parameter.getValue() == parameter.cache) continue; // no change
if (isnan(parameter.getValue()) && isnan(parameter.cache)) continue; // both are NAN
if (isnan(parameter.getValue()) && isnan(parameter.cache)) continue; // both are NaN
if (isinf(parameter.getValue()) && isinf(parameter.cache)) continue; // both are Inf
storage.putFloat(parameter.name, parameter.getValue());
parameter.cache = parameter.getValue(); // update cache

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@@ -9,14 +9,15 @@
SBUS rc(Serial2);
uint16_t channels[16]; // raw rc channels
int channelZero[16]; // calibration zero values
int channelMax[16]; // calibration max values
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 = NAN; // time of the last controls update
int rollChannel = -1, pitchChannel = -1, throttleChannel = -1, yawChannel = -1, modeChannel = -1; // channel mapping
// Channels mapping (nan means not assigned):
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
void setupRC() {
print("Setup RC\n");
@@ -40,11 +41,11 @@ void normalizeRC() {
controls[i] = mapf(channels[i], channelZero[i], channelMax[i], 0, 1);
}
// Update control values
controlRoll = rollChannel < 0 ? 0 : controls[rollChannel];
controlPitch = pitchChannel < 0 ? 0 : controls[pitchChannel];
controlYaw = yawChannel < 0 ? 0 : controls[yawChannel];
controlThrottle = throttleChannel < 0 ? 0 : controls[throttleChannel];
controlMode = modeChannel < 0 ? NAN : controls[modeChannel]; // mode control is ineffective if not mapped
controlRoll = rollChannel >= 0 ? controls[(int)rollChannel] : 0;
controlPitch = pitchChannel >= 0 ? controls[(int)pitchChannel] : 0;
controlYaw = yawChannel >= 0 ? controls[(int)yawChannel] : 0;
controlThrottle = throttleChannel >= 0 ? controls[(int)throttleChannel] : 0;
controlMode = modeChannel >= 0 ? controls[(int)modeChannel] : NAN; // mode switch should not have affect if not set
}
void calibrateRC() {
@@ -63,7 +64,7 @@ void calibrateRC() {
printRCCalibration();
}
void calibrateRCChannel(int *channel, uint16_t in[16], uint16_t out[16], const char *str) {
void calibrateRCChannel(float *channel, uint16_t in[16], uint16_t out[16], const char *str) {
print("%s", str);
pause(3);
for (int i = 0; i < 30; i++) readRC(); // try update 30 times max
@@ -84,15 +85,15 @@ void calibrateRCChannel(int *channel, uint16_t in[16], uint16_t out[16], const c
channelZero[ch] = in[ch];
channelMax[ch] = out[ch];
} else {
*channel = -1;
*channel = NAN;
}
}
void printRCCalibration() {
print("Control Ch Zero Max\n");
print("Roll %-7d%-7d%-7d\n", rollChannel, rollChannel < 0 ? 0 : channelZero[rollChannel], rollChannel < 0 ? 0 : channelMax[rollChannel]);
print("Pitch %-7d%-7d%-7d\n", pitchChannel, pitchChannel < 0 ? 0 : channelZero[pitchChannel], pitchChannel < 0 ? 0 : channelMax[pitchChannel]);
print("Yaw %-7d%-7d%-7d\n", yawChannel, yawChannel < 0 ? 0 : channelZero[yawChannel], yawChannel < 0 ? 0 : channelMax[yawChannel]);
print("Throttle %-7d%-7d%-7d\n", throttleChannel, throttleChannel < 0 ? 0 : channelZero[throttleChannel], throttleChannel < 0 ? 0 : channelMax[throttleChannel]);
print("Mode %-7d%-7d%-7d\n", modeChannel, modeChannel < 0 ? 0 : channelZero[modeChannel], modeChannel < 0 ? 0 : channelMax[modeChannel]);
print("Roll %-7g%-7g%-7g\n", rollChannel, rollChannel >= 0 ? channelZero[(int)rollChannel] : NAN, rollChannel >= 0 ? channelMax[(int)rollChannel] : NAN);
print("Pitch %-7g%-7g%-7g\n", pitchChannel, pitchChannel >= 0 ? channelZero[(int)pitchChannel] : NAN, pitchChannel >= 0 ? channelMax[(int)pitchChannel] : NAN);
print("Yaw %-7g%-7g%-7g\n", yawChannel, yawChannel >= 0 ? channelZero[(int)yawChannel] : NAN, yawChannel >= 0 ? channelMax[(int)yawChannel] : NAN);
print("Throttle %-7g%-7g%-7g\n", throttleChannel, throttleChannel >= 0 ? channelZero[(int)throttleChannel] : NAN, throttleChannel >= 0 ? channelMax[(int)throttleChannel] : NAN);
print("Mode %-7g%-7g%-7g\n", modeChannel, modeChannel >= 0 ? channelZero[(int)modeChannel] : NAN, modeChannel >= 0 ? channelMax[(int)modeChannel] : NAN);
}

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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();
@@ -43,7 +41,7 @@ void doCommand(String str, bool echo);
void handleInput();
void normalizeRC();
void calibrateRC();
void calibrateRCChannel(int *channel, uint16_t zero[16], uint16_t max[16], const char *str);
void calibrateRCChannel(float *channel, uint16_t zero[16], uint16_t max[16], const char *str);
void printRCCalibration();
void printLogHeader();
void printLogData();

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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));
}

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@@ -138,7 +138,7 @@ class Flix:
while True:
try:
msg: Optional[mavlink.MAVLink_message] = self.connection.recv_match(blocking=True)
if msg is None or msg.get_srcSystem() != self.system_id:
if msg is None:
continue
self._connected()
msg_dict = msg.to_dict()