11 Commits

Author SHA1 Message Date
Oleg Kalachev b235825f3d Implement battery voltage monitoring
Add power subsystem.
Add PWR_VOLT_PIN, PWR_VOLT_SCALE, PWR_VOLT_LPF_A parameters.
Support BATTERY_STATUS mavlink messages streaming.
Add pw cli command.
Add voltage field to pyflix library.
2026-04-21 05:18:52 +03:00
Oleg Kalachev d8591ea2a9 Fix working with parameters in pyflix examples
PITCH_P parameter was renamed to CTL_P_P
2026-04-18 05:23:47 +03:00
Oleg Kalachev c434107eaf Add parameter for configuring sbus pin number, disable sbus by default 2026-03-27 00:56:34 +03:00
Oleg Kalachev 814427dbfd Minor docs change 2026-03-27 00:40:19 +03:00
Oleg Kalachev 0730ceeffa Add new user builds 2026-02-21 07:12:36 +03:00
Oleg Kalachev a687303062 Make motor parameters apply without reboot
Add callback to parameter definition to call after parameter is changed.
2026-02-19 04:56:12 +03:00
Oleg Kalachev b2daf2587f Minor parameters code simplifications
readOnly is false by default
INFINITY == INFINITY, so remove redundant check
2026-02-19 02:59:38 +03:00
Oleg Kalachev a8c25d8ac0 Minor updates to usage article 2026-02-04 17:52:23 +03:00
Oleg Kalachev 3e49d41986 Make rc channel numbers and calibration params use int instead of float
As parameter subsystems supports int now, and int is much more natural here.
2026-02-02 20:36:22 +03:00
Oleg Kalachev 67430c7aac Several minor changes 2026-02-02 18:46:36 +03:00
Oleg Kalachev 3631743a29 Drop messages from another systems in pyflix
We shouldn't pass messages where system id != our system id. 
This change may be useful when there are many drones in one network.
2026-02-02 18:28:20 +03:00
25 changed files with 162 additions and 79 deletions
+2
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@@ -156,6 +156,8 @@ You can see a user-contributed [variant of complete circuit diagram](https://mir
*¹ — UART2 RX pin was [changed](https://docs.espressif.com/projects/arduino-esp32/en/latest/migration_guides/2.x_to_3.0.html#id14) to GPIO4 in Arduino ESP32 core 3.0.*
* Optionally connect the battery voltage divider for voltage monitoring to any ADC1 pin (e. g. *GPIO32* on ESP32, *GPIO3* on ESP32S3).
## Resources
* Telegram channel on developing the drone and the flight controller (in Russian): https://t.me/opensourcequadcopter.
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+4 -2
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@@ -13,7 +13,7 @@ Do the following:
Do the following:
* **Check the battery voltage**. Use a multimeter to measure the battery voltage. It should be in range of 3.7-4.2 V.
* **Check if there are some startup errors**. Connect the ESP32 to the computer and check the Serial Monitor output. Use the Reset button to make sure you see the whole ESP32 startup output.
* **Check if there are some startup errors**. Connect the ESP32 to the computer and check the Serial Monitor output. Use the Reset button or `reboot` command to see the whole startup output.
* **Check the baudrate is correct**. If you see garbage characters in the Serial Monitor, make sure the baudrate is set to 115200.
* **Make sure correct IMU model is chosen**. If using ICM-20948/MPU-6050 board, change `MPU9250` to `ICM20948`/`MPU6050` in the `imu.ino` file.
* **Check if the console is working**. Perform `help` command in Serial Monitor. You should see the list of available commands. You can also access the console using QGroundControl *(Vehicle Setup**Analyze Tools**MAVLink Console)*.
@@ -35,5 +35,7 @@ Do the following:
* **Check the propeller directions are correct**. Make sure your propeller types (A or B) are installed as on the picture:
<img src="img/user/peter_ukhov-2/1.jpg" width="200">
* **Check the remote control**. Using `rc` command, check the control values reflect your sticks movement. All the controls should change between -1 and 1, and throttle between 0 and 1.
* If using SBUS receiver, **calibrate the RC**. Type `cr` command in Serial Monitor and follow the instructions.
* **If using SBUS receiver**:
* **Define the used GPIO pin** in `RC_RX_PIN` parameter.
* **Calibrate the RC** using `cr` command in the console.
* **Check the IMU output using QGroundControl**. Connect to the drone using QGroundControl on your computer. Go to the *Analyze* tab, *MAVLINK Inspector*. Plot the data from the `SCALED_IMU` message. The gyroscope and accelerometer data should change according to the drone movement.
+28 -17
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@@ -143,32 +143,41 @@ 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
### Battery voltage monitoring
1. Check the IMU is working: perform `imu` command and check its output:
ESP32 ADC can measure only up to 3.3 V, so you need to use a voltage divider to monitor the battery voltage. To enable voltage measurement, set the following parameters:
1. `PWR_VOLT_PIN` — GPIO pin number where the voltage divider is connected (*-1* to disable).
2. `PWR_VOLT_SCALE` — voltage divider coefficient (*2* for two equal resistors).
After this setup, you should see the battery voltage in QGroundControl top panel or using `pw` command in the console.
### Important: check everything works
1. Check the IMU is working: perform `imu` command in the console and check the 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 in the console. Use the following commands **— remove the propellers before running the tests!**
3. Perform motor tests. Use the following commands **— remove the propellers before running the tests!**
* `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).
* `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).
Rotation diagram:
Make sure rotation directions and propeller types match the following diagram:
<img src="img/motors.svg" width=200>
@@ -193,11 +202,13 @@ There are several ways to control the drone's flight: using **smartphone** (Wi-F
### Control with a remote control
Before using remote SBUS-connected remote control, you need to calibrate it:
Before using SBUS-connected remote control you need to enable SBUS and calibrate it:
1. Access the console using QGroundControl (recommended) or Serial Monitor.
2. Type `cr` command and follow the instructions.
3. Use the remote control to fly the drone!
1. Connect to the drone using QGroundControl.
2. In parameters, set the `RC_RX_PIN` parameter to the GPIO pin number where the SBUS signal is connected, for example: 4. Negative value disables SBUS.
3. Reboot the drone to apply changes.
4. Open the console, type `cr` command and follow the instructions to calibrate the remote control.
5. Use the remote control to fly the drone!
### Control with a USB remote control
@@ -234,11 +245,11 @@ 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 or using the command line.
Flight mode is changed using mode switch on the remote control (if configured) or using the console commands. The main flight mode is *STAB*.
#### STAB
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.
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.
@@ -253,7 +264,7 @@ 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, if configured). The drone can be controlled using [pyflix](../tools/pyflix/) Python library, or by modifying the firmware to implement the needed autonomous behavior.
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.
If the pilot moves the control sticks, the drone will switch back to *STAB* mode.
+16
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@@ -4,6 +4,22 @@ 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.
+4 -3
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@@ -16,6 +16,7 @@ extern float controlTime;
extern int mode;
extern bool armed;
extern LowPassFilter<Vector> gyroBiasFilter;
extern float voltage;
const char* motd =
"\nWelcome to\n"
@@ -39,6 +40,7 @@ const char* motd =
"disarm - disarm the drone\n"
"raw/stab/acro/auto - set mode\n"
"rc - show RC data\n"
"pw - show power info\n"
"wifi - show Wi-Fi info\n"
"ap <ssid> <password> - setup Wi-Fi access point\n"
"sta <ssid> <password> - setup Wi-Fi client mode\n"
@@ -46,7 +48,6 @@ const char* motd =
"log [dump] - print log header [and data]\n"
"cr - calibrate RC\n"
"ca - calibrate accel\n"
"cl - calibrate level\n"
"mfr, mfl, mrr, mrl - test motor (remove props)\n"
"sys - show system info\n"
"reset - reset drone's state\n"
@@ -136,6 +137,8 @@ void doCommand(String str, bool echo = false) {
print("time: %.1f\n", controlTime);
print("mode: %s\n", getModeName());
print("armed: %d\n", armed);
} else if (command == "pw") {
print("Voltage: %.1f V\n", voltage);
} else if (command == "wifi") {
printWiFiInfo();
} else if (command == "ap") {
@@ -152,8 +155,6 @@ void doCommand(String str, bool echo = false) {
calibrateRC();
} else if (command == "ca") {
calibrateAccel();
} else if (command == "cl") {
calibrateLevel();
} else if (command == "mfr") {
testMotor(MOTOR_FRONT_RIGHT);
} else if (command == "mfl") {
+1 -1
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@@ -1,7 +1,7 @@
// Copyright (c) 2023 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Attitude estimation from gyro and accelerometer
// Attitude estimation using gyro and accelerometer
#include "quaternion.h"
#include "vector.h"
+2 -1
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@@ -21,8 +21,8 @@ void setup() {
disableBrownOut();
setupParameters();
setupLED();
setupMotors();
setLED(true);
setupMotors();
setupWiFi();
setupIMU();
setupRC();
@@ -39,6 +39,7 @@ void loop() {
sendMotors();
handleInput();
processMavlink();
readVoltage();
logData();
syncParameters();
}
-8
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@@ -110,14 +110,6 @@ void calibrateAccelOnce() {
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() {
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);
+13 -4
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@@ -7,13 +7,15 @@
#include "util.h"
extern float controlTime;
extern float voltage;
bool mavlinkConnected = false;
String mavlinkPrintBuffer;
int mavlinkSysId = 1;
Rate telemetryFast(10);
Rate telemetrySlow(2);
bool mavlinkConnected = false;
String mavlinkPrintBuffer;
void processMavlink() {
sendMavlink();
receiveMavlink();
@@ -38,12 +40,19 @@ void sendMavlink() {
mavlink_msg_extended_sys_state_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg,
MAV_VTOL_STATE_UNDEFINED, landed ? MAV_LANDED_STATE_ON_GROUND : MAV_LANDED_STATE_IN_AIR);
sendMessage(&msg);
uint16_t voltages[] = {voltage * 1000, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX, UINT16_MAX};
uint16_t voltagesExt[] = {0, 0, 0, 0};
float remaining = constrain(mapf(voltage, 3.4, 4.2, 0, 1), 0, 1);
mavlink_msg_battery_status_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, 0, MAV_BATTERY_FUNCTION_ALL,
MAV_BATTERY_TYPE_LIPO, INT16_MAX, voltages, -1, -1, -1, remaining * 100, 0, MAV_BATTERY_CHARGE_STATE_OK, voltagesExt, 0, 0);
sendMessage(&msg);
}
if (telemetryFast && mavlinkConnected) {
const float zeroQuat[] = {0, 0, 0, 0};
const float offset[] = {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, zeroQuat); // convert to frd
time, attitude.w, attitude.x, -attitude.y, -attitude.z, rates.x, -rates.y, -rates.z, offset); // convert to frd
sendMessage(&msg);
mavlink_msg_rc_channels_raw_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, controlTime * 1000, 0,
+1
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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); // when reconfiguring
}
sendMotors();
print("Motors initialized\n");
+27 -16
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@@ -6,21 +6,26 @@
#include <Preferences.h>
#include "util.h"
extern float channelZero[16];
extern float channelMax[16];
extern float rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
extern int channelZero[16];
extern int channelMax[16];
extern int rollChannel, pitchChannel, throttleChannel, yawChannel, armedChannel, modeChannel;
extern int rcRxPin;
extern int wifiMode, udpLocalPort, udpRemotePort;
extern float rcLossTimeout, descendTime;
extern int voltagePin;
extern float voltageScale;
extern LowPassFilter<float> voltageFilter;
Preferences storage;
struct Parameter {
const char *name; // max length is 15 (Preferences key limit)
const char *name; // max length is 15
bool integer;
union { float *f; int *i; }; // pointer to variable
union { float *f; int *i; }; // pointer to the variable
float cache; // what's stored in flash
Parameter(const char *name, float *variable) : name(name), integer(false), f(variable) {};
Parameter(const char *name, int *variable) : name(name), integer(true), i(variable) {};
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) {};
float getValue() const { return integer ? *i : *f; };
void setValue(const float value) { if (integer) *i = value; else *f = value; };
};
@@ -67,16 +72,17 @@ Parameter parameters[] = {
{"EST_ACC_WEIGHT", &accWeight},
{"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_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_PWM_STOP", &pwmStop},
{"MOT_PWM_MIN", &pwmMin},
{"MOT_PWM_MAX", &pwmMax},
// rc
{"RC_RX_PIN", &rcRxPin},
{"RC_ZERO_0", &channelZero[0]},
{"RC_ZERO_1", &channelZero[1]},
{"RC_ZERO_2", &channelZero[2]},
@@ -106,13 +112,18 @@ Parameter parameters[] = {
{"MAV_SYS_ID", &mavlinkSysId},
{"MAV_RATE_SLOW", &telemetrySlow.rate},
{"MAV_RATE_FAST", &telemetryFast.rate},
// power
{"PWR_VOLT_PIN", &voltagePin},
{"PWR_VOLT_SCALE", &voltageScale},
{"PWR_VOLT_LPF_A", &voltageFilter.alpha},
// safety
{"SF_RC_LOSS_TIME", &rcLossTimeout},
{"SF_DESCEND_TIME", &descendTime},
};
void setupParameters() {
storage.begin("flix", false);
print("Setup parameters\n");
storage.begin("flix");
// Read parameters from storage
for (auto &parameter : parameters) {
if (!storage.isKey(parameter.name)) {
@@ -151,6 +162,7 @@ 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();
return true;
}
}
@@ -164,8 +176,7 @@ 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 (isinf(parameter.getValue()) && isinf(parameter.cache)) continue; // both are Inf
if (isnan(parameter.getValue()) && isnan(parameter.cache)) continue; // both are NAN
storage.putFloat(parameter.name, parameter.getValue());
parameter.cache = parameter.getValue(); // update cache
+21
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@@ -0,0 +1,21 @@
// Copyright (c) 2026 Oleg Kalachev <okalachev@gmail.com>
// Repository: https://github.com/okalachev/flix
// Power management
#include "lpf.h"
#include "util.h"
float voltage;
LowPassFilter<float> voltageFilter(0.2);
int voltagePin = -1;
float voltageScale = 2;
void readVoltage() {
if (voltagePin < 0) return;
static Rate rate(10);
if (!rate) return;
float v = analogReadMilliVolts(voltagePin) * voltageScale / 1000.0f;
voltage = voltageFilter.update(v);
}
+23 -17
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@@ -7,24 +7,26 @@
#include "util.h"
SBUS rc(Serial2);
int rcRxPin = -1; // -1 means disabled
uint16_t channels[16]; // raw rc channels
float channelZero[16]; // calibration zero values
float channelMax[16]; // calibration max values
int channelZero[16]; // calibration zero values
int 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
// Channels mapping (nan means not assigned):
float rollChannel = NAN, pitchChannel = NAN, throttleChannel = NAN, yawChannel = NAN, modeChannel = NAN;
int rollChannel = -1, pitchChannel = -1, throttleChannel = -1, yawChannel = -1, modeChannel = -1; // channel mapping
void setupRC() {
if (rcRxPin < 0) return;
print("Setup RC\n");
rc.begin();
rc.begin(rcRxPin);
}
bool readRC() {
if (rcRxPin < 0) return false;
if (rc.read()) {
SBUSData data = rc.data();
for (int i = 0; i < 16; i++) channels[i] = data.ch[i]; // copy channels data
@@ -41,14 +43,18 @@ void normalizeRC() {
controls[i] = mapf(channels[i], channelZero[i], channelMax[i], 0, 1);
}
// Update control values
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
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
}
void calibrateRC() {
if (rcRxPin < 0) {
print("RC_RX_PIN = %d, set the RC pin!\n", rcRxPin);
return;
}
uint16_t zero[16];
uint16_t center[16];
uint16_t max[16];
@@ -64,7 +70,7 @@ void calibrateRC() {
printRCCalibration();
}
void calibrateRCChannel(float *channel, uint16_t in[16], uint16_t out[16], const char *str) {
void calibrateRCChannel(int *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
@@ -85,15 +91,15 @@ void calibrateRCChannel(float *channel, uint16_t in[16], uint16_t out[16], const
channelZero[ch] = in[ch];
channelMax[ch] = out[ch];
} else {
*channel = NAN;
*channel = -1;
}
}
void printRCCalibration() {
print("Control Ch Zero Max\n");
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);
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]);
}
+2
View File
@@ -165,6 +165,8 @@ 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; }
uint32_t analogReadMilliVolts(uint8_t pin) { return 0; }
unsigned long __micros;
unsigned long __resetTime = 0;
+1 -1
View File
@@ -13,7 +13,7 @@ class SBUS {
public:
SBUS(HardwareSerial& bus, const bool inv = true) {};
SBUS(HardwareSerial& bus, const int8_t rxpin, const int8_t txpin, const bool inv = true) {};
void begin() {};
void begin(int rxpin = -1, int txpin = -1, bool inv = true, bool fast = false) {};
bool read() { return joystickInit(); };
SBUSData data() {
SBUSData data;
+1 -2
View File
@@ -43,7 +43,7 @@ void doCommand(String str, bool echo);
void handleInput();
void normalizeRC();
void calibrateRC();
void calibrateRCChannel(float *channel, uint16_t zero[16], uint16_t max[16], const char *str);
void calibrateRCChannel(int *channel, uint16_t zero[16], uint16_t max[16], const char *str);
void printRCCalibration();
void printLogHeader();
void printLogData();
@@ -71,7 +71,6 @@ void resetParameters();
void setLED(bool on) {};
void calibrateGyro() { print("Skip gyro calibrating\n"); };
void calibrateAccel() { print("Skip accel calibrating\n"); };
void calibrateLevel() { print("Skip level calibrating\n"); };
void printIMUCalibration() { print("cal: N/A\n"); };
void printIMUInfo() {};
void printWiFiInfo() {};
+1
View File
@@ -27,6 +27,7 @@
#include "mavlink.ino"
#include "motors.ino"
#include "parameters.ino"
#include "power.ino"
#include "rc.ino"
#include "time.ino"
+4 -3
View File
@@ -10,6 +10,7 @@ print('Connected:', flix.connected)
print('Mode:', flix.mode)
print('Armed:', flix.armed)
print('Landed:', flix.landed)
print('Voltage:', flix.voltage, 'V')
print('Rates:', *[f'{math.degrees(r):.0f}°/s' for r in flix.rates])
print('Attitude:', *[f'{math.degrees(a):.0f}°' for a in flix.attitude_euler])
print('Motors:', flix.motors)
@@ -23,11 +24,11 @@ print('> imu')
print(flix.cli('imu'))
print('=== Get parameter...')
pitch_p = flix.get_param('PITCH_P')
print('PITCH_P = ', pitch_p)
pitch_p = flix.get_param('CTL_P_P')
print('CTL_P_P = ', pitch_p)
print('=== Set parameter...')
flix.set_param('PITCH_P', pitch_p)
flix.set_param('CTL_P_P', pitch_p)
print('=== Wait for gyro update...')
print('Gyro: ', flix.wait('gyro'))
+4 -2
View File
@@ -37,6 +37,7 @@ print(flix.connected) # True if connected to the drone
print(flix.mode) # current flight mode (str)
print(flix.armed) # True if the drone is armed
print(flix.landed) # True if the drone is landed
print(flix.voltage) # battery voltage
print(flix.attitude) # attitude quaternion [w, x, y, z]
print(flix.attitude_euler) # attitude as Euler angles [roll, pitch, yaw]
print(flix.rates) # angular rates [roll_rate, pitch_rate, yaw_rate]
@@ -95,6 +96,7 @@ Full list of events:
|`armed`|Armed state update|Armed state *(bool)*|
|`mode`|Flight mode update|Flight mode *(str)*|
|`landed`|Landed state update|Landed state *(bool)*|
|`voltage`|Battery voltage update|Voltage *(float)*|
|`print`|The drone prints text to the console|Text|
|`attitude`|Attitude update|Attitude quaternion *(list)*|
|`attitude_euler`|Attitude update|Euler angles *(list)*|
@@ -117,8 +119,8 @@ Full list of events:
Get and set firmware parameters using `get_param` and `set_param` methods:
```python
pitch_p = flix.get_param('PITCH_P') # get parameter value
flix.set_param('PITCH_P', 5) # set parameter value
pitch_p = flix.get_param('CTL_P_P') # get parameter value
flix.set_param('CTL_P_P', 5) # set parameter value
```
Execute console commands using `cli` method. This method returns the command response:
+7 -2
View File
@@ -26,6 +26,7 @@ class Flix:
mode: str = ''
armed: bool = False
landed: bool = False
voltage: float = 0
attitude: List[float]
attitude_euler: List[float] # roll, pitch, yaw
rates: List[float]
@@ -68,7 +69,7 @@ class Flix:
self._heartbeat_thread.start()
if wait_connection:
self.wait('mavlink.HEARTBEAT')
time.sleep(0.2) # give some time to receive initial state
time.sleep(0.6) # give some time to receive initial state
def _init_state(self):
self.attitude = [1, 0, 0, 0]
@@ -138,7 +139,7 @@ class Flix:
while True:
try:
msg: Optional[mavlink.MAVLink_message] = self.connection.recv_match(blocking=True)
if msg is None:
if msg is None or msg.get_srcSystem() != self.system_id:
continue
self._connected()
msg_dict = msg.to_dict()
@@ -190,6 +191,10 @@ class Flix:
self._trigger('acc', self.acc)
self._trigger('gyro', self.gyro)
if isinstance(msg, mavlink.MAVLink_battery_status_message):
self.voltage = msg.voltages[0] / 1000
self._trigger('voltage', self.voltage)
if isinstance(msg, mavlink.MAVLink_serial_control_message):
# new chunk of data
text = bytes(msg.data)[:msg.count].decode('utf-8', errors='ignore')