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https://github.com/okalachev/flix.git
synced 2026-06-28 05:56:44 +00:00
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1 Commits
| Author | SHA1 | Date | |
|---|---|---|---|
| b235825f3d |
@@ -77,7 +77,7 @@ Additional articles:
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|Motor|8520 3.7V brushed motor.<br>Motor with exact 3.7V voltage is needed, not ranged working voltage (3.7V — 6V).<br>Make sure the motor shaft diameter and propeller hole diameter match!|<img src="docs/img/motor.jpeg" width=100>|4|
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|Propeller|55 mm (alternatively 65 mm)|<img src="docs/img/prop.jpg" width=100>|4|
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|MOSFET (transistor)|100N03A or [analog](https://t.me/opensourcequadcopter/33)|<img src="docs/img/100n03a.jpg" width=100>|4|
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|Pull-down resistor<br>Voltage measurement resistor|10 kΩ|<img src="docs/img/resistor10k.jpg" width=100>|6|
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|Pull-down resistor|10 kΩ|<img src="docs/img/resistor10k.jpg" width=100>|4|
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|3.7V Li-Po battery|LW 952540 (or any compatible by the size)|<img src="docs/img/battery.jpg" width=100>|1|
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|Battery connector cable|MX2.0 2P female|<img src="docs/img/mx.png" width=100>|1|
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|Li-Po Battery charger|Any|<img src="docs/img/charger.jpg" width=100>|1|
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@@ -154,12 +154,10 @@ You can see a user-contributed [variant of complete circuit diagram](https://mir
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|VIN|VCC (or 3.3V depending on the receiver)|
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|Signal (TX)|GPIO4¹|
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*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.*
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*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.*
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* Optionally connect the battery voltage divider for voltage monitoring to any ADC1 pin (e. g. *GPIO32* on ESP32, *GPIO3* on ESP32S3).
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ESP32 and ESP32S3 [can measure](https://docs.espressif.com/projects/arduino-esp32/en/latest/api/adc.html#analogsetattenuation) up to 3.1 V and ESP32S3/ESP32C3 can measure up to 2.5 V, so choose the voltage divider resistors accordingly.
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## Resources
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* Telegram channel on developing the drone and the flight controller (in Russian): https://t.me/opensourcequadcopter.
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+3
-5
@@ -112,7 +112,7 @@ You can also work with parameters using `p` command in the console. Parameter na
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### Define IMU orientation
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The IMU orientation (relative to the drone's axes) is defined using the parameters: `IMU_ROT_ROLL`, `IMU_ROT_PITCH`, and `IMU_ROT_YAW`.
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Use parameters, to define the IMU board axes orientation relative to the drone's axes: `IMU_ROT_ROLL`, `IMU_ROT_PITCH`, and `IMU_ROT_YAW`.
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The drone has *X* axis pointing forward, *Y* axis pointing left, and *Z* axis pointing up, and the supported IMU boards have *X* axis pointing to the pins side and *Z* axis pointing up from the component side:
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@@ -138,8 +138,6 @@ Before flight you need to calibrate the accelerometer:
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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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Certain ESP32 models (such as ESP32-S3) support a lower maximum PWM frequency; on these boards the parameter `MOT_PWM_FREQ` should be set to 40000 Hz.
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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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@@ -247,7 +245,7 @@ When finished flying, **disarm** the drone, moving the left stick to the bottom
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### Flight modes
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Flight mode is changed using mode switch on the remote control (if configured) or using the console commands. The main flight mode is *STAB*. In order to change modes using SBUS remote control, set the parameters: `CTL_FLT_MODE_0`, `CTL_FLT_MODE_1`, and `CTL_FLT_MODE_2` to required mode numbers (0 for *RAW*, 1 for *ACRO*, 2 for *STAB*, 3 for *AUTO*).
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Flight mode is changed using mode switch on the remote control (if configured) or using the console commands. The main flight mode is *STAB*.
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#### STAB
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@@ -268,7 +266,7 @@ In this mode, the pilot controls the angular rates. This control method is diffi
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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.
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If the pilot moves the control sticks and mode switch is not configured, the drone will switch back to *STAB* mode.
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If the pilot moves the control sticks, the drone will switch back to *STAB* mode.
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## Wi-Fi configuration
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+1
-1
@@ -178,7 +178,7 @@ void doCommand(String str, bool echo = false) {
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String core = systemState[i].xCoreID == tskNO_AFFINITY ? "*" : String(systemState[i].xCoreID);
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int cpuPercentage = systemState[i].ulRunTimeCounter / (totalRunTime / 100);
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print("%-5d%-20s%-7d%-6d%-6s%d\n",systemState[i].xTaskNumber, systemState[i].pcTaskName,
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systemState[i].usStackHighWaterMark, systemState[i].uxCurrentPriority, core.c_str(), cpuPercentage);
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systemState[i].usStackHighWaterMark, systemState[i].uxCurrentPriority, core, cpuPercentage);
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}
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delete[] systemState;
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#endif
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+1
-14
@@ -67,7 +67,7 @@ void control() {
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void interpretControls() {
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if (controlMode < 0.25) mode = flightModes[0];
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else if (controlMode <= 0.75) mode = flightModes[1];
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else if (controlMode < 0.75) mode = flightModes[1];
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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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@@ -149,25 +149,12 @@ void controlTorque() {
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motors[MOTOR_REAR_LEFT] = thrustTarget + torqueTarget.x + torqueTarget.y - torqueTarget.z;
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motors[MOTOR_REAR_RIGHT] = thrustTarget - torqueTarget.x + torqueTarget.y + torqueTarget.z;
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desaturate(motors[MOTOR_FRONT_LEFT], motors[MOTOR_FRONT_RIGHT], motors[MOTOR_REAR_LEFT], motors[MOTOR_REAR_RIGHT]);
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motors[0] = constrain(motors[0], 0, 1);
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motors[1] = constrain(motors[1], 0, 1);
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motors[2] = constrain(motors[2], 0, 1);
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motors[3] = constrain(motors[3], 0, 1);
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}
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void desaturate(float& a, float& b, float& c, float& d) {
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float maxThrust = max(max(a, b), max(c, d));
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if (maxThrust > 1) {
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float diff = maxThrust - 1;
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a -= diff;
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b -= diff;
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c -= diff;
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d -= diff;
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}
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}
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const char* getModeName() {
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switch (mode) {
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case RAW: return "RAW";
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@@ -13,13 +13,11 @@ Quaternion attitude; // estimated attitude
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bool landed;
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float accWeight = 0.003;
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float levelWeight = 0.0002;
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LowPassFilter<Vector> ratesFilter(0.2); // cutoff frequency ~ 40 Hz
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void estimate() {
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applyGyro();
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applyAcc();
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applyLevel();
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}
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void applyGyro() {
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@@ -44,12 +42,3 @@ void applyAcc() {
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// apply correction
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attitude = Quaternion::rotate(attitude, Quaternion::fromRotationVector(correction));
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}
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void applyLevel() {
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if (landed) return;
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// assume the pilot keeps the drone more or less level in flight
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Vector up = Quaternion::rotateVector(Vector(0, 0, 1), attitude);
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Vector correction = Vector::rotationVectorBetween(Vector(0, 0, 1), up) * levelWeight;
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attitude = Quaternion::rotate(attitude, Quaternion::fromRotationVector(correction));
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}
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+1
-1
@@ -18,8 +18,8 @@ extern float motors[4];
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void setup() {
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Serial.begin(115200);
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print("Initializing flix\n");
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disableBrownOut();
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setupParameters();
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setupPower();
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setupLED();
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setLED(true);
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setupMotors();
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+1
-1
@@ -121,7 +121,7 @@ void printIMUInfo() {
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print("model: %s\n", imu.getModel());
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print("who am I: 0x%02X\n", imu.whoAmI());
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print("rate: %.0f\n", loopRate);
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print("gyro: %f %f %f\n", gyro.x, gyro.y, gyro.z);
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print("gyro: %f %f %f\n", rates.x, rates.y, rates.z);
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print("acc: %f %f %f\n", acc.x, acc.y, acc.z);
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imu.waitForData();
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Vector rawGyro, rawAcc;
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+1
-1
@@ -65,7 +65,7 @@ void sendMavlink() {
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sendMessage(&msg);
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mavlink_msg_scaled_imu_pack(mavlinkSysId, MAV_COMP_ID_AUTOPILOT1, &msg, time,
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acc.x / ONE_G * 1000, -acc.y / ONE_G * 1000, -acc.z / ONE_G * 1000, // convert to frd
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acc.x * 1000, -acc.y * 1000, -acc.z * 1000, // convert to frd
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gyro.x * 1000, -gyro.y * 1000, -gyro.z * 1000,
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0, 0, 0, 0);
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sendMessage(&msg);
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@@ -36,16 +36,13 @@ Parameter parameters[] = {
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{"CTL_R_RATE_I", &rollRatePID.i},
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{"CTL_R_RATE_D", &rollRatePID.d},
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{"CTL_R_RATE_WU", &rollRatePID.windup},
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{"CTL_R_RATE_D_A", &rollRatePID.lpf.alpha},
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{"CTL_P_RATE_P", &pitchRatePID.p},
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{"CTL_P_RATE_I", &pitchRatePID.i},
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{"CTL_P_RATE_D", &pitchRatePID.d},
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{"CTL_P_RATE_WU", &pitchRatePID.windup},
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{"CTL_P_RATE_D_A", &pitchRatePID.lpf.alpha},
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{"CTL_Y_RATE_P", &yawRatePID.p},
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{"CTL_Y_RATE_I", &yawRatePID.i},
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{"CTL_Y_RATE_D", &yawRatePID.d},
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{"CTL_Y_RATE_D_A", &yawRatePID.lpf.alpha},
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{"CTL_R_P", &rollPID.p},
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{"CTL_R_I", &rollPID.i},
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{"CTL_R_D", &rollPID.d},
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@@ -73,7 +70,6 @@ Parameter parameters[] = {
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{"IMU_GYRO_BIAS_A", &gyroBiasFilter.alpha},
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// estimate
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{"EST_ACC_WEIGHT", &accWeight},
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{"EST_LVL_WEIGHT", &levelWeight},
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{"EST_RATES_LPF_A", &ratesFilter.alpha},
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// motors
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{"MOT_PIN_FL", &motorPins[MOTOR_FRONT_LEFT], setupMotors},
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@@ -3,8 +3,6 @@
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// Power management
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#include <soc/soc.h>
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#include <soc/rtc_cntl_reg.h>
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#include "lpf.h"
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#include "util.h"
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@@ -13,11 +11,6 @@ LowPassFilter<float> voltageFilter(0.2);
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int voltagePin = -1;
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float voltageScale = 2;
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void setupPower() {
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// Disable reset on low voltage
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REG_CLR_BIT(RTC_CNTL_BROWN_OUT_REG, RTC_CNTL_BROWN_OUT_ENA);
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}
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void readVoltage() {
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if (voltagePin < 0) return;
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static Rate rate(10);
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+2
-2
@@ -37,8 +37,8 @@ void descend() {
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void autoFailsafe() {
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static float roll, pitch, yaw, throttle;
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if (roll != controlRoll || pitch != controlPitch || yaw != controlYaw || abs(throttle - controlThrottle) > 0.05) {
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// controls changed and mode switch is not configured
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if (mode == AUTO && invalid(controlMode)) mode = STAB; // regain control by the pilot
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// controls changed
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if (mode == AUTO) mode = STAB; // regain control by the pilot
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}
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roll = controlRoll;
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pitch = controlPitch;
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@@ -6,6 +6,8 @@
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#pragma once
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#include <math.h>
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#include <soc/soc.h>
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#include <soc/rtc_cntl_reg.h>
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const float ONE_G = 9.80665;
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extern float t;
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@@ -33,6 +35,11 @@ float wrapAngle(float angle) {
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return angle;
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}
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// Disable reset on low voltage
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void disableBrownOut() {
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REG_CLR_BIT(RTC_CNTL_BROWN_OUT_REG, RTC_CNTL_BROWN_OUT_ENA);
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}
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// Trim and split string by spaces
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void splitString(String& str, String& token0, String& token1, String& token2) {
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str.trim();
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+3
-16
@@ -105,23 +105,10 @@ public:
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}
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static Vector rotationVectorBetween(const Vector& a, const Vector& b) {
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float an = a.norm();
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float bn = b.norm();
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if (an < 1e-6 || bn < 1e-6) {
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return Vector(0, 0, 0);
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}
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Vector direction = cross(a, b);
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if (direction.norm() < 1e-6) { // vectors are parallel
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if (dot(a, b) > 0) { // same direction
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return Vector(0, 0, 0);
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}
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// opposite direction
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Vector perp = cross(a, Vector(1, 0, 0));
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if (perp.norm() < 1e-6) {
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perp = cross(a, Vector(0, 1, 0));
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}
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perp.normalize();
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return perp * PI;
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if (direction.zero()) {
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// vectors are opposite, return any perpendicular vector
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return cross(a, Vector(1, 0, 0));
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}
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direction.normalize();
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float angle = angleBetween(a, b);
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@@ -25,7 +25,6 @@ void setupWiFi() {
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} else if (wifiMode == W_STA) {
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WiFi.begin(storage.getString("WIFI_STA_SSID", "").c_str(), storage.getString("WIFI_STA_PASS", "").c_str());
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}
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WiFi.setSleep(false); // disable power save
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udp.begin(udpLocalPort);
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}
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@@ -21,8 +21,6 @@
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#define degrees(rad) ((rad)*RAD_TO_DEG)
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#define constrain(amt,low,high) ((amt)<(low)?(low):((amt)>(high)?(high):(amt)))
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template<typename T> T max(T a, T b) { return a > b ? a : b; }
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template<typename T> T min(T a, T b) { return a < b ? a : b; }
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long map(long x, long in_min, long in_max, long out_min, long out_max) {
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const long run = in_max - in_min;
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@@ -27,13 +27,11 @@ void step();
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void computeLoopRate();
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void applyGyro();
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void applyAcc();
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void applyLevel();
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void control();
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void interpretControls();
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void controlAttitude();
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void controlRates();
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void controlTorque();
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void desaturate(float& a, float& b, float& c, float& d);
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const char* getModeName();
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void sendMotors();
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int getDutyCycle(float value);
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@@ -1,3 +1,4 @@
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// Dummy file to make it possible to compile simulator with Flix' util.h
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#define WRITE_PERI_REG(addr, val) {}
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#define REG_CLR_BIT(_r, _b) {}
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@@ -24,13 +24,13 @@ pip install pyflix
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The API is accessed through the `Flix` class:
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```python
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from pyflix import Flix
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from flix import Flix
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flix = Flix() # create a Flix object and wait for connection
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```
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### Telemetry
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Basic telemetry is available through object properties. The property names generally match the corresponding variables in the firmware code:
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Basic telemetry is available through object properties. The property names generally match the corresponding variables in the firmware itself:
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```python
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print(flix.connected) # True if connected to the drone
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@@ -186,8 +186,7 @@ class Flix:
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self._trigger('motors', self.motors)
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if isinstance(msg, mavlink.MAVLink_scaled_imu_message):
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ONE_G = 9.80665
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self.acc = self._mavlink_to_flu([msg.xacc * ONE_G / 1000, msg.yacc * ONE_G / 1000, msg.zacc * ONE_G / 1000])
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self.acc = self._mavlink_to_flu([msg.xacc / 1000, msg.yacc / 1000, msg.zacc / 1000])
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self.gyro = self._mavlink_to_flu([msg.xgyro / 1000, msg.ygyro / 1000, msg.zgyro / 1000])
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self._trigger('acc', self.acc)
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self._trigger('gyro', self.gyro)
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@@ -1,6 +1,6 @@
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[project]
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name = "pyflix"
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version = "0.14"
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version = "0.11"
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description = "Python API for Flix drone"
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authors = [{ name="Oleg Kalachev", email="okalachev@gmail.com" }]
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license = "MIT"
|
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|
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