int32_t calculateAltHoldThrottleAdjustment(int32_t vel_tmp, float accZ_tmp, float accZ_old)
{
int32_t result = 0;
int32_t error;
int32_t setVel;
if (!isThrustFacingDownwards(&attitude)) {
return result;
}
// Altitude P-Controller
if (!velocityControl) {
error = constrain(AltHold - EstAlt, -500, 500);
error = applyDeadband(error, 10); // remove small P parameter to reduce noise near zero position
setVel = constrain((pidProfile()->P8[PIDALT] * error / 128), -300, +300); // limit velocity to +/- 3 m/s
} else {
setVel = setVelocity;
}
// Velocity PID-Controller
// P
error = setVel - vel_tmp;
result = constrain((pidProfile()->P8[PIDVEL] * error / 32), -300, +300);
// I
errorVelocityI += (pidProfile()->I8[PIDVEL] * error);
errorVelocityI = constrain(errorVelocityI, -(8192 * 200), (8192 * 200));
result += errorVelocityI / 8192; // I in range +/-200
// D
result -= constrain(pidProfile()->D8[PIDVEL] * (accZ_tmp + accZ_old) / 512, -150, 150);
return result;
}
static long cmsx_FilterPerProfileRead(void)
{
cmsx_dterm_lpf_hz = pidProfile()->dterm_lpf_hz;
cmsx_gyroSoftLpf = gyroConfig()->gyro_soft_lpf_hz;
cmsx_yaw_p_limit = pidProfile()->yaw_p_limit;
cmsx_yaw_lpf_hz = pidProfile()->yaw_lpf_hz;
return 0;
}
static long cmsx_profileOtherOnEnter(void)
{
profileIndexString[1] = '0' + tmpProfileIndex;
cmsx_dtermSetpointWeight = pidProfile()->dtermSetpointWeight;
cmsx_setpointRelaxRatio = pidProfile()->setpointRelaxRatio;
cmsx_angleStrength = pidProfile()[PIDLEVEL].P;
cmsx_horizonStrength = pidProfile()[PIDLEVEL].I;
cmsx_horizonTransition = pidProfile()[PIDLEVEL].D;
return 0;
}
static void activateConfig(void)
{
activateControlRateConfig();
resetAdjustmentStates();
useRcControlsConfig(modeActivationProfile()->modeActivationConditions);
pidInitFilters(pidProfile());
#ifdef GPS
gpsUsePIDs(pidProfile());
#endif
useFailsafeConfig();
setAccelerationTrims(&sensorTrims()->accZero);
accelerationFilterInit(accelerometerConfig()->acc_cut_hz);
#ifdef USE_SERVOS
mixerUseConfigs(servoProfile()->servoConf);
#endif
#ifdef GPS
recalculateMagneticDeclination();
#endif
#ifdef VTX
initVTXState();
#endif
static imuRuntimeConfig_t imuRuntimeConfig;
imuRuntimeConfig.dcm_kp = imuConfig()->dcm_kp / 10000.0f;
imuRuntimeConfig.dcm_ki = imuConfig()->dcm_ki / 10000.0f;
imuRuntimeConfig.acc_cut_hz = accelerometerConfig()->acc_cut_hz;
imuRuntimeConfig.acc_unarmedcal = accelerometerConfig()->acc_unarmedcal;
imuRuntimeConfig.small_angle = imuConfig()->small_angle;
imuConfigure(
&imuRuntimeConfig,
&accelerometerConfig()->accDeadband,
accelerometerConfig()->accz_lpf_cutoff,
throttleCorrectionConfig()->throttle_correction_angle
);
}
void init_Gtune(void)
{
uint8_t i;
if (pidProfile()->pidController == 2) {
floatPID = true; // LuxFloat is using float values for PID settings
} else {
floatPID = false;
}
updateDelayCycles();
for (i = 0; i < 3; i++) {
if ((gtuneConfig()->gtune_hilimP[i] && gtuneConfig()->gtune_lolimP[i] > gtuneConfig()->gtune_hilimP[i]) || (motorCount < 4 && i == FD_YAW)) { // User config error disable axisis for tuning
gtuneConfig()->gtune_hilimP[i] = 0; // Disable YAW tuning for everything below a quadcopter
}
if(pidProfile()->P8[i] < gtuneConfig()->gtune_lolimP[i]) {
pidProfile()->P8[i] = gtuneConfig()->gtune_lolimP[i];
}
result_P64[i] = (int16_t)pidProfile()->P8[i] << 6; // 6 bit extra resolution for P.
OldError[i] = 0;
time_skip[i] = delay_cycles;
}
}
void updateMagHold(void)
{
if (ABS(rcCommand[YAW]) < 15 && FLIGHT_MODE(MAG_MODE)) {
int16_t dif = DECIDEGREES_TO_DEGREES(attitude.values.yaw) - magHold;
if (dif <= -180)
dif += 360;
if (dif >= +180)
dif -= 360;
dif *= -rcControlsConfig()->yaw_control_direction;
if (STATE(SMALL_ANGLE))
rcCommand[YAW] -= dif * pidProfile()->P8[PIDMAG] / 30; // 18 deg
} else
magHold = DECIDEGREES_TO_DEGREES(attitude.values.yaw);
}
void subTaskPidController(void)
{
const uint32_t startTime = micros();
// PID - note this is function pointer set by setPIDController()
pidLuxFloat(
pidProfile(),
currentControlRateProfile,
imuConfig()->max_angle_inclination,
&accelerometerConfig()->accelerometerTrims,
rxConfig()
);
if (debugMode == DEBUG_PIDLOOP) {debug[2] = micros() - startTime;}
}
void annexCode(void)
{
int32_t tmp, tmp2;
int32_t axis, prop1 = 0, prop2;
// PITCH & ROLL only dynamic PID adjustment, depending on throttle value
if (rcData[THROTTLE] < currentControlRateProfile->tpa_breakpoint) {
prop2 = 100;
} else {
if (rcData[THROTTLE] < 2000) {
prop2 = 100 - (uint16_t)currentControlRateProfile->dynThrPID * (rcData[THROTTLE] - currentControlRateProfile->tpa_breakpoint) / (2000 - currentControlRateProfile->tpa_breakpoint);
} else {
prop2 = 100 - currentControlRateProfile->dynThrPID;
}
}
for (axis = 0; axis < 3; axis++) {
tmp = MIN(ABS(rcData[axis] - rxConfig()->midrc), 500);
if (axis == ROLL || axis == PITCH) {
if (rcControlsConfig()->deadband) {
if (tmp > rcControlsConfig()->deadband) {
tmp -= rcControlsConfig()->deadband;
} else {
tmp = 0;
}
}
tmp2 = tmp / 100;
rcCommand[axis] = lookupPitchRollRC[tmp2] + (tmp - tmp2 * 100) * (lookupPitchRollRC[tmp2 + 1] - lookupPitchRollRC[tmp2]) / 100;
prop1 = 100 - (uint16_t)currentControlRateProfile->rates[axis] * tmp / 500;
prop1 = (uint16_t)prop1 * prop2 / 100;
} else if (axis == YAW) {
if (rcControlsConfig()->yaw_deadband) {
if (tmp > rcControlsConfig()->yaw_deadband) {
tmp -= rcControlsConfig()->yaw_deadband;
} else {
tmp = 0;
}
}
tmp2 = tmp / 100;
rcCommand[axis] = (lookupYawRC[tmp2] + (tmp - tmp2 * 100) * (lookupYawRC[tmp2 + 1] - lookupYawRC[tmp2]) / 100) * -rcControlsConfig()->yaw_control_direction;
prop1 = 100 - (uint16_t)currentControlRateProfile->rates[axis] * ABS(tmp) / 500;
}
// FIXME axis indexes into pids. use something like lookupPidIndex(rc_alias_e alias) to reduce coupling.
dynP8[axis] = (uint16_t)pidProfile()->P8[axis] * prop1 / 100;
dynI8[axis] = (uint16_t)pidProfile()->I8[axis] * prop1 / 100;
dynD8[axis] = (uint16_t)pidProfile()->D8[axis] * prop1 / 100;
// non coupled PID reduction scaler used in PID controller 1 and PID controller 2. YAW TPA disabled. 100 means 100% of the pids
if (axis == YAW) {
PIDweight[axis] = 100;
}
else {
PIDweight[axis] = prop2;
}
if (rcData[axis] < rxConfig()->midrc)
rcCommand[axis] = -rcCommand[axis];
}
tmp = constrain(rcData[THROTTLE], rxConfig()->mincheck, PWM_RANGE_MAX);
tmp = (uint32_t)(tmp - rxConfig()->mincheck) * PWM_RANGE_MIN / (PWM_RANGE_MAX - rxConfig()->mincheck); // [MINCHECK;2000] -> [0;1000]
tmp2 = tmp / 100;
rcCommand[THROTTLE] = lookupThrottleRC[tmp2] + (tmp - tmp2 * 100) * (lookupThrottleRC[tmp2 + 1] - lookupThrottleRC[tmp2]) / 100; // [0;1000] -> expo -> [MINTHROTTLE;MAXTHROTTLE]
if (FLIGHT_MODE(HEADFREE_MODE)) {
float radDiff = degreesToRadians(DECIDEGREES_TO_DEGREES(attitude.values.yaw) - headFreeModeHold);
float cosDiff = cos_approx(radDiff);
float sinDiff = sin_approx(radDiff);
int16_t rcCommand_PITCH = rcCommand[PITCH] * cosDiff + rcCommand[ROLL] * sinDiff;
rcCommand[ROLL] = rcCommand[ROLL] * cosDiff - rcCommand[PITCH] * sinDiff;
rcCommand[PITCH] = rcCommand_PITCH;
}
if (ARMING_FLAG(ARMED)) {
LED0_ON;
} else {
if (IS_RC_MODE_ACTIVE(BOXARM) == 0) {
ENABLE_ARMING_FLAG(OK_TO_ARM);
}
if (!imuIsAircraftArmable(armingConfig()->max_arm_angle)) {
DISABLE_ARMING_FLAG(OK_TO_ARM);
debug[3] = ARMING_FLAG(OK_TO_ARM);
}
if (isCalibrating() || isSystemOverloaded()) {
warningLedFlash();
DISABLE_ARMING_FLAG(OK_TO_ARM);
} else {
if (ARMING_FLAG(OK_TO_ARM)) {
warningLedDisable();
} else {
warningLedFlash();
}
}
debug[3] = ARMING_FLAG(OK_TO_ARM);
warningLedUpdate();
}
// Read out gyro temperature. can use it for something somewhere. maybe get MCU temperature instead? lots of fun possibilities.
if (gyro.temperature)
gyro.temperature(&telemTemperature1);
}
void init(void)
{
drv_pwm_config_t pwm_params;
printfSupportInit();
initEEPROM();
ensureEEPROMContainsValidData();
readEEPROM();
systemState |= SYSTEM_STATE_CONFIG_LOADED;
#ifdef STM32F303
// start fpu
SCB->CPACR = (0x3 << (10*2)) | (0x3 << (11*2));
#endif
#ifdef STM32F303xC
SetSysClock();
#endif
#ifdef STM32F10X
// Configure the System clock frequency, HCLK, PCLK2 and PCLK1 prescalers
// Configure the Flash Latency cycles and enable prefetch buffer
SetSysClock(systemConfig()->emf_avoidance);
#endif
i2cSetOverclock(systemConfig()->i2c_highspeed);
systemInit();
#ifdef USE_HARDWARE_REVISION_DETECTION
detectHardwareRevision();
#endif
// Latch active features to be used for feature() in the remainder of init().
latchActiveFeatures();
// initialize IO (needed for all IO operations)
IOInitGlobal();
debugMode = debugConfig()->debug_mode;
#ifdef USE_EXTI
EXTIInit();
#endif
#ifdef ALIENFLIGHTF3
if (hardwareRevision == AFF3_REV_1) {
ledInit(false);
} else {
ledInit(true);
}
#else
ledInit(false);
#endif
#ifdef BEEPER
beeperConfig_t beeperConfig = {
.gpioPeripheral = BEEP_PERIPHERAL,
.gpioPin = BEEP_PIN,
.gpioPort = BEEP_GPIO,
#ifdef BEEPER_INVERTED
.gpioMode = Mode_Out_PP,
.isInverted = true
#else
.gpioMode = Mode_Out_OD,
.isInverted = false
#endif
};
#ifdef NAZE
if (hardwareRevision >= NAZE32_REV5) {
// naze rev4 and below used opendrain to PNP for buzzer. Rev5 and above use PP to NPN.
beeperConfig.gpioMode = Mode_Out_PP;
beeperConfig.isInverted = true;
}
#endif
beeperInit(&beeperConfig);
#endif
#ifdef BUTTONS
buttonsInit();
if (!isMPUSoftReset()) {
buttonsHandleColdBootButtonPresses();
}
#endif
#ifdef SPEKTRUM_BIND
if (feature(FEATURE_RX_SERIAL)) {
switch (rxConfig()->serialrx_provider) {
case SERIALRX_SPEKTRUM1024:
case SERIALRX_SPEKTRUM2048:
// Spektrum satellite binding if enabled on startup.
// Must be called before that 100ms sleep so that we don't lose satellite's binding window after startup.
// The rest of Spektrum initialization will happen later - via spektrumInit()
spektrumBind(rxConfig());
break;
}
}
#endif
delay(100);
timerInit(); // timer must be initialized before any channel is allocated
dmaInit();
serialInit(feature(FEATURE_SOFTSERIAL));
mixerInit(customMotorMixer(0));
#ifdef USE_SERVOS
mixerInitServos(customServoMixer(0));
#endif
memset(&pwm_params, 0, sizeof(pwm_params));
#ifdef SONAR
const sonarHardware_t *sonarHardware = NULL;
sonarGPIOConfig_t sonarGPIOConfig;
if (feature(FEATURE_SONAR)) {
bool usingCurrentMeterIOPins = (feature(FEATURE_AMPERAGE_METER) && batteryConfig()->amperageMeterSource == AMPERAGE_METER_ADC);
sonarHardware = sonarGetHardwareConfiguration(usingCurrentMeterIOPins);
sonarGPIOConfig.triggerGPIO = sonarHardware->trigger_gpio;
sonarGPIOConfig.triggerPin = sonarHardware->trigger_pin;
sonarGPIOConfig.echoGPIO = sonarHardware->echo_gpio;
sonarGPIOConfig.echoPin = sonarHardware->echo_pin;
pwm_params.sonarGPIOConfig = &sonarGPIOConfig;
}
#endif
// when using airplane/wing mixer, servo/motor outputs are remapped
if (mixerConfig()->mixerMode == MIXER_AIRPLANE || mixerConfig()->mixerMode == MIXER_FLYING_WING || mixerConfig()->mixerMode == MIXER_CUSTOM_AIRPLANE)
pwm_params.airplane = true;
else
pwm_params.airplane = false;
#if defined(USE_UART2) && defined(STM32F10X)
pwm_params.useUART2 = doesConfigurationUsePort(SERIAL_PORT_UART2);
#endif
#if defined(USE_UART3)
pwm_params.useUART3 = doesConfigurationUsePort(SERIAL_PORT_UART3);
#endif
#if defined(USE_UART4)
pwm_params.useUART4 = doesConfigurationUsePort(SERIAL_PORT_UART4);
#endif
#if defined(USE_UART5)
pwm_params.useUART5 = doesConfigurationUsePort(SERIAL_PORT_UART5);
#endif
pwm_params.useVbat = feature(FEATURE_VBAT);
pwm_params.useSoftSerial = feature(FEATURE_SOFTSERIAL);
pwm_params.useParallelPWM = feature(FEATURE_RX_PARALLEL_PWM);
pwm_params.useRSSIADC = feature(FEATURE_RSSI_ADC);
pwm_params.useCurrentMeterADC = (
feature(FEATURE_AMPERAGE_METER)
&& batteryConfig()->amperageMeterSource == AMPERAGE_METER_ADC
);
pwm_params.useLEDStrip = feature(FEATURE_LED_STRIP);
pwm_params.usePPM = feature(FEATURE_RX_PPM);
pwm_params.useSerialRx = feature(FEATURE_RX_SERIAL);
#ifdef SONAR
pwm_params.useSonar = feature(FEATURE_SONAR);
#endif
#ifdef USE_SERVOS
pwm_params.useServos = isMixerUsingServos();
pwm_params.useChannelForwarding = feature(FEATURE_CHANNEL_FORWARDING);
pwm_params.servoCenterPulse = servoConfig()->servoCenterPulse;
pwm_params.servoPwmRate = servoConfig()->servo_pwm_rate;
#endif
pwm_params.useOneshot = feature(FEATURE_ONESHOT125);
pwm_params.motorPwmRate = motorConfig()->motor_pwm_rate;
pwm_params.idlePulse = calculateMotorOff();
if (pwm_params.motorPwmRate > 500)
pwm_params.idlePulse = 0; // brushed motors
pwmRxInit();
// pwmInit() needs to be called as soon as possible for ESC compatibility reasons
pwmIOConfiguration_t *pwmIOConfiguration = pwmInit(&pwm_params);
mixerUsePWMIOConfiguration(pwmIOConfiguration);
#ifdef DEBUG_PWM_CONFIGURATION
debug[2] = pwmIOConfiguration->pwmInputCount;
debug[3] = pwmIOConfiguration->ppmInputCount;
#endif
if (!feature(FEATURE_ONESHOT125))
motorControlEnable = true;
systemState |= SYSTEM_STATE_MOTORS_READY;
#ifdef INVERTER
initInverter();
#endif
#ifdef USE_SPI
spiInit(SPI1);
spiInit(SPI2);
#ifdef STM32F303xC
#ifdef ALIENFLIGHTF3
if (hardwareRevision == AFF3_REV_2) {
spiInit(SPI3);
}
#else
spiInit(SPI3);
#endif
#endif
#endif
#ifdef USE_HARDWARE_REVISION_DETECTION
updateHardwareRevision();
#endif
#if defined(NAZE)
if (hardwareRevision == NAZE32_SP) {
serialRemovePort(SERIAL_PORT_SOFTSERIAL2);
} else {
serialRemovePort(SERIAL_PORT_UART3);
}
#endif
#if defined(SPRACINGF3) && defined(SONAR) && defined(USE_SOFTSERIAL2)
if (feature(FEATURE_SONAR) && feature(FEATURE_SOFTSERIAL)) {
serialRemovePort(SERIAL_PORT_SOFTSERIAL2);
}
#endif
#if defined(SPRACINGF3MINI) && defined(SONAR) && defined(USE_SOFTSERIAL1)
if (feature(FEATURE_SONAR) && feature(FEATURE_SOFTSERIAL)) {
serialRemovePort(SERIAL_PORT_SOFTSERIAL1);
}
#endif
#ifdef USE_I2C
#if defined(NAZE)
if (hardwareRevision != NAZE32_SP) {
i2cInit(I2C_DEVICE);
} else {
if (!doesConfigurationUsePort(SERIAL_PORT_UART3)) {
i2cInit(I2C_DEVICE);
}
}
#elif defined(CC3D)
if (!doesConfigurationUsePort(SERIAL_PORT_UART3)) {
i2cInit(I2C_DEVICE);
}
#else
i2cInit(I2C_DEVICE);
#endif
#endif
#ifdef USE_ADC
drv_adc_config_t adc_params;
adc_params.channelMask = 0;
#ifdef ADC_BATTERY
adc_params.channelMask = (feature(FEATURE_VBAT) ? ADC_CHANNEL_MASK(ADC_BATTERY) : 0);
#endif
#ifdef ADC_RSSI
adc_params.channelMask |= (feature(FEATURE_RSSI_ADC) ? ADC_CHANNEL_MASK(ADC_RSSI) : 0);
#endif
#ifdef ADC_AMPERAGE
adc_params.channelMask |= (feature(FEATURE_AMPERAGE_METER) ? ADC_CHANNEL_MASK(ADC_AMPERAGE) : 0);
#endif
#ifdef ADC_POWER_12V
adc_params.channelMask |= ADC_CHANNEL_MASK(ADC_POWER_12V);
#endif
#ifdef ADC_POWER_5V
adc_params.channelMask |= ADC_CHANNEL_MASK(ADC_POWER_5V);
#endif
#ifdef ADC_POWER_3V
adc_params.channelMask |= ADC_CHANNEL_MASK(ADC_POWER_3V);
#endif
#ifdef NAZE
// optional ADC5 input on rev.5 hardware
adc_params.channelMask |= (hardwareRevision >= NAZE32_REV5) ? ADC_CHANNEL_MASK(ADC_EXTERNAL) : 0;
#endif
adcInit(&adc_params);
#endif
initBoardAlignment();
#ifdef DISPLAY
if (feature(FEATURE_DISPLAY)) {
displayInit();
}
#endif
#ifdef NAZE
if (hardwareRevision < NAZE32_REV5) {
gyroConfig()->gyro_sync = 0;
}
#endif
if (!sensorsAutodetect()) {
// if gyro was not detected due to whatever reason, we give up now.
failureMode(FAILURE_MISSING_ACC);
}
systemState |= SYSTEM_STATE_SENSORS_READY;
flashLedsAndBeep();
mspInit();
mspSerialInit();
const uint16_t pidPeriodUs = US_FROM_HZ(gyro.sampleFrequencyHz);
pidSetTargetLooptime(pidPeriodUs * gyroConfig()->pid_process_denom);
pidInitFilters(pidProfile());
#ifdef USE_SERVOS
mixerInitialiseServoFiltering(targetPidLooptime);
#endif
imuInit();
#ifdef USE_CLI
cliInit();
#endif
failsafeInit();
rxInit(modeActivationProfile()->modeActivationConditions);
#ifdef GPS
if (feature(FEATURE_GPS)) {
gpsInit();
navigationInit(pidProfile());
}
#endif
#ifdef SONAR
if (feature(FEATURE_SONAR)) {
sonarInit(sonarHardware);
}
#endif
#ifdef LED_STRIP
ledStripInit();
if (feature(FEATURE_LED_STRIP)) {
ledStripEnable();
}
#endif
#ifdef TELEMETRY
if (feature(FEATURE_TELEMETRY)) {
telemetryInit();
}
#endif
#ifdef USB_CABLE_DETECTION
usbCableDetectInit();
#endif
#ifdef TRANSPONDER
if (feature(FEATURE_TRANSPONDER)) {
transponderInit(transponderConfig()->data);
transponderEnable();
transponderStartRepeating();
systemState |= SYSTEM_STATE_TRANSPONDER_ENABLED;
}
#endif
#ifdef USE_FLASHFS
#ifdef NAZE
if (hardwareRevision == NAZE32_REV5) {
m25p16_init();
}
#elif defined(USE_FLASH_M25P16)
m25p16_init();
#endif
flashfsInit();
#endif
#ifdef USE_SDCARD
bool sdcardUseDMA = false;
sdcardInsertionDetectInit();
#ifdef SDCARD_DMA_CHANNEL_TX
#if defined(LED_STRIP) && defined(WS2811_DMA_CHANNEL)
// Ensure the SPI Tx DMA doesn't overlap with the led strip
sdcardUseDMA = !feature(FEATURE_LED_STRIP) || SDCARD_DMA_CHANNEL_TX != WS2811_DMA_CHANNEL;
#else
sdcardUseDMA = true;
#endif
#endif
sdcard_init(sdcardUseDMA);
afatfs_init();
#endif
#ifdef BLACKBOX
initBlackbox();
#endif
if (mixerConfig()->mixerMode == MIXER_GIMBAL) {
accSetCalibrationCycles(CALIBRATING_ACC_CYCLES);
}
gyroSetCalibrationCycles(CALIBRATING_GYRO_CYCLES);
#ifdef BARO
baroSetCalibrationCycles(CALIBRATING_BARO_CYCLES);
#endif
// start all timers
// TODO - not implemented yet
timerStart();
ENABLE_STATE(SMALL_ANGLE);
DISABLE_ARMING_FLAG(PREVENT_ARMING);
#ifdef SOFTSERIAL_LOOPBACK
// FIXME this is a hack, perhaps add a FUNCTION_LOOPBACK to support it properly
loopbackPort = (serialPort_t*)&(softSerialPorts[0]);
if (!loopbackPort->vTable) {
loopbackPort = openSoftSerial(0, NULL, 19200, SERIAL_NOT_INVERTED);
}
serialPrint(loopbackPort, "LOOPBACK\r\n");
#endif
if (feature(FEATURE_VBAT)) {
// Now that everything has powered up the voltage and cell count be determined.
voltageMeterInit();
batteryInit();
}
if (feature(FEATURE_AMPERAGE_METER)) {
amperageMeterInit();
}
#ifdef DISPLAY
if (feature(FEATURE_DISPLAY)) {
#ifdef USE_OLED_GPS_DEBUG_PAGE_ONLY
displayShowFixedPage(PAGE_GPS);
#else
displayResetPageCycling();
displayEnablePageCycling();
#endif
}
#endif
#ifdef CJMCU
LED2_ON;
#endif
// Latch active features AGAIN since some may be modified by init().
latchActiveFeatures();
motorControlEnable = true;
systemState |= SYSTEM_STATE_READY;
}
#ifdef SOFTSERIAL_LOOPBACK
void processLoopback(void) {
if (loopbackPort) {
uint8_t bytesWaiting;
while ((bytesWaiting = serialRxBytesWaiting(loopbackPort))) {
uint8_t b = serialRead(loopbackPort);
serialWrite(loopbackPort, b);
};
}
}
#else
#define processLoopback()
#endif
void configureScheduler(void)
{
schedulerInit();
setTaskEnabled(TASK_SYSTEM, true);
uint16_t gyroPeriodUs = US_FROM_HZ(gyro.sampleFrequencyHz);
rescheduleTask(TASK_GYRO, gyroPeriodUs);
setTaskEnabled(TASK_GYRO, true);
rescheduleTask(TASK_PID, gyroPeriodUs);
setTaskEnabled(TASK_PID, true);
if (sensors(SENSOR_ACC)) {
setTaskEnabled(TASK_ACCEL, true);
}
setTaskEnabled(TASK_ATTITUDE, sensors(SENSOR_ACC));
setTaskEnabled(TASK_SERIAL, true);
#ifdef BEEPER
setTaskEnabled(TASK_BEEPER, true);
#endif
setTaskEnabled(TASK_BATTERY, feature(FEATURE_VBAT) || feature(FEATURE_AMPERAGE_METER));
setTaskEnabled(TASK_RX, true);
#ifdef GPS
setTaskEnabled(TASK_GPS, feature(FEATURE_GPS));
#endif
#ifdef MAG
setTaskEnabled(TASK_COMPASS, sensors(SENSOR_MAG));
#if defined(MPU6500_SPI_INSTANCE) && defined(USE_MAG_AK8963)
// fixme temporary solution for AK6983 via slave I2C on MPU9250
rescheduleTask(TASK_COMPASS, 1000000 / 40);
#endif
#endif
#ifdef BARO
setTaskEnabled(TASK_BARO, sensors(SENSOR_BARO));
#endif
#ifdef SONAR
setTaskEnabled(TASK_SONAR, sensors(SENSOR_SONAR));
#endif
#if defined(BARO) || defined(SONAR)
setTaskEnabled(TASK_ALTITUDE, sensors(SENSOR_BARO) || sensors(SENSOR_SONAR));
#endif
#ifdef DISPLAY
setTaskEnabled(TASK_DISPLAY, feature(FEATURE_DISPLAY));
#endif
#ifdef TELEMETRY
setTaskEnabled(TASK_TELEMETRY, feature(FEATURE_TELEMETRY));
#endif
#ifdef LED_STRIP
setTaskEnabled(TASK_LEDSTRIP, feature(FEATURE_LED_STRIP));
#endif
#ifdef TRANSPONDER
setTaskEnabled(TASK_TRANSPONDER, feature(FEATURE_TRANSPONDER));
#endif
}
/*
This function processes RX dependent coefficients when new RX commands are available
Those are: TPA, throttle expo
*/
static void updateRcCommands(void)
{
int32_t prop2;
// PITCH & ROLL only dynamic PID adjustment, depending on throttle value
if (rcData[THROTTLE] < currentControlRateProfile->tpa_breakpoint) {
prop2 = 100;
} else {
if (rcData[THROTTLE] < 2000) {
prop2 = 100 - (uint16_t)currentControlRateProfile->dynThrPID * (rcData[THROTTLE] - currentControlRateProfile->tpa_breakpoint) / (2000 - currentControlRateProfile->tpa_breakpoint);
} else {
prop2 = 100 - currentControlRateProfile->dynThrPID;
}
}
for (int axis = 0; axis < 3; axis++) {
int32_t prop1;
int32_t tmp = MIN(ABS(rcData[axis] - rxConfig()->midrc), 500);
if (axis == ROLL || axis == PITCH) {
if (rcControlsConfig()->deadband) {
if (tmp > rcControlsConfig()->deadband) {
tmp -= rcControlsConfig()->deadband;
} else {
tmp = 0;
}
}
rcCommand[axis] = rcLookupPitchRoll(tmp);
prop1 = 100 - (uint16_t)currentControlRateProfile->rates[axis] * tmp / 500;
prop1 = (uint16_t)prop1 * prop2 / 100;
// non coupled PID reduction scaler used in PID controller 1 and PID controller 2. 100 means 100% of the pids
PIDweight[axis] = prop2;
} else {
if (rcControlsConfig()->yaw_deadband) {
if (tmp > rcControlsConfig()->yaw_deadband) {
tmp -= rcControlsConfig()->yaw_deadband;
} else {
tmp = 0;
}
}
rcCommand[axis] = rcLookupYaw(tmp) * -rcControlsConfig()->yaw_control_direction;
prop1 = 100 - (uint16_t)currentControlRateProfile->rates[axis] * ABS(tmp) / 500;
// YAW TPA disabled.
PIDweight[axis] = 100;
}
#ifdef USE_PID_MW23
// FIXME axis indexes into pids. use something like lookupPidIndex(rc_alias_e alias) to reduce coupling.
dynP8[axis] = (uint16_t)pidProfile()->P8[axis] * prop1 / 100;
dynI8[axis] = (uint16_t)pidProfile()->I8[axis] * prop1 / 100;
dynD8[axis] = (uint16_t)pidProfile()->D8[axis] * prop1 / 100;
#endif
if (rcData[axis] < rxConfig()->midrc) {
rcCommand[axis] = -rcCommand[axis];
}
}
int32_t tmp = constrain(rcData[THROTTLE], rxConfig()->mincheck, PWM_RANGE_MAX);
tmp = (uint32_t)(tmp - rxConfig()->mincheck) * PWM_RANGE_MIN / (PWM_RANGE_MAX - rxConfig()->mincheck); // [MINCHECK;2000] -> [0;1000]
rcCommand[THROTTLE] = rcLookupThrottle(tmp);
if (FLIGHT_MODE(HEADFREE_MODE)) {
float radDiff = degreesToRadians(DECIDEGREES_TO_DEGREES(attitude.values.yaw) - headFreeModeHold);
float cosDiff = cos_approx(radDiff);
float sinDiff = sin_approx(radDiff);
int16_t rcCommand_PITCH = rcCommand[PITCH] * cosDiff + rcCommand[ROLL] * sinDiff;
rcCommand[ROLL] = rcCommand[ROLL] * cosDiff - rcCommand[PITCH] * sinDiff;
rcCommand[PITCH] = rcCommand_PITCH;
}
}
/*
This function processes RX dependent coefficients when new RX commands are available
Those are: TPA, throttle expo
*/
void processRxDependentCoefficients(void) {
int32_t tmp, tmp2;
int32_t axis, prop1 = 0, prop2;
// TODO: SINTEF JAKOB - Add offsets somewhere in this code, so that it is not affected by deadbands,
// and so that it does not affect command stick-positions
int16_t tmpThrottle = rcData[THROTTLE] + rxMspReadOffsetRC(&rxRuntimeConfig, THROTTLE);
// PITCH & ROLL only dynamic PID adjustment, depending on throttle value
if (rcData[THROTTLE] < currentControlRateProfile->tpa_breakpoint) {
prop2 = 100;
} else {
if (rcData[THROTTLE] < 2000) {
prop2 = 100 - (uint16_t)currentControlRateProfile->dynThrPID * (rcData[THROTTLE] - currentControlRateProfile->tpa_breakpoint) / (2000 - currentControlRateProfile->tpa_breakpoint);
} else {
prop2 = 100 - currentControlRateProfile->dynThrPID;
}
}
for (axis = 0; axis < 3; axis++) {
tmp = MIN(ABS(rcData[axis] - rxConfig()->midrc), 500);
if (axis == ROLL || axis == PITCH) {
if (rcControlsConfig()->deadband) {
if (tmp > rcControlsConfig()->deadband) {
tmp -= rcControlsConfig()->deadband;
} else {
tmp = 0;
}
}
tmp += rxMspReadOffsetRC(&rxRuntimeConfig, axis);
tmp2 = tmp / 100;
rcCommand[axis] = lookupPitchRollRC[tmp2] + (tmp - tmp2 * 100) * (lookupPitchRollRC[tmp2 + 1] - lookupPitchRollRC[tmp2]) / 100;
prop1 = 100 - (uint16_t)currentControlRateProfile->rates[axis] * tmp / 500;
prop1 = (uint16_t)prop1 * prop2 / 100;
} else if (axis == YAW) {
if (rcControlsConfig()->yaw_deadband) {
if (tmp > rcControlsConfig()->yaw_deadband) {
tmp -= rcControlsConfig()->yaw_deadband;
} else {
tmp = 0;
}
}
tmp += rxMspReadOffsetRC(&rxRuntimeConfig, axis);
tmp2 = tmp / 100;
rcCommand[axis] = (lookupYawRC[tmp2] + (tmp - tmp2 * 100) * (lookupYawRC[tmp2 + 1] - lookupYawRC[tmp2]) / 100) * -rcControlsConfig()->yaw_control_direction;
prop1 = 100 - (uint16_t)currentControlRateProfile->rates[axis] * ABS(tmp) / 500;
}
#ifndef SKIP_PID_MW23
// FIXME axis indexes into pids. use something like lookupPidIndex(rc_alias_e alias) to reduce coupling.
dynP8[axis] = (uint16_t)pidProfile()->P8[axis] * prop1 / 100;
dynI8[axis] = (uint16_t)pidProfile()->I8[axis] * prop1 / 100;
dynD8[axis] = (uint16_t)pidProfile()->D8[axis] * prop1 / 100;
#endif
// non coupled PID reduction scaler used in PID controller 1 and PID controller 2. YAW TPA disabled. 100 means 100% of the pids
if (axis == YAW) {
PIDweight[axis] = 100;
}
else {
PIDweight[axis] = prop2;
}
if (rcData[axis] < rxConfig()->midrc)
rcCommand[axis] = -rcCommand[axis];
}
tmp = constrain(rcData[THROTTLE], rxConfig()->mincheck, PWM_RANGE_MAX);
tmp = (uint32_t)(tmp - rxConfig()->mincheck) * PWM_RANGE_MIN / (PWM_RANGE_MAX - rxConfig()->mincheck); // [MINCHECK;2000] -> [0;1000]
tmp2 = tmp / 100;
rcCommand[THROTTLE] = lookupThrottleRC[tmp2] + (tmp - tmp2 * 100) * (lookupThrottleRC[tmp2 + 1] - lookupThrottleRC[tmp2]) / 100; // [0;1000] -> expo -> [MINTHROTTLE;MAXTHROTTLE]
// Throttle calculations done, reset rcData to value before offset
rcData[THROTTLE] = tmpThrottle;
}
// Default settings
STATIC_UNIT_TESTED void resetConf(void)
{
pgResetAll(MAX_PROFILE_COUNT);
setProfile(0);
pgActivateProfile(0);
setControlRateProfile(0);
featureClearAll();
featureSet(DEFAULT_RX_FEATURE);
#ifdef BOARD_HAS_VOLTAGE_DIVIDER
// only enable the VBAT feature by default if the board has a voltage divider otherwise
// the user may see incorrect readings and unexpected issues with pin mappings may occur.
featureSet(FEATURE_VBAT);
#endif
featureSet(FEATURE_FAILSAFE);
parseRcChannels("AETR1234", rxConfig());
featureSet(FEATURE_BLACKBOX);
#if defined(COLIBRI_RACE)
// alternative defaults settings for COLIBRI RACE targets
imuConfig()->looptime = 1000;
featureSet(FEATURE_ONESHOT125);
featureSet(FEATURE_LED_STRIP);
#endif
#ifdef SPRACINGF3EVO
featureSet(FEATURE_TRANSPONDER);
featureSet(FEATURE_RSSI_ADC);
featureSet(FEATURE_CURRENT_METER);
featureSet(FEATURE_TELEMETRY);
#endif
// alternative defaults settings for ALIENWIIF1 and ALIENWIIF3 targets
#ifdef ALIENWII32
featureSet(FEATURE_RX_SERIAL);
featureSet(FEATURE_MOTOR_STOP);
# ifdef ALIENWIIF3
serialConfig()->portConfigs[2].functionMask = FUNCTION_RX_SERIAL;
batteryConfig()->vbatscale = 20;
# else
serialConfig()->portConfigs[1].functionMask = FUNCTION_RX_SERIAL;
# endif
rxConfig()->serialrx_provider = SERIALRX_SPEKTRUM2048;
rxConfig()->spektrum_sat_bind = 5;
motorAndServoConfig()->minthrottle = 1000;
motorAndServoConfig()->maxthrottle = 2000;
motorAndServoConfig()->motor_pwm_rate = 32000;
imuConfig()->looptime = 2000;
pidProfile()->pidController = 3;
pidProfile()->P8[PIDROLL] = 36;
pidProfile()->P8[PIDPITCH] = 36;
failsafeConfig()->failsafe_delay = 2;
failsafeConfig()->failsafe_off_delay = 0;
currentControlRateProfile->rcRate8 = 130;
currentControlRateProfile->rates[ROLL] = 20;
currentControlRateProfile->rates[PITCH] = 20;
currentControlRateProfile->rates[YAW] = 100;
parseRcChannels("TAER1234", rxConfig());
*customMotorMixer(0) = (motorMixer_t){ 1.0f, -0.414178f, 1.0f, -1.0f }; // REAR_R
*customMotorMixer(1) = (motorMixer_t){ 1.0f, -0.414178f, -1.0f, 1.0f }; // FRONT_R
*customMotorMixer(2) = (motorMixer_t){ 1.0f, 0.414178f, 1.0f, 1.0f }; // REAR_L
*customMotorMixer(3) = (motorMixer_t){ 1.0f, 0.414178f, -1.0f, -1.0f }; // FRONT_L
*customMotorMixer(4) = (motorMixer_t){ 1.0f, -1.0f, -0.414178f, -1.0f }; // MIDFRONT_R
*customMotorMixer(5) = (motorMixer_t){ 1.0f, 1.0f, -0.414178f, 1.0f }; // MIDFRONT_L
*customMotorMixer(6) = (motorMixer_t){ 1.0f, -1.0f, 0.414178f, 1.0f }; // MIDREAR_R
*customMotorMixer(7) = (motorMixer_t){ 1.0f, 1.0f, 0.414178f, -1.0f }; // MIDREAR_L
#endif
// copy first profile into remaining profile
PG_FOREACH_PROFILE(reg) {
for (int i = 1; i < MAX_PROFILE_COUNT; i++) {
memcpy(reg->address + i * pgSize(reg), reg->address, pgSize(reg));
}
}
for (int i = 1; i < MAX_PROFILE_COUNT; i++) {
configureRateProfileSelection(i, i % MAX_CONTROL_RATE_PROFILE_COUNT);
}
}
void calculate_Gtune(uint8_t axis)
{
int16_t error, diff_G, threshP;
if(rcCommand[axis] || (axis != FD_YAW && (FLIGHT_MODE(ANGLE_MODE) || FLIGHT_MODE(HORIZON_MODE)))) { // Block tuning on stick input. Always allow G-Tune on YAW, Roll & Pitch only in acromode
OldError[axis] = 0;
time_skip[axis] = delay_cycles; // Some settle time after stick center. default 450ms
} else {
if (!time_skip[axis]) AvgGyro[axis] = 0;
time_skip[axis]++;
if (time_skip[axis] > 0) {
if (axis == FD_YAW) {
AvgGyro[axis] += 32 * ((int16_t)gyroADC[axis] / 32); // Chop some jitter and average
} else {
AvgGyro[axis] += 128 * ((int16_t)gyroADC[axis] / 128); // Chop some jitter and average
}
}
if (time_skip[axis] == gtuneConfig()->gtune_average_cycles) { // Looptime cycles for gyro average calculation. default 16.
AvgGyro[axis] /= time_skip[axis]; // AvgGyro[axis] has now very clean gyrodata
time_skip[axis] = 0;
if (axis == FD_YAW) {
threshP = 20;
error = -AvgGyro[axis];
} else {
threshP = 10;
error = AvgGyro[axis];
}
if (gtuneConfig()->gtune_hilimP[axis] && error && OldError[axis] && error != OldError[axis]) { // Don't run when not needed or pointless to do so
diff_G = ABS(error) - ABS(OldError[axis]);
if ((error > 0 && OldError[axis] > 0) || (error < 0 && OldError[axis] < 0)) {
if (diff_G > threshP) {
if (axis == FD_YAW) {
result_P64[axis] += 256 + gtuneConfig()->gtune_pwr; // YAW ends up at low limit on float PID, give it some more to work with.
} else {
result_P64[axis] += 64 + gtuneConfig()->gtune_pwr; // Shift balance a little on the plus side.
}
} else {
if (diff_G < -threshP) {
if (axis == FD_YAW) {
result_P64[axis] -= 64 + gtuneConfig()->gtune_pwr;
} else {
result_P64[axis] -= 32;
}
}
}
} else {
if (ABS(diff_G) > threshP && axis != FD_YAW) {
result_P64[axis] -= 32; // Don't use antiwobble for YAW
}
}
int16_t newP = constrain((result_P64[axis] >> 6), (int16_t)gtuneConfig()->gtune_lolimP[axis], (int16_t)gtuneConfig()->gtune_hilimP[axis]);
#ifdef BLACKBOX
if (feature(FEATURE_BLACKBOX)) {
flightLogEvent_gtuneCycleResult_t eventData;
eventData.gtuneAxis = axis;
eventData.gtuneGyroAVG = AvgGyro[axis];
eventData.gtuneNewP = newP; // for float PID the logged P value is still mutiplyed by 10
blackboxLogEvent(FLIGHT_LOG_EVENT_GTUNE_RESULT, (flightLogEventData_t*)&eventData);
}
#endif
pidProfile()->P8[axis] = newP; // new P value
}
OldError[axis] = error;
}
/*
This function processes RX dependent coefficients when new RX commands are available
Those are: TPA, throttle expo
*/
void processRxDependentCoefficients(void) {
int32_t tmp, tmp2;
int32_t axis, prop1 = 0, prop2;
// PITCH & ROLL only dynamic PID adjustment, depending on throttle value
if (rcData[THROTTLE] < currentControlRateProfile->tpa_breakpoint) {
prop2 = 100;
} else {
if (rcData[THROTTLE] < 2000) {
prop2 = 100 - (uint16_t)currentControlRateProfile->dynThrPID * (rcData[THROTTLE] - currentControlRateProfile->tpa_breakpoint) / (2000 - currentControlRateProfile->tpa_breakpoint);
} else {
prop2 = 100 - currentControlRateProfile->dynThrPID;
}
}
for (axis = 0; axis < 3; axis++) {
tmp = MIN(ABS(rcData[axis] - rxConfig()->midrc), 500);
if (axis == ROLL || axis == PITCH) {
if (rcControlsConfig()->deadband) {
if (tmp > rcControlsConfig()->deadband) {
tmp -= rcControlsConfig()->deadband;
} else {
tmp = 0;
}
}
tmp2 = tmp / 100;
rcCommand[axis] = lookupPitchRollRC[tmp2] + (tmp - tmp2 * 100) * (lookupPitchRollRC[tmp2 + 1] - lookupPitchRollRC[tmp2]) / 100;
prop1 = 100 - (uint16_t)currentControlRateProfile->rates[axis] * tmp / 500;
prop1 = (uint16_t)prop1 * prop2 / 100;
} else if (axis == YAW) {
if (rcControlsConfig()->yaw_deadband) {
if (tmp > rcControlsConfig()->yaw_deadband) {
tmp -= rcControlsConfig()->yaw_deadband;
} else {
tmp = 0;
}
}
tmp2 = tmp / 100;
rcCommand[axis] = (lookupYawRC[tmp2] + (tmp - tmp2 * 100) * (lookupYawRC[tmp2 + 1] - lookupYawRC[tmp2]) / 100) * -rcControlsConfig()->yaw_control_direction;
prop1 = 100 - (uint16_t)currentControlRateProfile->rates[axis] * ABS(tmp) / 500;
}
#ifndef SKIP_PID_MW23
// FIXME axis indexes into pids. use something like lookupPidIndex(rc_alias_e alias) to reduce coupling.
dynP8[axis] = (uint16_t)pidProfile()->P8[axis] * prop1 / 100;
dynI8[axis] = (uint16_t)pidProfile()->I8[axis] * prop1 / 100;
dynD8[axis] = (uint16_t)pidProfile()->D8[axis] * prop1 / 100;
#endif
// non coupled PID reduction scaler used in PID controller 1 and PID controller 2. YAW TPA disabled. 100 means 100% of the pids
if (axis == YAW) {
PIDweight[axis] = 100;
}
else {
PIDweight[axis] = prop2;
}
if (rcData[axis] < rxConfig()->midrc)
rcCommand[axis] = -rcCommand[axis];
}
if (FLIGHT_MODE(HEADFREE_MODE)) {
float radDiff = degreesToRadians(DECIDEGREES_TO_DEGREES(attitude.values.yaw) - headFreeModeHold);
float cosDiff = cos_approx(radDiff);
float sinDiff = sin_approx(radDiff);
int16_t rcCommand_PITCH = rcCommand[PITCH] * cosDiff + rcCommand[ROLL] * sinDiff;
rcCommand[ROLL] = rcCommand[ROLL] * cosDiff - rcCommand[PITCH] * sinDiff;
rcCommand[PITCH] = rcCommand_PITCH;
}
}
void applyFixedWingLaunchController(timeUs_t currentTimeUs)
{
// Called at PID rate
if (launchState.launchDetected) {
bool applyLaunchIdleLogic = true;
if (launchState.motorControlAllowed) {
// If launch detected we are in launch procedure - control airplane
const float timeElapsedSinceLaunchMs = US2MS(currentTimeUs - launchState.launchStartedTime);
// If user moves the stick - finish the launch
if ((ABS(rcCommand[ROLL]) > rcControlsConfig()->pos_hold_deadband) || (ABS(rcCommand[PITCH]) > rcControlsConfig()->pos_hold_deadband)) {
launchState.launchFinished = true;
}
// Abort launch after a pre-set time
if (timeElapsedSinceLaunchMs >= navConfig()->fw.launch_timeout) {
launchState.launchFinished = true;
}
// Motor control enabled
if (timeElapsedSinceLaunchMs >= navConfig()->fw.launch_motor_timer) {
// Don't apply idle logic anymore
applyLaunchIdleLogic = false;
// Increase throttle gradually over `launch_motor_spinup_time` milliseconds
if (navConfig()->fw.launch_motor_spinup_time > 0) {
const float timeSinceMotorStartMs = constrainf(timeElapsedSinceLaunchMs - navConfig()->fw.launch_motor_timer, 0.0f, navConfig()->fw.launch_motor_spinup_time);
const uint16_t minIdleThrottle = MAX(motorConfig()->minthrottle, navConfig()->fw.launch_idle_throttle);
rcCommand[THROTTLE] = scaleRangef(timeSinceMotorStartMs,
0.0f, navConfig()->fw.launch_motor_spinup_time,
minIdleThrottle, navConfig()->fw.launch_throttle);
}
else {
rcCommand[THROTTLE] = navConfig()->fw.launch_throttle;
}
}
}
if (applyLaunchIdleLogic) {
// Launch idle logic - low throttle and zero out PIDs
applyFixedWingLaunchIdleLogic();
}
}
else {
// We are waiting for launch - update launch detector
updateFixedWingLaunchDetector(currentTimeUs);
// Launch idle logic - low throttle and zero out PIDs
applyFixedWingLaunchIdleLogic();
}
// Control beeper
if (!launchState.launchFinished) {
beeper(BEEPER_LAUNCH_MODE_ENABLED);
}
// Lock out controls
rcCommand[ROLL] = 0;
rcCommand[PITCH] = pidAngleToRcCommand(-DEGREES_TO_DECIDEGREES(navConfig()->fw.launch_climb_angle), pidProfile()->max_angle_inclination[FD_PITCH]);
rcCommand[YAW] = 0;
}
void taskMainPidLoop(void)
{
cycleTime = getTaskDeltaTime(TASK_SELF);
dT = (float)cycleTime * 0.000001f;
// Calculate average cycle time and average jitter
filteredCycleTime = filterApplyPt1(cycleTime, &filteredCycleTimeState, 1, dT);
debug[0] = cycleTime;
debug[1] = cycleTime - filteredCycleTime;
imuUpdateGyroAndAttitude();
annexCode();
if (rxConfig()->rcSmoothing) {
filterRc();
}
#if defined(BARO) || defined(SONAR)
haveProcessedAnnexCodeOnce = true;
#endif
#ifdef MAG
if (sensors(SENSOR_MAG)) {
updateMagHold();
}
#endif
#if defined(BARO) || defined(SONAR)
if (sensors(SENSOR_BARO) || sensors(SENSOR_SONAR)) {
if (FLIGHT_MODE(BARO_MODE) || FLIGHT_MODE(SONAR_MODE)) {
applyAltHold();
}
}
#endif
// If we're armed, at minimum throttle, and we do arming via the
// sticks, do not process yaw input from the rx. We do this so the
// motors do not spin up while we are trying to arm or disarm.
// Allow yaw control for tricopters if the user wants the servo to move even when unarmed.
if (isUsingSticksForArming() && rcData[THROTTLE] <= rxConfig()->mincheck
#ifndef USE_QUAD_MIXER_ONLY
#ifdef USE_SERVOS
&& !((mixerConfig()->mixerMode == MIXER_TRI || mixerConfig()->mixerMode == MIXER_CUSTOM_TRI) && mixerConfig()->tri_unarmed_servo)
#endif
&& mixerConfig()->mixerMode != MIXER_AIRPLANE
&& mixerConfig()->mixerMode != MIXER_FLYING_WING
#endif
) {
rcCommand[YAW] = 0;
}
if (throttleCorrectionConfig()->throttle_correction_value && (FLIGHT_MODE(ANGLE_MODE) || FLIGHT_MODE(HORIZON_MODE))) {
rcCommand[THROTTLE] += calculateThrottleAngleCorrection(throttleCorrectionConfig()->throttle_correction_value);
}
#ifdef GPS
if (sensors(SENSOR_GPS)) {
if ((FLIGHT_MODE(GPS_HOME_MODE) || FLIGHT_MODE(GPS_HOLD_MODE)) && STATE(GPS_FIX_HOME)) {
updateGpsStateForHomeAndHoldMode();
}
}
#endif
// PID - note this is function pointer set by setPIDController()
pid_controller(
pidProfile(),
currentControlRateProfile,
imuConfig()->max_angle_inclination,
&accelerometerConfig()->accelerometerTrims,
rxConfig()
);
mixTable();
#ifdef USE_SERVOS
filterServos();
writeServos();
#endif
if (motorControlEnable) {
writeMotors();
}
#ifdef USE_SDCARD
afatfs_poll();
#endif
#ifdef BLACKBOX
if (!cliMode && feature(FEATURE_BLACKBOX)) {
handleBlackbox();
}
#endif
}
void autotuneFixedWingUpdate(const flight_dynamics_index_t axis, float desiredRateDps, float reachedRateDps, float pidOutput)
{
const timeMs_t currentTimeMs = millis();
const float absDesiredRateDps = fabsf(desiredRateDps);
float maxDesiredRate = currentControlRateProfile->stabilized.rates[axis] * 10.0f;
pidAutotuneState_e newState;
// Use different max desired rate in ANGLE for pitch and roll
// Maximum reasonable error in ANGLE mode is 200% of angle inclination (control dublet), but we are conservative and tune for control singlet.
if (FLIGHT_MODE(ANGLE_MODE) && (axis == FD_PITCH || axis == FD_ROLL)) {
float maxDesiredRateInAngleMode = DECIDEGREES_TO_DEGREES(pidProfile()->max_angle_inclination[axis] * 1.0f) * pidBank()->pid[PID_LEVEL].P / FP_PID_LEVEL_P_MULTIPLIER;
maxDesiredRate = MIN(maxDesiredRate, maxDesiredRateInAngleMode);
}
if (fabsf(pidOutput) >= pidProfile()->pidSumLimit) {
// If we have saturated the pid output by P+FF don't increase the gain
tuneCurrent[axis].pidSaturated = true;
}
if (absDesiredRateDps < (pidAutotuneConfig()->fw_max_rate_threshold / 100.0f) * maxDesiredRate) {
// We can make decisions only when we are demanding at least 50% of max configured rate
newState = DEMAND_TOO_LOW;
}
else if (fabsf(reachedRateDps) > absDesiredRateDps) {
newState = DEMAND_OVERSHOOT;
}
else {
newState = DEMAND_UNDERSHOOT;
}
if (newState != tuneCurrent[axis].state) {
const timeDelta_t stateTimeMs = currentTimeMs - tuneCurrent[axis].stateEnterTime;
bool gainsUpdated = false;
switch (tuneCurrent[axis].state) {
case DEMAND_TOO_LOW:
break;
case DEMAND_OVERSHOOT:
if (stateTimeMs >= pidAutotuneConfig()->fw_overshoot_time) {
tuneCurrent[axis].gainD = tuneCurrent[axis].gainD * (100 - AUTOTUNE_FIXED_WING_DECREASE_STEP) / 100.0f;
if (tuneCurrent[axis].gainD < AUTOTUNE_FIXED_WING_MIN_FF) {
tuneCurrent[axis].gainD = AUTOTUNE_FIXED_WING_MIN_FF;
}
gainsUpdated = true;
}
break;
case DEMAND_UNDERSHOOT:
if (stateTimeMs >= pidAutotuneConfig()->fw_undershoot_time && !tuneCurrent[axis].pidSaturated) {
tuneCurrent[axis].gainD = tuneCurrent[axis].gainD * (100 + AUTOTUNE_FIXED_WING_INCREASE_STEP) / 100.0f;
if (tuneCurrent[axis].gainD > AUTOTUNE_FIXED_WING_MAX_FF) {
tuneCurrent[axis].gainD = AUTOTUNE_FIXED_WING_MAX_FF;
}
gainsUpdated = true;
}
break;
}
if (gainsUpdated) {
// Set P-gain to 10% of FF gain (quite agressive - FIXME)
tuneCurrent[axis].gainP = tuneCurrent[axis].gainD * (pidAutotuneConfig()->fw_ff_to_p_gain / 100.0f);
// Set integrator gain to reach the same response as FF gain in 0.667 second
tuneCurrent[axis].gainI = (tuneCurrent[axis].gainD / FP_PID_RATE_FF_MULTIPLIER) * (1000.0f / pidAutotuneConfig()->fw_ff_to_i_time_constant) * FP_PID_RATE_I_MULTIPLIER;
tuneCurrent[axis].gainI = constrainf(tuneCurrent[axis].gainI, 2.0f, 50.0f);
autotuneUpdateGains(tuneCurrent);
switch (axis) {
case FD_ROLL:
blackboxLogAutotuneEvent(ADJUSTMENT_ROLL_D, tuneCurrent[axis].gainD);
break;
case FD_PITCH:
blackboxLogAutotuneEvent(ADJUSTMENT_PITCH_D, tuneCurrent[axis].gainD);
break;
case FD_YAW:
blackboxLogAutotuneEvent(ADJUSTMENT_YAW_D, tuneCurrent[axis].gainD);
break;
}
}
// Change state and reset saturation flag
tuneCurrent[axis].state = newState;
tuneCurrent[axis].stateEnterTime = currentTimeMs;
tuneCurrent[axis].pidSaturated = false;
}
}