void taskMainPidLoop(void)
{
cycleTime = getTaskDeltaTime(TASK_SELF);
dT = (float)cycleTime * 0.000001f;
imuUpdateAccelerometer();
imuUpdateGyroAndAttitude();
annexCode();
if (masterConfig.rxConfig.rcSmoothing) {
filterRc(isRXDataNew);
}
#if defined(NAV)
if (isRXDataNew) {
updateWaypointsAndNavigationMode();
}
#endif
isRXDataNew = false;
#if defined(NAV)
updatePositionEstimator();
applyWaypointNavigationAndAltitudeHold();
#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] <= masterConfig.rxConfig.mincheck
#ifndef USE_QUAD_MIXER_ONLY
#ifdef USE_SERVOS
&& !((masterConfig.mixerMode == MIXER_TRI || masterConfig.mixerMode == MIXER_CUSTOM_TRI) && masterConfig.servoMixerConfig.tri_unarmed_servo)
#endif
&& masterConfig.mixerMode != MIXER_AIRPLANE
&& masterConfig.mixerMode != MIXER_FLYING_WING
&& masterConfig.mixerMode != MIXER_CUSTOM_AIRPLANE
#endif
) {
rcCommand[YAW] = 0;
}
// Apply throttle tilt compensation
if (!STATE(FIXED_WING)) {
int16_t thrTiltCompStrength = 0;
if (navigationRequiresThrottleTiltCompensation()) {
thrTiltCompStrength = 100;
}
else if (currentProfile->throttle_tilt_compensation_strength && (FLIGHT_MODE(ANGLE_MODE) || FLIGHT_MODE(HORIZON_MODE))) {
thrTiltCompStrength = currentProfile->throttle_tilt_compensation_strength;
}
if (thrTiltCompStrength) {
rcCommand[THROTTLE] = constrain(masterConfig.motorConfig.minthrottle
+ (rcCommand[THROTTLE] - masterConfig.motorConfig.minthrottle) * calculateThrottleTiltCompensationFactor(thrTiltCompStrength),
masterConfig.motorConfig.minthrottle,
masterConfig.motorConfig.maxthrottle);
}
}
pidController(¤tProfile->pidProfile, currentControlRateProfile, &masterConfig.rxConfig);
#ifdef HIL
if (hilActive) {
hilUpdateControlState();
motorControlEnable = false;
}
#endif
mixTable();
#ifdef USE_SERVOS
if (isMixerUsingServos()) {
servoMixer(currentProfile->flaperon_throw_offset, currentProfile->flaperon_throw_inverted);
}
if (feature(FEATURE_SERVO_TILT)) {
processServoTilt();
}
//Servos should be filtered or written only when mixer is using servos or special feaures are enabled
if (isServoOutputEnabled()) {
filterServos();
writeServos();
}
#endif
if (motorControlEnable) {
writeMotors();
}
#ifdef USE_SDCARD
afatfs_poll();
#endif
#ifdef BLACKBOX
if (!cliMode && feature(FEATURE_BLACKBOX)) {
handleBlackbox();
}
#endif
}
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
}
