Exemple #1
0
void useRcControlsConfig(modeActivationCondition_t *modeActivationConditions, escAndServoConfig_t *escAndServoConfigToUse, pidProfile_t *pidProfileToUse)
{
    escAndServoConfig = escAndServoConfigToUse;
    pidProfile = pidProfileToUse;

    isUsingSticksToArm = !isModeActivationConditionPresent(modeActivationConditions, BOXARM);
}
Exemple #2
0
void useRcControlsConfig(modeActivationCondition_t *modeActivationConditions, motorConfig_t *motorConfig, pidProfile_t *pidProfileToUse)
{
    motorConfig = motorConfig;
    pidProfile = pidProfileToUse;

    isUsingSticksToArm = !isModeActivationConditionPresent(modeActivationConditions, BOXARM);
}
Exemple #3
0
void updateUsedModeActivationConditionFlags(void)
{
    memset(specifiedConditionCountPerMode, 0, CHECKBOX_ITEM_COUNT);
    for (int index = 0; index < MAX_MODE_ACTIVATION_CONDITION_COUNT; index++) {
        if (IS_RANGE_USABLE(&modeActivationConditions(index)->range)) {
            specifiedConditionCountPerMode[modeActivationConditions(index)->modeId]++;
        }
    }

    isUsingSticksToArm = !isModeActivationConditionPresent(BOXARM);

#ifdef NAV
    isUsingNAVModes = isModeActivationConditionPresent(BOXNAVPOSHOLD) ||
                        isModeActivationConditionPresent(BOXNAVRTH) ||
                        isModeActivationConditionPresent(BOXNAVWP);
#endif
}
Exemple #4
0
static FAST_CODE void subTaskPidController(timeUs_t currentTimeUs)
{
    uint32_t startTime = 0;
    if (debugMode == DEBUG_PIDLOOP) {startTime = micros();}
    // PID - note this is function pointer set by setPIDController()
    pidController(currentPidProfile, &accelerometerConfig()->accelerometerTrims, currentTimeUs);
    DEBUG_SET(DEBUG_PIDLOOP, 1, micros() - startTime);

#ifdef USE_RUNAWAY_TAKEOFF
    // Check to see if runaway takeoff detection is active (anti-taz), the pidSum is over the threshold,
    // and gyro rate for any axis is above the limit for at least the activate delay period.
    // If so, disarm for safety
    if (ARMING_FLAG(ARMED)
        && !STATE(FIXED_WING)
        && pidConfig()->runaway_takeoff_prevention
        && !runawayTakeoffCheckDisabled
        && !flipOverAfterCrashMode
        && !runawayTakeoffTemporarilyDisabled
        && (!feature(FEATURE_MOTOR_STOP) || isAirmodeActive() || (calculateThrottleStatus() != THROTTLE_LOW))) {

        if (((fabsf(pidData[FD_PITCH].Sum) >= RUNAWAY_TAKEOFF_PIDSUM_THRESHOLD)
            || (fabsf(pidData[FD_ROLL].Sum) >= RUNAWAY_TAKEOFF_PIDSUM_THRESHOLD)
            || (fabsf(pidData[FD_YAW].Sum) >= RUNAWAY_TAKEOFF_PIDSUM_THRESHOLD))
            && ((ABS(gyroAbsRateDps(FD_PITCH)) > RUNAWAY_TAKEOFF_GYRO_LIMIT_RP)
                || (ABS(gyroAbsRateDps(FD_ROLL)) > RUNAWAY_TAKEOFF_GYRO_LIMIT_RP)
                || (ABS(gyroAbsRateDps(FD_YAW)) > RUNAWAY_TAKEOFF_GYRO_LIMIT_YAW))) {

            if (runawayTakeoffTriggerUs == 0) {
                runawayTakeoffTriggerUs = currentTimeUs + RUNAWAY_TAKEOFF_ACTIVATE_DELAY;
            } else if (currentTimeUs > runawayTakeoffTriggerUs) {
                setArmingDisabled(ARMING_DISABLED_RUNAWAY_TAKEOFF);
                disarm();
            }
        } else {
            runawayTakeoffTriggerUs = 0;
        }
        DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_ENABLED_STATE, DEBUG_RUNAWAY_TAKEOFF_TRUE);
        DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_ACTIVATING_DELAY, runawayTakeoffTriggerUs == 0 ? DEBUG_RUNAWAY_TAKEOFF_FALSE : DEBUG_RUNAWAY_TAKEOFF_TRUE);
    } else {
        runawayTakeoffTriggerUs = 0;
        DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_ENABLED_STATE, DEBUG_RUNAWAY_TAKEOFF_FALSE);
        DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_ACTIVATING_DELAY, DEBUG_RUNAWAY_TAKEOFF_FALSE);
    }
#endif


#ifdef USE_PID_AUDIO
    if (isModeActivationConditionPresent(BOXPIDAUDIO)) {
        pidAudioUpdate();
    }
#endif
}
bool telemetryDetermineEnabledState(portSharing_e portSharing)
{
    bool enabled = portSharing == PORTSHARING_NOT_SHARED;

    if (portSharing == PORTSHARING_SHARED) {
        if (isModeActivationConditionPresent(BOXTELEMETRY))
            enabled = IS_RC_MODE_ACTIVE(BOXTELEMETRY);
        else
            enabled = ARMING_FLAG(ARMED);
    }

    return enabled;
}
Exemple #6
0
throttleStatus_e calculateThrottleStatus(void)
{
    if (feature(FEATURE_3D)) {
        if (IS_RC_MODE_ACTIVE(BOX3DDISABLE) || isModeActivationConditionPresent(BOX3DONASWITCH)) {
            if (rcData[THROTTLE] < rxConfig()->mincheck) {
                return THROTTLE_LOW;
            }
        } else if ((rcData[THROTTLE] > (rxConfig()->midrc - flight3DConfig()->deadband3d_throttle) && rcData[THROTTLE] < (rxConfig()->midrc + flight3DConfig()->deadband3d_throttle))) {
            return THROTTLE_LOW;
        }
    } else if (rcData[THROTTLE] < rxConfig()->mincheck) {
        return THROTTLE_LOW;
    }

    return THROTTLE_HIGH;
}
Exemple #7
0
void useRcControlsConfig(pidProfile_t *pidProfileToUse)
{
    pidProfile = pidProfileToUse;

    isUsingSticksToArm = !isModeActivationConditionPresent(BOXARM);
}
Exemple #8
0
/*
 * processRx called from taskUpdateRxMain
 */
bool processRx(timeUs_t currentTimeUs)
{
    static bool armedBeeperOn = false;

    if (!calculateRxChannelsAndUpdateFailsafe(currentTimeUs)) {
        return false;
    }

    // in 3D mode, we need to be able to disarm by switch at any time
    if (feature(FEATURE_3D)) {
        if (!IS_RC_MODE_ACTIVE(BOXARM))
            disarm();
    }

    updateRSSI(currentTimeUs);

    if (currentTimeUs > FAILSAFE_POWER_ON_DELAY_US && !failsafeIsMonitoring()) {
        failsafeStartMonitoring();
    }
    failsafeUpdateState();

    const throttleStatus_e throttleStatus = calculateThrottleStatus();
    const uint8_t throttlePercent = calculateThrottlePercent();

    if (isAirmodeActive() && ARMING_FLAG(ARMED)) {
        if (throttlePercent >= rxConfig()->airModeActivateThreshold) {
            airmodeIsActivated = true; // Prevent Iterm from being reset
        }
    } else {
        airmodeIsActivated = false;
    }

    /* In airmode Iterm should be prevented to grow when Low thottle and Roll + Pitch Centered.
     This is needed to prevent Iterm winding on the ground, but keep full stabilisation on 0 throttle while in air */
    if (throttleStatus == THROTTLE_LOW && !airmodeIsActivated) {
        pidResetITerm();
        if (currentPidProfile->pidAtMinThrottle)
            pidStabilisationState(PID_STABILISATION_ON);
        else
            pidStabilisationState(PID_STABILISATION_OFF);
    } else {
        pidStabilisationState(PID_STABILISATION_ON);
    }

#ifdef USE_RUNAWAY_TAKEOFF
    // If runaway_takeoff_prevention is enabled, accumulate the amount of time that throttle
    // is above runaway_takeoff_deactivate_throttle with the any of the R/P/Y sticks deflected
    // to at least runaway_takeoff_stick_percent percent while the pidSum on all axis is kept low.
    // Once the amount of accumulated time exceeds runaway_takeoff_deactivate_delay then disable
    // prevention for the remainder of the battery.

    if (ARMING_FLAG(ARMED)
        && pidConfig()->runaway_takeoff_prevention
        && !runawayTakeoffCheckDisabled
        && !flipOverAfterCrashMode
        && !runawayTakeoffTemporarilyDisabled
        && !STATE(FIXED_WING)) {

        // Determine if we're in "flight"
        //   - motors running
        //   - throttle over runaway_takeoff_deactivate_throttle_percent
        //   - sticks are active and have deflection greater than runaway_takeoff_deactivate_stick_percent
        //   - pidSum on all axis is less then runaway_takeoff_deactivate_pidlimit
        bool inStableFlight = false;
        if (!feature(FEATURE_MOTOR_STOP) || isAirmodeActive() || (throttleStatus != THROTTLE_LOW)) { // are motors running?
            const uint8_t lowThrottleLimit = pidConfig()->runaway_takeoff_deactivate_throttle;
            const uint8_t midThrottleLimit = constrain(lowThrottleLimit * 2, lowThrottleLimit * 2, RUNAWAY_TAKEOFF_HIGH_THROTTLE_PERCENT);
            if ((((throttlePercent >= lowThrottleLimit) && areSticksActive(RUNAWAY_TAKEOFF_DEACTIVATE_STICK_PERCENT)) || (throttlePercent >= midThrottleLimit))
                && (fabsf(pidData[FD_PITCH].Sum) < RUNAWAY_TAKEOFF_DEACTIVATE_PIDSUM_LIMIT)
                && (fabsf(pidData[FD_ROLL].Sum) < RUNAWAY_TAKEOFF_DEACTIVATE_PIDSUM_LIMIT)
                && (fabsf(pidData[FD_YAW].Sum) < RUNAWAY_TAKEOFF_DEACTIVATE_PIDSUM_LIMIT)) {

                inStableFlight = true;
                if (runawayTakeoffDeactivateUs == 0) {
                    runawayTakeoffDeactivateUs = currentTimeUs;
                }
            }
        }

        // If we're in flight, then accumulate the time and deactivate once it exceeds runaway_takeoff_deactivate_delay milliseconds
        if (inStableFlight) {
            if (runawayTakeoffDeactivateUs == 0) {
                runawayTakeoffDeactivateUs = currentTimeUs;
            }
            uint16_t deactivateDelay = pidConfig()->runaway_takeoff_deactivate_delay;
            // at high throttle levels reduce deactivation delay by 50%
            if (throttlePercent >= RUNAWAY_TAKEOFF_HIGH_THROTTLE_PERCENT) {
                deactivateDelay = deactivateDelay / 2;
            }
            if ((cmpTimeUs(currentTimeUs, runawayTakeoffDeactivateUs) + runawayTakeoffAccumulatedUs) > deactivateDelay * 1000) {
                runawayTakeoffCheckDisabled = true;
            }

        } else {
            if (runawayTakeoffDeactivateUs != 0) {
                runawayTakeoffAccumulatedUs += cmpTimeUs(currentTimeUs, runawayTakeoffDeactivateUs);
            }
            runawayTakeoffDeactivateUs = 0;
        }
        if (runawayTakeoffDeactivateUs == 0) {
            DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_DEACTIVATING_DELAY, DEBUG_RUNAWAY_TAKEOFF_FALSE);
            DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_DEACTIVATING_TIME, runawayTakeoffAccumulatedUs / 1000);
        } else {
            DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_DEACTIVATING_DELAY, DEBUG_RUNAWAY_TAKEOFF_TRUE);
            DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_DEACTIVATING_TIME, (cmpTimeUs(currentTimeUs, runawayTakeoffDeactivateUs) + runawayTakeoffAccumulatedUs) / 1000);
        }
    } else {
        DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_DEACTIVATING_DELAY, DEBUG_RUNAWAY_TAKEOFF_FALSE);
        DEBUG_SET(DEBUG_RUNAWAY_TAKEOFF, DEBUG_RUNAWAY_TAKEOFF_DEACTIVATING_TIME, DEBUG_RUNAWAY_TAKEOFF_FALSE);
    }
#endif

    // When armed and motors aren't spinning, do beeps and then disarm
    // board after delay so users without buzzer won't lose fingers.
    // mixTable constrains motor commands, so checking  throttleStatus is enough
    if (ARMING_FLAG(ARMED)
        && feature(FEATURE_MOTOR_STOP)
        && !STATE(FIXED_WING)
        && !feature(FEATURE_3D)
        && !isAirmodeActive()
    ) {
        if (isUsingSticksForArming()) {
            if (throttleStatus == THROTTLE_LOW) {
                if (armingConfig()->auto_disarm_delay != 0
                    && (int32_t)(disarmAt - millis()) < 0
                ) {
                    // auto-disarm configured and delay is over
                    disarm();
                    armedBeeperOn = false;
                } else {
                    // still armed; do warning beeps while armed
                    beeper(BEEPER_ARMED);
                    armedBeeperOn = true;
                }
            } else {
                // throttle is not low
                if (armingConfig()->auto_disarm_delay != 0) {
                    // extend disarm time
                    disarmAt = millis() + armingConfig()->auto_disarm_delay * 1000;
                }

                if (armedBeeperOn) {
                    beeperSilence();
                    armedBeeperOn = false;
                }
            }
        } else {
            // arming is via AUX switch; beep while throttle low
            if (throttleStatus == THROTTLE_LOW) {
                beeper(BEEPER_ARMED);
                armedBeeperOn = true;
            } else if (armedBeeperOn) {
                beeperSilence();
                armedBeeperOn = false;
            }
        }
    }

    processRcStickPositions();

    if (feature(FEATURE_INFLIGHT_ACC_CAL)) {
        updateInflightCalibrationState();
    }

    updateActivatedModes();

#ifdef USE_DSHOT
    /* Enable beep warning when the crash flip mode is active */
    if (isMotorProtocolDshot() && isModeActivationConditionPresent(BOXFLIPOVERAFTERCRASH) && IS_RC_MODE_ACTIVE(BOXFLIPOVERAFTERCRASH)) {
        beeper(BEEPER_CRASH_FLIP_MODE);
    }
#endif

    if (!cliMode) {
        updateAdjustmentStates();
        processRcAdjustments(currentControlRateProfile);
    }

    bool canUseHorizonMode = true;

    if ((IS_RC_MODE_ACTIVE(BOXANGLE) || failsafeIsActive()) && (sensors(SENSOR_ACC))) {
        // bumpless transfer to Level mode
        canUseHorizonMode = false;

        if (!FLIGHT_MODE(ANGLE_MODE)) {
            ENABLE_FLIGHT_MODE(ANGLE_MODE);
        }
    } else {
        DISABLE_FLIGHT_MODE(ANGLE_MODE); // failsafe support
    }

    if (IS_RC_MODE_ACTIVE(BOXHORIZON) && canUseHorizonMode) {

        DISABLE_FLIGHT_MODE(ANGLE_MODE);

        if (!FLIGHT_MODE(HORIZON_MODE)) {
            ENABLE_FLIGHT_MODE(HORIZON_MODE);
        }
    } else {
        DISABLE_FLIGHT_MODE(HORIZON_MODE);
    }

#ifdef USE_GPS_RESCUE
    if (IS_RC_MODE_ACTIVE(BOXGPSRESCUE) || (failsafeIsActive() && failsafeConfig()->failsafe_procedure == FAILSAFE_PROCEDURE_GPS_RESCUE)) {
        if (!FLIGHT_MODE(GPS_RESCUE_MODE)) {
            ENABLE_FLIGHT_MODE(GPS_RESCUE_MODE);
        }
    } else {
        DISABLE_FLIGHT_MODE(GPS_RESCUE_MODE);
    }
#endif

    if (FLIGHT_MODE(ANGLE_MODE) || FLIGHT_MODE(HORIZON_MODE)) {
        LED1_ON;
        // increase frequency of attitude task to reduce drift when in angle or horizon mode
        rescheduleTask(TASK_ATTITUDE, TASK_PERIOD_HZ(500));
    } else {
        LED1_OFF;
        rescheduleTask(TASK_ATTITUDE, TASK_PERIOD_HZ(100));
    }

    if (!IS_RC_MODE_ACTIVE(BOXPREARM) && ARMING_FLAG(WAS_ARMED_WITH_PREARM)) {
        DISABLE_ARMING_FLAG(WAS_ARMED_WITH_PREARM);
    }

#if defined(USE_ACC) || defined(USE_MAG)
    if (sensors(SENSOR_ACC) || sensors(SENSOR_MAG)) {
#if defined(USE_GPS) || defined(USE_MAG)
        if (IS_RC_MODE_ACTIVE(BOXMAG)) {
            if (!FLIGHT_MODE(MAG_MODE)) {
                ENABLE_FLIGHT_MODE(MAG_MODE);
                magHold = DECIDEGREES_TO_DEGREES(attitude.values.yaw);
            }
        } else {
            DISABLE_FLIGHT_MODE(MAG_MODE);
        }
#endif
        if (IS_RC_MODE_ACTIVE(BOXHEADFREE)) {
            if (!FLIGHT_MODE(HEADFREE_MODE)) {
                ENABLE_FLIGHT_MODE(HEADFREE_MODE);
            }
        } else {
            DISABLE_FLIGHT_MODE(HEADFREE_MODE);
        }
        if (IS_RC_MODE_ACTIVE(BOXHEADADJ)) {
            if (imuQuaternionHeadfreeOffsetSet()){
               beeper(BEEPER_RX_SET);
            }
        }
    }
#endif

    if (IS_RC_MODE_ACTIVE(BOXPASSTHRU)) {
        ENABLE_FLIGHT_MODE(PASSTHRU_MODE);
    } else {
        DISABLE_FLIGHT_MODE(PASSTHRU_MODE);
    }

    if (mixerConfig()->mixerMode == MIXER_FLYING_WING || mixerConfig()->mixerMode == MIXER_AIRPLANE) {
        DISABLE_FLIGHT_MODE(HEADFREE_MODE);
    }

#ifdef USE_TELEMETRY
    static bool sharedPortTelemetryEnabled = false;

    if (feature(FEATURE_TELEMETRY)) {
        bool enableSharedPortTelemetry = (!isModeActivationConditionPresent(BOXTELEMETRY) && ARMING_FLAG(ARMED)) || (isModeActivationConditionPresent(BOXTELEMETRY) && IS_RC_MODE_ACTIVE(BOXTELEMETRY));
        if (enableSharedPortTelemetry && !sharedPortTelemetryEnabled) {
            mspSerialReleaseSharedTelemetryPorts();
            telemetryCheckState();

            sharedPortTelemetryEnabled = true;
        } else if (!enableSharedPortTelemetry && sharedPortTelemetryEnabled) {
            // the telemetry state must be checked immediately so that shared serial ports are released.
            telemetryCheckState();
            mspSerialAllocatePorts();

            sharedPortTelemetryEnabled = false;
        }
    }
#endif

#ifdef USE_VTX_CONTROL
    vtxUpdateActivatedChannel();

    if (canUpdateVTX()) {
        handleVTXControlButton();
    }
#endif

#ifdef USE_ACRO_TRAINER
    pidSetAcroTrainerState(IS_RC_MODE_ACTIVE(BOXACROTRAINER) && sensors(SENSOR_ACC));
#endif // USE_ACRO_TRAINER

#ifdef USE_RC_SMOOTHING_FILTER
    if (ARMING_FLAG(ARMED) && !rcSmoothingInitializationComplete()) {
        beeper(BEEPER_RC_SMOOTHING_INIT_FAIL);
    }
#endif

    pidSetAntiGravityState(IS_RC_MODE_ACTIVE(BOXANTIGRAVITY) || feature(FEATURE_ANTI_GRAVITY));
    
    return true;
}
Exemple #9
0
void tryArm(void)
{
    if (armingConfig()->gyro_cal_on_first_arm) {
        gyroStartCalibration(true);
    }

    updateArmingStatus();

    if (!isArmingDisabled()) {
        if (ARMING_FLAG(ARMED)) {
            return;
        }
#ifdef USE_DSHOT
        if (micros() - getLastDshotBeaconCommandTimeUs() < DSHOT_BEACON_GUARD_DELAY_US) {
            if (tryingToArm == ARMING_DELAYED_DISARMED) {
                if (isModeActivationConditionPresent(BOXFLIPOVERAFTERCRASH) && IS_RC_MODE_ACTIVE(BOXFLIPOVERAFTERCRASH)) {
                    tryingToArm = ARMING_DELAYED_CRASHFLIP;
                } else {
                    tryingToArm = ARMING_DELAYED_NORMAL;
                }
            }
            return;
        }
        if (isMotorProtocolDshot() && isModeActivationConditionPresent(BOXFLIPOVERAFTERCRASH)) {
            if (!(IS_RC_MODE_ACTIVE(BOXFLIPOVERAFTERCRASH) || (tryingToArm == ARMING_DELAYED_CRASHFLIP))) {
                flipOverAfterCrashMode = false;
                if (!feature(FEATURE_3D)) {
                    pwmWriteDshotCommand(ALL_MOTORS, getMotorCount(), DSHOT_CMD_SPIN_DIRECTION_NORMAL, false);
                }
            } else {
                flipOverAfterCrashMode = true;
#ifdef USE_RUNAWAY_TAKEOFF
                runawayTakeoffCheckDisabled = false;
#endif
                if (!feature(FEATURE_3D)) {
                    pwmWriteDshotCommand(ALL_MOTORS, getMotorCount(), DSHOT_CMD_SPIN_DIRECTION_REVERSED, false);
                }
            }
        }
#endif

        ENABLE_ARMING_FLAG(ARMED);
        ENABLE_ARMING_FLAG(WAS_EVER_ARMED);

        resetTryingToArm();

#ifdef USE_ACRO_TRAINER
        pidAcroTrainerInit();
#endif // USE_ACRO_TRAINER

        if (isModeActivationConditionPresent(BOXPREARM)) {
            ENABLE_ARMING_FLAG(WAS_ARMED_WITH_PREARM);
        }
        imuQuaternionHeadfreeOffsetSet();

        disarmAt = millis() + armingConfig()->auto_disarm_delay * 1000;   // start disarm timeout, will be extended when throttle is nonzero

        lastArmingDisabledReason = 0;

        //beep to indicate arming
#ifdef USE_GPS
        if (feature(FEATURE_GPS) && STATE(GPS_FIX) && gpsSol.numSat >= 5) {
            beeper(BEEPER_ARMING_GPS_FIX);
        } else {
            beeper(BEEPER_ARMING);
        }
#else
        beeper(BEEPER_ARMING);
#endif

#ifdef USE_RUNAWAY_TAKEOFF
        runawayTakeoffDeactivateUs = 0;
        runawayTakeoffAccumulatedUs = 0;
        runawayTakeoffTriggerUs = 0;
#endif
    } else {
       resetTryingToArm();
        if (!isFirstArmingGyroCalibrationRunning()) {
            int armingDisabledReason = ffs(getArmingDisableFlags());
            if (lastArmingDisabledReason != armingDisabledReason) {
                lastArmingDisabledReason = armingDisabledReason;

                beeperWarningBeeps(armingDisabledReason);
            }
        }
    }
}
Exemple #10
0
void updateArmingStatus(void)
{
    if (ARMING_FLAG(ARMED)) {
        LED0_ON;
    } else {
        // Check if the power on arming grace time has elapsed
        if ((getArmingDisableFlags() & ARMING_DISABLED_BOOT_GRACE_TIME) && (millis() >= systemConfig()->powerOnArmingGraceTime * 1000)) {
            // If so, unset the grace time arming disable flag
            unsetArmingDisabled(ARMING_DISABLED_BOOT_GRACE_TIME);
        }

        // Clear the crash flip active status
        flipOverAfterCrashMode = false;

        // If switch is used for arming then check it is not defaulting to on when the RX link recovers from a fault
        if (!isUsingSticksForArming()) {
            static bool hadRx = false;
            const bool haveRx = rxIsReceivingSignal();

            const bool justGotRxBack = !hadRx && haveRx;

            if (justGotRxBack && IS_RC_MODE_ACTIVE(BOXARM)) {
                // If the RX has just started to receive a signal again and the arm switch is on, apply arming restriction
                setArmingDisabled(ARMING_DISABLED_BAD_RX_RECOVERY);
            } else if (haveRx && !IS_RC_MODE_ACTIVE(BOXARM)) {
                // If RX signal is OK and the arm switch is off, remove arming restriction
                unsetArmingDisabled(ARMING_DISABLED_BAD_RX_RECOVERY);
            }

            hadRx = haveRx;
        }

        if (IS_RC_MODE_ACTIVE(BOXFAILSAFE)) {
            setArmingDisabled(ARMING_DISABLED_BOXFAILSAFE);
        } else {
            unsetArmingDisabled(ARMING_DISABLED_BOXFAILSAFE);
        }

        if (calculateThrottleStatus() != THROTTLE_LOW) {
            setArmingDisabled(ARMING_DISABLED_THROTTLE);
        } else {
            unsetArmingDisabled(ARMING_DISABLED_THROTTLE);
        }

        if (!STATE(SMALL_ANGLE) && !IS_RC_MODE_ACTIVE(BOXFLIPOVERAFTERCRASH)) {
            setArmingDisabled(ARMING_DISABLED_ANGLE);
        } else {
            unsetArmingDisabled(ARMING_DISABLED_ANGLE);
        }

        if (averageSystemLoadPercent > 100) {
            setArmingDisabled(ARMING_DISABLED_LOAD);
        } else {
            unsetArmingDisabled(ARMING_DISABLED_LOAD);
        }

        if (isCalibrating()) {
            setArmingDisabled(ARMING_DISABLED_CALIBRATING);
        } else {
            unsetArmingDisabled(ARMING_DISABLED_CALIBRATING);
        }

        if (isModeActivationConditionPresent(BOXPREARM)) {
            if (IS_RC_MODE_ACTIVE(BOXPREARM) && !ARMING_FLAG(WAS_ARMED_WITH_PREARM)) {
                unsetArmingDisabled(ARMING_DISABLED_NOPREARM);
            } else {
                setArmingDisabled(ARMING_DISABLED_NOPREARM);
            }
        }

#ifdef USE_GPS_RESCUE
        if (isModeActivationConditionPresent(BOXGPSRESCUE)) {
            if (!gpsRescueConfig()->minSats || STATE(GPS_FIX_HOME) || ARMING_FLAG(WAS_EVER_ARMED)) {
                unsetArmingDisabled(ARMING_DISABLED_GPS);
            } else {
                setArmingDisabled(ARMING_DISABLED_GPS);
            }
        }
#endif

        if (IS_RC_MODE_ACTIVE(BOXPARALYZE)) {
            setArmingDisabled(ARMING_DISABLED_PARALYZE);
        }

        if (!isUsingSticksForArming()) {
          /* Ignore ARMING_DISABLED_CALIBRATING if we are going to calibrate gyro on first arm */
          bool ignoreGyro = armingConfig()->gyro_cal_on_first_arm
                         && !(getArmingDisableFlags() & ~(ARMING_DISABLED_ARM_SWITCH | ARMING_DISABLED_CALIBRATING));

          /* Ignore ARMING_DISABLED_THROTTLE (once arm switch is on) if we are in 3D mode */
          bool ignoreThrottle = feature(FEATURE_3D)
                             && !IS_RC_MODE_ACTIVE(BOX3D)
                             && !flight3DConfig()->switched_mode3d
                             && !(getArmingDisableFlags() & ~(ARMING_DISABLED_ARM_SWITCH | ARMING_DISABLED_THROTTLE));

#ifdef USE_RUNAWAY_TAKEOFF
           if (!IS_RC_MODE_ACTIVE(BOXARM)) {
               unsetArmingDisabled(ARMING_DISABLED_RUNAWAY_TAKEOFF);
           }
#endif

          // If arming is disabled and the ARM switch is on
          if (isArmingDisabled()
              && !ignoreGyro
              && !ignoreThrottle
              && IS_RC_MODE_ACTIVE(BOXARM)) {
              setArmingDisabled(ARMING_DISABLED_ARM_SWITCH);
          } else if (!IS_RC_MODE_ACTIVE(BOXARM)) {
              unsetArmingDisabled(ARMING_DISABLED_ARM_SWITCH);
          }
        }

        if (isArmingDisabled()) {
            warningLedFlash();
        } else {
            warningLedDisable();
        }

        warningLedUpdate();
    }
}