예제 #1
0
파일: config.c 프로젝트: jeyong/cleanflight
// 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);
    }
}
예제 #2
0
// Default settings
STATIC_UNIT_TESTED void resetConf(void)
{
    pgResetAll(MAX_PROFILE_COUNT);

    setProfile(0);
    pgActivateProfile(0);

    setControlRateProfile(0);

    parseRcChannels("AETR1234", rxConfig());

    featureClearAll();

    featureSet(DEFAULT_RX_FEATURE | FEATURE_FAILSAFE | FEATURE_BLACKBOX);
#ifdef DEFAULT_FEATURES
    featureSet(DEFAULT_FEATURES);
#endif

#ifdef BOARD_HAS_VOLTAGE_DIVIDER
    // only enable the feature by default if the board has supporting hardware
    featureSet(FEATURE_VBAT);
#endif

#ifdef BOARD_HAS_AMPERAGE_METER
    // only enable the feature by default if the board has supporting hardware
    featureSet(FEATURE_AMPERAGE_METER);
    batteryConfig()->amperageMeterSource = AMPERAGE_METER_ADC;
#endif

    // alternative defaults settings for ALIENFLIGHTF1 and ALIENFLIGHTF3 targets
#ifdef ALIENFLIGHT
#ifdef ALIENFLIGHTF3
    serialConfig()->portConfigs[2].functionMask = FUNCTION_RX_SERIAL;
    getVoltageMeterConfig(ADC_BATTERY)->vbatscale = 20;
    sensorSelectionConfig()->mag_hardware = MAG_NONE;            // disabled by default
# else
    serialConfig()->portConfigs[1].functionMask = FUNCTION_RX_SERIAL;
# endif
    rxConfig()->serialrx_provider = SERIALRX_SPEKTRUM2048;
    rxConfig()->spektrum_sat_bind = 5;
    motorConfig()->minthrottle = 1000;
    motorConfig()->maxthrottle = 2000;
    motorConfig()->motor_pwm_rate = 32000;
    failsafeConfig()->failsafe_delay = 2;
    failsafeConfig()->failsafe_off_delay = 0;
    mixerConfig()->yaw_jump_prevention_limit = YAW_JUMP_PREVENTION_LIMIT_HIGH;
    currentControlRateProfile->rcRate8 = 100;
    currentControlRateProfile->rates[PITCH] = 20;
    currentControlRateProfile->rates[ROLL] = 20;
    currentControlRateProfile->rates[YAW] = 20;
    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);
    }
}
예제 #3
0
파일: fc_core.c 프로젝트: 4712/cleanflight
/*
 * 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;
}