C++ ARMING_FLAG函数代码示例

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本文整理汇总了C++中ARMING_FLAG函数的典型用法代码示例。如果您正苦于以下问题：C++ ARMING_FLAG函数的具体用法？C++ ARMING_FLAG怎么用？C++ ARMING_FLAG使用的例子？那么恭喜您, 这里精选的函数代码示例或许可以为您提供帮助。

在下文中一共展示了ARMING_FLAG函数的20个代码示例，这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞，您的评价将有助于我们的系统推荐出更棒的C++代码示例。

示例1: ltm_sframe

static void ltm_sframe(void)
{
    uint8_t lt_flightmode;
    uint8_t lt_statemode;
    if (FLIGHT_MODE(PASSTHRU_MODE))
        lt_flightmode = 0;
    else if (FLIGHT_MODE(NAV_WP_MODE))
        lt_flightmode = 10;
    else if (FLIGHT_MODE(NAV_RTH_MODE))
        lt_flightmode = 13;
    else if (FLIGHT_MODE(NAV_POSHOLD_MODE))
        lt_flightmode = 9;
    else if (FLIGHT_MODE(HEADFREE_MODE) || FLIGHT_MODE(MAG_MODE))
        lt_flightmode = 11;
    else if (FLIGHT_MODE(NAV_ALTHOLD_MODE))
        lt_flightmode = 8;
    else if (FLIGHT_MODE(ANGLE_MODE))
        lt_flightmode = 2;
    else if (FLIGHT_MODE(HORIZON_MODE))
        lt_flightmode = 3;
    else
        lt_flightmode = 1;      // Rate mode

    lt_statemode = (ARMING_FLAG(ARMED)) ? 1 : 0;
    if (failsafeIsActive())
        lt_statemode |= 2;
    ltm_initialise_packet('S');
    ltm_serialise_16(vbat * 100);    //vbat converted to mv
    ltm_serialise_16(0);             //  current, not implemented
    ltm_serialise_8((uint8_t)((rssi * 254) / 1023));        // scaled RSSI (uchar)
    ltm_serialise_8(0);              // no airspeed
    ltm_serialise_8((lt_flightmode << 2) | lt_statemode);
    ltm_finalise();
}

开发者ID:damdam2，项目名称:inav，代码行数:34，代码来源:ltm.c

示例2: applyLedThrustRingLayer

static void applyLedThrustRingLayer(bool updateNow, uint32_t *timer)
{
    static uint8_t rotationPhase;
    int ledRingIndex = 0;

    if (updateNow) {
        rotationPhase = rotationPhase > 0 ? rotationPhase - 1 : ledCounts.ringSeqLen - 1;

        int scale = scaledThrottle; // ARMING_FLAG(ARMED) ? scaleRange(rcData[THROTTLE], PWM_RANGE_MIN, PWM_RANGE_MAX, 10, 100) : 10;
        *timer += LED_STRIP_HZ(5) * 10 / scale;  // 5 - 50Hz update rate
    }

    for (int ledIndex = 0; ledIndex < ledCounts.count; ledIndex++) {
        const ledConfig_t *ledConfig = &currentLedStripConfig->ledConfigs[ledIndex];
        if (ledGetFunction(ledConfig) == LED_FUNCTION_THRUST_RING) {

            bool applyColor;
            if (ARMING_FLAG(ARMED)) {
                applyColor = (ledRingIndex + rotationPhase) % ledCounts.ringSeqLen < ROTATION_SEQUENCE_LED_WIDTH;
            } else {
                applyColor = !(ledRingIndex % 2); // alternating pattern
            }

            if (applyColor) {
                const hsvColor_t *ringColor = &currentLedStripConfig->colors[ledGetColor(ledConfig)];
                setLedHsv(ledIndex, ringColor);
            }

            ledRingIndex++;
        }
    }
}

开发者ID:AlienWiiBF，项目名称:betaflight，代码行数:32，代码来源:ledstrip.c

示例3: taskUpdateBattery

void taskUpdateBattery(void)
{
    static uint32_t vbatLastServiced = 0;
    static uint32_t ibatLastServiced = 0;

    if (feature(FEATURE_VBAT)) {
        if (cmp32(currentTime, vbatLastServiced) >= VBATINTERVAL) {
            vbatLastServiced = currentTime;

            voltageMeterUpdate();
            batteryUpdate();
        }
    }

    if (feature(FEATURE_AMPERAGE_METER)) {
        int32_t ibatTimeSinceLastServiced = cmp32(currentTime, ibatLastServiced);

        if (ibatTimeSinceLastServiced >= IBATINTERVAL) {
            ibatLastServiced = currentTime;

            if (batteryConfig()->amperageMeterSource == AMPERAGE_METER_ADC) {
                amperageUpdateMeter(ibatTimeSinceLastServiced);
            } else {
                throttleStatus_e throttleStatus = calculateThrottleStatus(rxConfig(), rcControlsConfig()->deadband3d_throttle);
                bool throttleLowAndMotorStop = (throttleStatus == THROTTLE_LOW && feature(FEATURE_MOTOR_STOP));
                int32_t throttleOffset = (int32_t)rcCommand[THROTTLE] - 1000;

                amperageUpdateVirtualMeter(ibatTimeSinceLastServiced, ARMING_FLAG(ARMED), throttleLowAndMotorStop, throttleOffset);
            }
        }
    }
}

开发者ID:hexfet，项目名称:cleanflight，代码行数:32，代码来源:cleanflight_fc.c

示例4: disarm

void disarm(void)
{
    if (ARMING_FLAG(ARMED)) {
        DISABLE_ARMING_FLAG(ARMED);
        lastDisarmTimeUs = micros();

#ifdef USE_BLACKBOX
        if (blackboxConfig()->device && blackboxConfig()->mode != BLACKBOX_MODE_ALWAYS_ON) { // Close the log upon disarm except when logging mode is ALWAYS ON
            blackboxFinish();
        }
#endif
        BEEP_OFF;
#ifdef USE_DSHOT
        if (isMotorProtocolDshot() && flipOverAfterCrashMode && !feature(FEATURE_3D)) {
            pwmWriteDshotCommand(ALL_MOTORS, getMotorCount(), DSHOT_CMD_SPIN_DIRECTION_NORMAL, false);
        }
#endif
        flipOverAfterCrashMode = false;

        // if ARMING_DISABLED_RUNAWAY_TAKEOFF is set then we want to play it's beep pattern instead
        if (!(getArmingDisableFlags() & ARMING_DISABLED_RUNAWAY_TAKEOFF)) {
            beeper(BEEPER_DISARMING);      // emit disarm tone
        }
    }
}

开发者ID:4712，项目名称:cleanflight，代码行数:25，代码来源:fc_core.c

示例5: updateCurrentMeter

void updateCurrentMeter(int32_t lastUpdateAt, rxConfig_t *rxConfig, uint16_t deadband3d_throttle)
{
    static int32_t amperageRaw = 0;
    static int64_t mAhdrawnRaw = 0;
    int32_t throttleOffset = (int32_t)rcCommand[THROTTLE] - 1000;
    int32_t throttleFactor = 0;

    switch(batteryConfig->currentMeterType) {
        case CURRENT_SENSOR_ADC:
            amperageRaw -= amperageRaw / 8;
            amperageRaw += (amperageLatestADC = adcGetChannel(ADC_CURRENT));
            amperage = currentSensorToCentiamps(amperageRaw / 8);
            break;
        case CURRENT_SENSOR_VIRTUAL:
            amperage = (int32_t)batteryConfig->currentMeterOffset;
            if (ARMING_FLAG(ARMED)) {
                throttleStatus_e throttleStatus = calculateThrottleStatus(rxConfig, deadband3d_throttle);
                if (throttleStatus == THROTTLE_LOW && feature(FEATURE_MOTOR_STOP))
                    throttleOffset = 0;
                throttleFactor = throttleOffset + (throttleOffset * throttleOffset / 50);
                amperage += throttleFactor * (int32_t)batteryConfig->currentMeterScale  / 1000;
            }
            break;
        case CURRENT_SENSOR_NONE:
            amperage = 0;
            break;
    }

    mAhdrawnRaw += (amperage * lastUpdateAt) / 1000;
    mAhDrawn = mAhdrawnRaw / (3600 * 100);
}

开发者ID:AlienWiiBF，项目名称:betaflight，代码行数:31，代码来源:battery.c

示例6: ltm_sframe

static void ltm_sframe(void)
{
    uint8_t lt_flightmode;
    uint8_t lt_statemode;
    if (FLIGHT_MODE(PASSTHRU_MODE))
        lt_flightmode = 0;
    else if (FLIGHT_MODE(GPS_HOME_MODE))
        lt_flightmode = 13;
    else if (FLIGHT_MODE(GPS_HOLD_MODE))
        lt_flightmode = 9;
    else if (FLIGHT_MODE(HEADFREE_MODE))
        lt_flightmode = 4;
    else if (FLIGHT_MODE(BARO_MODE))
        lt_flightmode = 8;
    else if (FLIGHT_MODE(ANGLE_MODE))
        lt_flightmode = 2;
    else if (FLIGHT_MODE(HORIZON_MODE))
        lt_flightmode = 3;
    else
        lt_flightmode = 1;      // Rate mode

    lt_statemode = (ARMING_FLAG(ARMED)) ? 1 : 0;
    if (failsafeIsActive())
        lt_statemode |= 2;
    ltm_initialise_packet('S');
    ltm_serialise_16(getBatteryVoltage() * 100);    //vbat converted to mv
    ltm_serialise_16(0);             //  current, not implemented
    ltm_serialise_8((uint8_t)((getRssi() * 254) / 1023));        // scaled RSSI (uchar)
    ltm_serialise_8(0);              // no airspeed
    ltm_serialise_8((lt_flightmode << 2) | lt_statemode);
    ltm_finalise();
}

开发者ID:rotcehdnih，项目名称:betaflight，代码行数:32，代码来源:ltm.c

示例7: applyLedThrustRingLayer

static void applyLedThrustRingLayer(bool updateNow, timeUs_t *timer)
{
    static uint8_t rotationPhase;
    int ledRingIndex = 0;

    if (updateNow) {
        rotationPhase = rotationPhase > 0 ? rotationPhase - 1 : ledCounts.ringSeqLen - 1;

        *timer += HZ_TO_US(5 + (45 * scaledThrottle) / 100);  // 5 - 50Hz update rate
    }

    for (int ledIndex = 0; ledIndex < ledCounts.count; ledIndex++) {
        const ledConfig_t *ledConfig = &ledStripConfig()->ledConfigs[ledIndex];
        if (ledGetFunction(ledConfig) == LED_FUNCTION_THRUST_RING) {

            bool applyColor;
            if (ARMING_FLAG(ARMED)) {
                applyColor = (ledRingIndex + rotationPhase) % ledCounts.ringSeqLen < ROTATION_SEQUENCE_LED_WIDTH;
            } else {
                applyColor = !(ledRingIndex % 2); // alternating pattern
            }

            if (applyColor) {
                const hsvColor_t *ringColor = &ledStripConfig()->colors[ledGetColor(ledConfig)];
                setLedHsv(ledIndex, ringColor);
            }

            ledRingIndex++;
        }
    }
}

开发者ID:DTFUHF，项目名称:betaflight，代码行数:31，代码来源:ledstrip.c

示例8: applyLedAnimationLayer

static void applyLedAnimationLayer(bool updateNow, uint32_t *timer)
{
    static uint8_t frameCounter = 0;
    const int animationFrames = ledGridHeight;
    if(updateNow) {
        frameCounter = (frameCounter + 1 < animationFrames) ? frameCounter + 1 : 0;
        *timer += LED_STRIP_HZ(20);
    }

    if (ARMING_FLAG(ARMED))
        return;

    int previousRow = frameCounter > 0 ? frameCounter - 1 : animationFrames - 1;
    int currentRow = frameCounter;
    int nextRow = (frameCounter + 1 < animationFrames) ? frameCounter + 1 : 0;

    for (int ledIndex = 0; ledIndex < ledCounts.count; ledIndex++) {
        const ledConfig_t *ledConfig = &masterConfig.ledConfigs[ledIndex];

        if (ledGetY(ledConfig) == previousRow) {
            setLedHsv(ledIndex, getSC(LED_SCOLOR_ANIMATION));
            scaleLedValue(ledIndex, 50);
        } else if (ledGetY(ledConfig) == currentRow) {
            setLedHsv(ledIndex, getSC(LED_SCOLOR_ANIMATION));
        } else if (ledGetY(ledConfig) == nextRow) {
            scaleLedValue(ledIndex, 50);
        }
    }
}

开发者ID:npsm，项目名称:inav，代码行数:29，代码来源:ledstrip.c

示例9: taskCameraControl

static void taskCameraControl(uint32_t currentTime)
{
    if (ARMING_FLAG(ARMED)) {
        return;
    }

    cameraControlProcess(currentTime);
}

开发者ID:channgo2203，项目名称:cleanflight，代码行数:8，代码来源:fc_tasks.c

示例10: mwArm

void mwArm(void)
{
    if (ARMING_FLAG(OK_TO_ARM)) {
        if (ARMING_FLAG(ARMED)) {
			//led0_op(true);
            return;
        }
        if (IS_RC_MODE_ACTIVE(BOXFAILSAFE)) {
            return;
        }
        if (!ARMING_FLAG(PREVENT_ARMING)) {
            ENABLE_ARMING_FLAG(ARMED);
            headFreeModeHold = heading;
           // led2_op(1);//drona led
           // led1_op(1);//drona led
           // led0_op(0);//drona led

#ifdef BLACKBOX
            if (feature(FEATURE_BLACKBOX)) {
                serialPort_t *sharedBlackboxAndMspPort = findSharedSerialPort(FUNCTION_BLACKBOX, FUNCTION_MSP);
                if (sharedBlackboxAndMspPort) {
                    mspReleasePortIfAllocated(sharedBlackboxAndMspPort);
                }
                startBlackbox();
            }
#endif
            disarmAt = millis() + masterConfig.auto_disarm_delay * 1000;   // start disarm timeout, will be extended when throttle is nonzero

            //beep to indicate arming
#ifdef GPS
            if (feature(FEATURE_GPS) && STATE(GPS_FIX) && GPS_numSat >= 5)
                beeper(BEEPER_ARMING_GPS_FIX);
            else
                beeper(BEEPER_ARMING);
#else
            beeper(BEEPER_ARMING);
#endif

            return;
        }
    }

    if (!ARMING_FLAG(ARMED)) {
        beeperConfirmationBeeps(1);
    }
}

开发者ID:braininahat，项目名称:Pluto，代码行数:46，代码来源:mw.c

示例11: mwArm

void mwArm(void)
{
    if (ARMING_FLAG(OK_TO_ARM)) {
        if (ARMING_FLAG(ARMED)) {
            return;
        }
        if (!ARMING_FLAG(PREVENT_ARMING)) {
            ENABLE_ARMING_FLAG(ARMED);
            headFreeModeHold = heading;
            return;
        }
    }

    if (!ARMING_FLAG(ARMED)) {
        blinkLedAndSoundBeeper(2, 255, 1);
    }
}

开发者ID:zatalian，项目名称:cleanflight，代码行数:17，代码来源:mw.c

示例12: applyLedWarningLayer

static void applyLedWarningLayer(bool updateNow, uint32_t *timer)
{
    static uint8_t warningFlashCounter = 0;
    static uint8_t warningFlags = 0;          // non-zero during blinks

    if (updateNow) {
        // keep counter running, so it stays in sync with blink
        warningFlashCounter++;
        warningFlashCounter &= 0xF;

        if (warningFlashCounter == 0) {      // update when old flags was processed
            warningFlags = 0;
            if (feature(FEATURE_VBAT) && getBatteryState() != BATTERY_OK)
                warningFlags |= 1 << WARNING_LOW_BATTERY;
            if (feature(FEATURE_FAILSAFE) && failsafeIsActive())
                warningFlags |= 1 << WARNING_FAILSAFE;
            if (!ARMING_FLAG(ARMED) && !ARMING_FLAG(OK_TO_ARM))
                warningFlags |= 1 << WARNING_ARMING_DISABLED;
        }
        *timer += LED_STRIP_HZ(10);
    }

    if (warningFlags) {
        const hsvColor_t *warningColor = NULL;

        bool colorOn = (warningFlashCounter % 2) == 0;   // w_w_
        warningFlags_e warningId = warningFlashCounter / 4;
        if (warningFlags & (1 << warningId)) {
            switch (warningId) {
                case WARNING_ARMING_DISABLED:
                    warningColor = colorOn ? &HSV(GREEN)  : &HSV(BLACK);
                    break;
                case WARNING_LOW_BATTERY:
                    warningColor = colorOn ? &HSV(RED)    : &HSV(BLACK);
                    break;
                case WARNING_FAILSAFE:
                    warningColor = colorOn ? &HSV(YELLOW) : &HSV(BLUE);
                    break;
                default:;
            }
        }
        if (warningColor)
            applyLedHsv(LED_MOV_OVERLAY(LED_FLAG_OVERLAY(LED_OVERLAY_WARNING)), warningColor);
    }
}

开发者ID:andriuP6，项目名称:betaflight，代码行数:45，代码来源:ledstrip.c

示例13: mwArm

void mwArm(void)
{
    if (ARMING_FLAG(OK_TO_ARM)) {
        if (ARMING_FLAG(ARMED)) {
            return;
        }
        if (IS_RC_MODE_ACTIVE(BOXFAILSAFE)) {
            return;
        }
        if (!ARMING_FLAG(PREVENT_ARMING)) {
            ENABLE_ARMING_FLAG(ARMED);
            ENABLE_ARMING_FLAG(WAS_EVER_ARMED);
            headFreeModeHold = DECIDEGREES_TO_DEGREES(attitude.values.yaw);

            resetMagHoldHeading(DECIDEGREES_TO_DEGREES(attitude.values.yaw));

#ifdef BLACKBOX
            if (feature(FEATURE_BLACKBOX)) {
                serialPort_t *sharedBlackboxAndMspPort = findSharedSerialPort(FUNCTION_BLACKBOX, FUNCTION_MSP);
                if (sharedBlackboxAndMspPort) {
                    mspSerialReleasePortIfAllocated(sharedBlackboxAndMspPort);
                }
                startBlackbox();
            }
#endif
            disarmAt = millis() + masterConfig.auto_disarm_delay * 1000;   // start disarm timeout, will be extended when throttle is nonzero

            //beep to indicate arming
#ifdef NAV
            if (navigationPositionEstimateIsHealthy())
                beeper(BEEPER_ARMING_GPS_FIX);
            else
                beeper(BEEPER_ARMING);
#else
            beeper(BEEPER_ARMING);
#endif

            return;
        }
    }

    if (!ARMING_FLAG(ARMED)) {
        beeperConfirmationBeeps(1);
    }
}

开发者ID:iforce2d，项目名称:cleanflight，代码行数:45，代码来源:mw.c

示例14: taskVtxControl

// Everything that listens to VTX devices
void taskVtxControl(uint32_t currentTime)
{
    if (ARMING_FLAG(ARMED))
        return;

#ifdef VTX_COMMON
    vtxCommonProcess(currentTime);
#endif
}

开发者ID:basdelfos，项目名称:betaflight，代码行数:10，代码来源:fc_tasks.c

示例15: taskBatteryAlerts

static void taskBatteryAlerts(timeUs_t currentTimeUs)
{
    if (!ARMING_FLAG(ARMED)) {
        // the battery *might* fall out in flight, but if that happens the FC will likely be off too unless the user has battery backup.
        batteryUpdatePresence();
    }
    batteryUpdateStates(currentTimeUs);
    batteryUpdateAlarms();
}

开发者ID:channgo2203，项目名称:cleanflight，代码行数:9，代码来源:fc_tasks.c

示例16: mwArm

void mwArm(void)
{
    static bool firstArmingCalibrationWasCompleted;

    if (armingConfig()->gyro_cal_on_first_arm && !firstArmingCalibrationWasCompleted) {
        gyroSetCalibrationCycles();
        armingCalibrationWasInitialised = true;
        firstArmingCalibrationWasCompleted = true;
    }

    if (!isGyroCalibrationComplete()) return;  // prevent arming before gyro is calibrated

    if (ARMING_FLAG(OK_TO_ARM)) {
        if (ARMING_FLAG(ARMED)) {
            return;
        }
        if (IS_RC_MODE_ACTIVE(BOXFAILSAFE)) {
            return;
        }
        if (!ARMING_FLAG(PREVENT_ARMING)) {
            ENABLE_ARMING_FLAG(ARMED);
            ENABLE_ARMING_FLAG(WAS_EVER_ARMED);
            headFreeModeHold = DECIDEGREES_TO_DEGREES(attitude.values.yaw);

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

            //beep to indicate arming
#ifdef GPS
            if (feature(FEATURE_GPS) && STATE(GPS_FIX) && GPS_numSat >= 5)
                beeper(BEEPER_ARMING_GPS_FIX);
            else
                beeper(BEEPER_ARMING);
#else
            beeper(BEEPER_ARMING);
#endif

            return;
        }
    }

    if (!ARMING_FLAG(ARMED)) {
        beeperConfirmationBeeps(1);
    }
}

开发者ID:savaga，项目名称:betaflight-sirinfpv，代码行数:44，代码来源:fc_core.c

示例17: sendThrottleOrBatterySizeAsRpm

static void sendThrottleOrBatterySizeAsRpm(void)
{
    sendDataHead(ID_RPM);
    if (ARMING_FLAG(ARMED)) {
        serialize16(rcCommand[THROTTLE] / BLADE_NUMBER_DIVIDER);
    } else {
        serialize16((batteryConfig->batteryCapacity / BLADE_NUMBER_DIVIDER));
    }

}

开发者ID:FLYFPV，项目名称:cleanflight，代码行数:10，代码来源:frsky.c

示例18: pidLuxFloat

void pidLuxFloat(const pidProfile_t *pidProfile, const controlRateConfig_t *controlRateConfig,
        uint16_t max_angle_inclination, const rollAndPitchTrims_t *angleTrim, const rxConfig_t *rxConfig)
{
    float horizonLevelStrength = 0.0f;
    if (FLIGHT_MODE(HORIZON_MODE)) {
        // (convert 0-100 range to 0.0-1.0 range)
        horizonLevelStrength = (float)calcHorizonLevelStrength(rxConfig->midrc, pidProfile->horizon_tilt_effect,
                pidProfile->horizon_tilt_mode, pidProfile->D8[PIDLEVEL]) / 100.0f;
    }

    // ----------PID controller----------
    for (int axis = 0; axis < 3; axis++) {
        const uint8_t rate = controlRateConfig->rates[axis];

        // -----Get the desired angle rate depending on flight mode
        float angleRate;
        if (axis == FD_YAW) {
            // YAW is always gyro-controlled (MAG correction is applied to rcCommand) 100dps to 1100dps max yaw rate
            angleRate = (float)((rate + 27) * rcCommand[YAW]) / 32.0f;
        } else {
            // control is GYRO based for ACRO and HORIZON - direct sticks control is applied to rate PID
            angleRate = (float)((rate + 27) * rcCommand[axis]) / 16.0f; // 200dps to 1200dps max roll/pitch rate
            if (FLIGHT_MODE(ANGLE_MODE) || FLIGHT_MODE(HORIZON_MODE)) {
                // calculate error angle and limit the angle to the max inclination
                // multiplication of rcCommand corresponds to changing the sticks scaling here
#ifdef GPS
                const float errorAngle = constrain(2 * rcCommand[axis] + GPS_angle[axis], -((int)max_angle_inclination), max_angle_inclination)
                        - attitude.raw[axis] + angleTrim->raw[axis];
#else
                const float errorAngle = constrain(2 * rcCommand[axis], -((int)max_angle_inclination), max_angle_inclination)
                        - attitude.raw[axis] + angleTrim->raw[axis];
#endif
                if (FLIGHT_MODE(ANGLE_MODE)) {
                    // ANGLE mode
                    angleRate = errorAngle * pidProfile->P8[PIDLEVEL] / 16.0f;
                } else {
                    // HORIZON mode
                    // mix in errorAngle to desired angleRate to add a little auto-level feel.
                    // horizonLevelStrength has been scaled to the stick input
                    angleRate += errorAngle * pidProfile->I8[PIDLEVEL] * horizonLevelStrength / 16.0f;
                }
            }
        }

        // --------low-level gyro-based PID. ----------
        const float gyroRate = luxGyroScale * gyroADCf[axis] * gyro.scale;
        axisPID[axis] = pidLuxFloatCore(axis, pidProfile, gyroRate, angleRate);
        //axisPID[axis] = constrain(axisPID[axis], -PID_LUX_FLOAT_MAX_PID, PID_LUX_FLOAT_MAX_PID);
#ifdef GTUNE
        if (FLIGHT_MODE(GTUNE_MODE) && ARMING_FLAG(ARMED)) {
            calculate_Gtune(axis);
        }
#endif
    }
}

开发者ID:hexfet，项目名称:cleanflight，代码行数:55，代码来源:pid_luxfloat.c

示例19: mwArm

void mwArm(void)
{
    if (ARMING_FLAG(OK_TO_ARM)) {
        if (ARMING_FLAG(ARMED)) {
            return;
        }
        if (rcModeIsActive(BOXFAILSAFE)) {
            return;
        }
        if (!ARMING_FLAG(PREVENT_ARMING)) {
            ENABLE_ARMING_FLAG(ARMED);
            headFreeModeHold = DECIDEGREES_TO_DEGREES(attitude.values.yaw);

#ifdef BLACKBOX
            if (feature(FEATURE_BLACKBOX)) {
                serialPort_t *sharedBlackboxAndMspPort = findSharedSerialPort(FUNCTION_BLACKBOX, FUNCTION_MSP_SERVER);
                if (sharedBlackboxAndMspPort) {
                    mspSerialReleasePortIfAllocated(sharedBlackboxAndMspPort);
                }
                startBlackbox();
            }
#endif
            disarmAt = millis() + armingConfig()->auto_disarm_delay * 1000;   // start disarm timeout, will be extended when throttle is nonzero

            //beep to indicate arming
#ifdef GPS
            if (feature(FEATURE_GPS) && STATE(GPS_FIX) && GPS_numSat >= 5)
                beeper(BEEPER_ARMING_GPS_FIX);
            else
                beeper(BEEPER_ARMING);
#else
            beeper(BEEPER_ARMING);
#endif

            return;
        }
    }

    if (!ARMING_FLAG(ARMED)) {
        beeperConfirmationBeeps(1);
    }
}

开发者ID:LupinIII，项目名称:cleanflight，代码行数:42，代码来源:cleanflight_fc.c

示例20: updateGtuneState

void updateGtuneState(void)
{
    static bool GTuneWasUsed = false;

    if (IS_RC_MODE_ACTIVE(BOXGTUNE)) {
        if (!FLIGHT_MODE(GTUNE_MODE) && ARMING_FLAG(ARMED)) {
            ENABLE_FLIGHT_MODE(GTUNE_MODE);
            init_Gtune(&currentProfile->pidProfile);
            GTuneWasUsed = true;
        }
        if (!FLIGHT_MODE(GTUNE_MODE) && !ARMING_FLAG(ARMED) && GTuneWasUsed) {
            saveConfigAndNotify();
            GTuneWasUsed = false;
        }
    } else {
        if (FLIGHT_MODE(GTUNE_MODE) && ARMING_FLAG(ARMED)) {
            DISABLE_FLIGHT_MODE(GTUNE_MODE);
        }
    }
}

开发者ID:ledvinap，项目名称:cleanflight，代码行数:20，代码来源:mw.c

注：本文中的ARMING_FLAG函数示例整理自Github/MSDocs等源码及文档管理平台，相关代码片段筛选自各路编程大神贡献的开源项目，源码版权归原作者所有，传播和使用请参考对应项目的License；未经允许，请勿转载。

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C++ ARMING_FLAG函数代码示例

示例1: ltm_sframe

示例2: applyLedThrustRingLayer

示例3: taskUpdateBattery

示例4: disarm

示例5: updateCurrentMeter

示例6: ltm_sframe

示例7: applyLedThrustRingLayer

示例8: applyLedAnimationLayer

示例9: taskCameraControl

示例10: mwArm

示例11: mwArm

示例12: applyLedWarningLayer

示例13: mwArm

示例14: taskVtxControl

示例15: taskBatteryAlerts

示例16: mwArm

示例17: sendThrottleOrBatterySizeAsRpm

示例18: pidLuxFloat

示例19: mwArm

示例20: updateGtuneState

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