コード例 #1
0
ファイル: mw.cpp プロジェクト: f8industries/hackflight
void setup(void)
{
    board.init();

    // sleep for 100ms
    board.delayMilliseconds(100);

    // flash the LEDs to indicate startup
    board.ledRedOn();
    board.ledGreenOff();
    for (uint8_t i = 0; i < 10; i++) {
        board.ledRedToggle();
        board.ledGreenToggle();
        board.delayMilliseconds(50);
    }
    board.ledRedOff();
    board.ledGreenOff();

    // initialize our RC, IMU, mixer, and PID controller
    rc.init(&board);
    imu.init(&board);
    pid.init();
    mixer.init(&board, &rc, &pid); 
    msp.init(&board, &imu, &mixer, &rc);

    // set initial time
    previousTime = board.getMicros();

    // always do gyro calibration at startup
    calibratingG = CONFIG_CALIBRATING_GYRO_CYCLES;

    // trigger accelerometer calibration requirement
    haveSmallAngle = true;

} // setup
コード例 #2
0
ファイル: mw.cpp プロジェクト: rwagajualfred/hackflight
void setup(void)
{
    uint32_t calibratingGyroMsec;

    // Get particulars for board
    board.init(imuLooptimeUsec, calibratingGyroMsec);

    // sleep for 100ms
    board.delayMilliseconds(100);

    // flash the LEDs to indicate startup
    board.ledRedOn();
    board.ledGreenOff();
    for (uint8_t i = 0; i < 10; i++) {
        board.ledRedToggle();
        board.ledGreenToggle();
        board.delayMilliseconds(50);
    }
    board.ledRedOff();
    board.ledGreenOff();

    // compute cycles for calibration based on board's time constant
    calibratingGyroCycles = (uint16_t)(1000. * calibratingGyroMsec / imuLooptimeUsec);
    calibratingAccCycles  = (uint16_t)(1000. * CONFIG_CALIBRATING_ACC_MSEC  / imuLooptimeUsec);

    // initializing timing tasks
    imuTask.init(imuLooptimeUsec);
    rcTask.init(CONFIG_RC_LOOPTIME_MSEC * 1000);
    accelCalibrationTask.init(CONFIG_CALIBRATE_ACCTIME_MSEC * 1000);
    altitudeEstimationTask.init(CONFIG_ALTITUDE_UPDATE_MSEC * 1000);

    // initialize our external objects with objects they need
    rc.init(&board);
    stab.init(&rc, &imu);
    imu.init(&board, calibratingGyroCycles, calibratingAccCycles);
    mixer.init(&board, &rc, &stab); 
    msp.init(&board, &imu, &nav, &mixer, &rc);
    nav.init(&board, &imu, &baro, &rc);

    // always do gyro calibration at startup
    calibratingG = calibratingGyroCycles;

    // assume shallow angle (no accelerometer calibration needed)
    haveSmallAngle = true;

    // ensure not armed
    armed = false;
    
    // attempt to initialize barometer
    baro.init(&board);

} // setup
コード例 #3
0
ファイル: mw.cpp プロジェクト: rwagajualfred/hackflight
void loop(void)
{
    static bool     accCalibrated;
    static uint16_t calibratingA;
    static uint32_t currentTime;
    static uint32_t disarmTime;

    if (rcTask.checkAndUpdate(currentTime)) {

        // update RC channels
        rc.update();

        // when landed, reset integral component of PID
        if (rc.throttleIsDown()) 
            stab.resetIntegral();

        if (rc.changed()) {

            if (armed) {      // actions during armed

                // Disarm on throttle down + yaw
                if (rc.sticks == THR_LO + YAW_LO + PIT_CE + ROL_CE) {
                    if (armed) {
                        armed = false;
                        // Reset disarm time so that it works next time we arm the board.
                        if (disarmTime != 0)
                            disarmTime = 0;
                    }
                }
            } else {         // actions during not armed

                // gyro calibration
                if (rc.sticks == THR_LO + YAW_LO + PIT_LO + ROL_CE) 
                    calibratingG = calibratingGyroCycles;

                // Arm via throttle-low / yaw-right
                if (rc.sticks == THR_LO + YAW_HI + PIT_CE + ROL_CE)
                    if (calibratingG == 0 && accCalibrated) 
                        if (!rc.auxState()) // aux switch must be in zero position
                            if (!armed)          
                                armed = true;

                // accel calibration
                if (rc.sticks == THR_HI + YAW_LO + PIT_LO + ROL_CE)
                    calibratingA = calibratingAccCycles;

            } // not armed

        } // rc.changed()

        // Switch to alt-hold when switch moves to position 1 or 2
        nav.checkSwitch();

    } else {                    // not in rc loop

        static int taskOrder;   // never call all functions in the same loop, to avoid high delay spikes

        switch (taskOrder) {
            case 0:
                if (baro.available())
                    baro.update();
                taskOrder++;
                break;
            case 1:
                if (baro.available() && altitudeEstimationTask.checkAndUpdate(currentTime)) {
                    nav.updateAltitudePid(armed);
                }
                taskOrder++;
                break;
            case 2:
                taskOrder++;
                break;
            case 3:
                taskOrder++;
                break;
            case 4:
                taskOrder = 0;
                break;
        }
    }

    currentTime = board.getMicros();

    if (imuTask.checkAndUpdate(currentTime)) {

        imu.update(currentTime, armed, calibratingA, calibratingG);

        haveSmallAngle = abs(imu.angle[0]) < CONFIG_SMALL_ANGLE && abs(imu.angle[1]) < CONFIG_SMALL_ANGLE;

        // measure loop rate just afer reading the sensors
        currentTime = board.getMicros();

        // compute exponential RC commands
        rc.computeExpo();

        // use LEDs to indicate calibration status
        if (calibratingA > 0 || calibratingG > 0) 
            board.ledGreenOn();
        else {
            if (accCalibrated)
                board.ledGreenOff();
            if (armed)
                board.ledRedOn();
            else
                board.ledRedOff();
        }

        // periodically update accelerometer calibration status
        if (accelCalibrationTask.check(currentTime)) {
            if (!haveSmallAngle) {
                accCalibrated = false; 
                board.ledGreenToggle();
                accelCalibrationTask.update(currentTime);
            } else {
                accCalibrated = true;
            }
        }

        // handle serial communications
        msp.update(armed);

        // perform navigation tasks (alt-hold etc.)
        nav.perform();

        // update stability PID controller 
        stab.update();

        // update mixer
        mixer.update(armed);

    } // IMU update

} // loop()
コード例 #4
0
ファイル: mw.cpp プロジェクト: f8industries/hackflight
void loop(void)
{
    static uint32_t rcTime = 0;
    static uint32_t loopTime;
    static uint32_t calibratedAccTime;
    static bool     accCalibrated;
    static bool     armed;
    static uint16_t calibratingA;
    static uint32_t currentTime;
    static uint32_t disarmTime = 0;

    if (check_and_update_timed_task(&rcTime, CONFIG_RC_LOOPTIME_USEC, currentTime)) {

        // update RC channels
        rc.update();

        // when landed, reset integral component of PID
        if (rc.throttleIsDown()) 
            pid.resetIntegral();

        if (rc.changed()) {

            if (armed) {      // actions during armed

                // Disarm on throttle down + yaw
                if (rc.sticks == THR_LO + YAW_LO + PIT_CE + ROL_CE) {
                    if (armed) {
                        armed = false;
                        // Reset disarm time so that it works next time we arm the board.
                        if (disarmTime != 0)
                            disarmTime = 0;
                    }
                }
            } else {            // actions during not armed

                // GYRO calibration
                if (rc.sticks == THR_LO + YAW_LO + PIT_LO + ROL_CE) {
                    calibratingG = CONFIG_CALIBRATING_GYRO_CYCLES;
                } 

                // Arm via YAW
                if ((rc.sticks == THR_LO + YAW_HI + PIT_CE + ROL_CE)) {
                    if (calibratingG == 0 && accCalibrated) {
                        if (!armed) {         // arm now!
                            armed = true;
                        }
                    } else if (!armed) {
                        blinkLED(2, 255, 1);
                    }
                }

                // Calibrating Acc
                else if (rc.sticks == THR_HI + YAW_LO + PIT_LO + ROL_CE)
                    calibratingA = CONFIG_CALIBRATING_ACC_CYCLES;

            } // not armed

        } // rc.changed()

    } else {                    // not in rc loop

        static int taskOrder;   // never call all functions in the same loop, to avoid high delay spikes

        switch (taskOrder) {
            case 0:
                taskOrder++;
                //sensorsGetBaro();
            case 1:
                taskOrder++;
                //sensorsGetSonar();
            case 2:
                taskOrder++;
            case 3:
                taskOrder++;
            case 4:
                taskOrder = 0;
                break;
        }
    }

    currentTime = board.getMicros();

    if (check_and_update_timed_task(&loopTime, CONFIG_IMU_LOOPTIME_USEC, currentTime)) {

        imu.update(armed, calibratingA, calibratingG);

        haveSmallAngle = abs(imu.angle[0]) < CONFIG_SMALL_ANGLE && abs(imu.angle[1]) < CONFIG_SMALL_ANGLE;

        // measure loop rate just afer reading the sensors
        currentTime = board.getMicros();
        previousTime = currentTime;

        // compute exponential RC commands
        rc.computeExpo();

        // use LEDs to indicate calibration status
        if (calibratingA > 0 || calibratingG > 0) { 
            board.ledGreenToggle();
        } else {
            if (accCalibrated)
                board.ledGreenOff();
            if (armed)
                board.ledRedOn();
            else
                board.ledRedOff();
        }

        if (check_timed_task(calibratedAccTime, currentTime)) {
            if (!haveSmallAngle) {
                accCalibrated = false; // accelerometer not calibrated or angle too steep
                board.ledGreenToggle();
                update_timed_task(&calibratedAccTime, CONFIG_CALIBRATE_ACCTIME_USEC, currentTime);
            } else {
                accCalibrated = true;
            }
        }

        // handle serial communications
        msp.update(armed);

        // update PID controller 
        pid.update(&rc, &imu);

        // update mixer
        mixer.update(armed);

    } // IMU update

} // loop()