Пример #1
0
void calculateEstimatedAltitude(uint32_t currentTime)
{
    static uint32_t previousTime;
    uint32_t dTime;
    int32_t baroVel;
    float dt;
    float vel_acc;
    int32_t vel_tmp;
    float accZ_tmp;
    static float accZ_old = 0.0f;
    static float vel = 0.0f;
    static float accAlt = 0.0f;
    static int32_t lastBaroAlt;

#ifdef SONAR
    int32_t sonarAlt = SONAR_OUT_OF_RANGE;
    static int32_t baroAlt_offset = 0;
    float sonarTransition;
#endif

    dTime = currentTime - previousTime;
    if (dTime < BARO_UPDATE_FREQUENCY_40HZ)
        return;

    previousTime = currentTime;

#ifdef BARO
    if (!isBaroCalibrationComplete()) {
        performBaroCalibrationCycle();
        vel = 0;
        accAlt = 0;
    }

    BaroAlt = baroCalculateAltitude();
#else
    BaroAlt = 0;
#endif

#ifdef SONAR
    sonarAlt = sonarRead();
    sonarAlt = sonarCalculateAltitude(sonarAlt, getCosTiltAngle());

    if (sonarAlt > 0 && sonarAlt < sonarCfAltCm) {
        // just use the SONAR
        baroAlt_offset = BaroAlt - sonarAlt;
        BaroAlt = sonarAlt;
    } else {
        BaroAlt -= baroAlt_offset;
        if (sonarAlt > 0  && sonarAlt <= sonarMaxAltWithTiltCm) {
            // SONAR in range, so use complementary filter
            sonarTransition = (float)(sonarMaxAltWithTiltCm - sonarAlt) / (sonarMaxAltWithTiltCm - sonarCfAltCm);
            BaroAlt = sonarAlt * sonarTransition + BaroAlt * (1.0f - sonarTransition);
        }
    }
#endif

    dt = accTimeSum * 1e-6f; // delta acc reading time in seconds

    // Integrator - velocity, cm/sec
    if (accSumCount) {
        accZ_tmp = (float)accSum[2] / (float)accSumCount;
    } else {
        accZ_tmp = 0;
    }
    vel_acc = accZ_tmp * accVelScale * (float)accTimeSum;

    // Integrator - Altitude in cm
    accAlt += (vel_acc * 0.5f) * dt + vel * dt;                                                                 // integrate velocity to get distance (x= a/2 * t^2)
    accAlt = accAlt * barometerConfig->baro_cf_alt + (float)BaroAlt * (1.0f - barometerConfig->baro_cf_alt);    // complementary filter for altitude estimation (baro & acc)
    vel += vel_acc;

#ifdef DEBUG_ALT_HOLD
    debug[1] = accSum[2] / accSumCount; // acceleration
    debug[2] = vel;                     // velocity
    debug[3] = accAlt;                  // height
#endif

    imuResetAccelerationSum();

#ifdef BARO
    if (!isBaroCalibrationComplete()) {
        return;
    }
#endif

#ifdef SONAR
    if (sonarAlt > 0 && sonarAlt < sonarCfAltCm) {
        // the sonar has the best range
        EstAlt = BaroAlt;
    } else {
        EstAlt = accAlt;
    }
#else
    EstAlt = accAlt;
#endif

    baroVel = (BaroAlt - lastBaroAlt) * 1000000.0f / dTime;
    lastBaroAlt = BaroAlt;

    baroVel = constrain(baroVel, -1500, 1500);  // constrain baro velocity +/- 1500cm/s
    baroVel = applyDeadband(baroVel, 10);       // to reduce noise near zero

    // apply Complimentary Filter to keep the calculated velocity based on baro velocity (i.e. near real velocity).
    // By using CF it's possible to correct the drift of integrated accZ (velocity) without loosing the phase, i.e without delay
    vel = vel * barometerConfig->baro_cf_vel + baroVel * (1.0f - barometerConfig->baro_cf_vel);
    vel_tmp = lrintf(vel);

    // set vario
    vario = applyDeadband(vel_tmp, 5);

    altHoldThrottleAdjustment = calculateAltHoldThrottleAdjustment(vel_tmp, accZ_tmp, accZ_old);

    accZ_old = accZ_tmp;
}
Пример #2
0
void calculateEstimatedAltitude(uint32_t currentTime)
{
    static uint32_t previousTime;
    uint32_t dTime;
    int32_t baroVel;
    float dt;
    float vel_acc;
    int32_t vel_tmp;
    float accZ_tmp;
    int32_t sonarAlt = -1;
    static float accZ_old = 0.0f;
    static float vel = 0.0f;
    static float accAlt = 0.0f;
    static int32_t lastBaroAlt;

    static int32_t baroAlt_offset = 0;
    float sonarTransition;

#ifdef SONAR
    int16_t tiltAngle;
#endif

    dTime = currentTime - previousTime;
    if (dTime < BARO_UPDATE_FREQUENCY_40HZ)
        return;

    previousTime = currentTime;

#ifdef BARO
    if (!isBaroCalibrationComplete()) {
        performBaroCalibrationCycle();
        vel = 0;
        accAlt = 0;
    }

    BaroAlt = baroCalculateAltitude();
#else
    BaroAlt = 0;
#endif

#ifdef SONAR
    tiltAngle = calculateTiltAngle(&inclination);
    sonarAlt = sonarRead();
    sonarAlt = sonarCalculateAltitude(sonarAlt, tiltAngle);
#endif

    if (sonarAlt > 0 && sonarAlt < 200) {
        baroAlt_offset = BaroAlt - sonarAlt;
        BaroAlt = sonarAlt;
    } else {
        BaroAlt -= baroAlt_offset;
        if (sonarAlt > 0  && sonarAlt <= 300) {
            sonarTransition = (300 - sonarAlt) / 100.0f;
            BaroAlt = sonarAlt * sonarTransition + BaroAlt * (1.0f - sonarTransition);
        }
    }

    dt = accTimeSum * 1e-6f; // delta acc reading time in seconds

    // Integrator - velocity, cm/sec
    if (accSumCount) {
        accZ_tmp = (float)accSum[2] / (float)accSumCount;
    } else {
        accZ_tmp = 0;
    }
    vel_acc = accZ_tmp * accVelScale * (float)accTimeSum;

    // Integrator - Altitude in cm
    accAlt += (vel_acc * 0.5f) * dt + vel * dt; 
    accalttemp=lrintf(100*accAlt); //Checking how acc measures height                                                                // integrate velocity to get distance (x= a/2 * t^2)
    accAlt = accAlt * barometerConfig->baro_cf_alt + (float)BaroAlt * (1.0f - barometerConfig->baro_cf_alt);    // complementary filter for altitude estimation (baro & acc)
    vel += vel_acc;

#ifdef DEBUG_ALT_HOLD
    debug[1] = accSum[2] / accSumCount; // acceleration
    debug[2] = vel;                     // velocity
    debug[3] = accAlt;                  // height
#endif

    imuResetAccelerationSum();

#ifdef BARO
    if (!isBaroCalibrationComplete()) {
        return;
    }
#endif

    if (sonarAlt > 0 && sonarAlt < 200) {
        // the sonar has the best range
        EstAlt = BaroAlt;
    } else {
        EstAlt = accAlt;
    }

    baroVel = (BaroAlt - lastBaroAlt) * 1000000.0f / dTime;
    lastBaroAlt = BaroAlt;

    baroVel = constrain(baroVel, -1500, 1500);  // constrain baro velocity +/- 1500cm/s
    baroVel = applyDeadband(baroVel, 10);       // to reduce noise near zero

    // apply Complimentary Filter to keep the calculated velocity based on baro velocity (i.e. near real velocity).
    // By using CF it's possible to correct the drift of integrated accZ (velocity) without loosing the phase, i.e without delay
    vel = vel * barometerConfig->baro_cf_vel + baroVel * (1.0f - barometerConfig->baro_cf_vel);
    vel_tmp = lrintf(vel);

    // set vario
    vario = applyDeadband(vel_tmp, 5);
     if (1)//!(ABS(rcData[THROTTLE] - initialThrottleHold) > rcControlsConfig->alt_hold_deadband))
     {
        altHoldThrottleAdjustment = calculateAltHoldThrottleAdjustment(vel_tmp, accZ_tmp, accZ_old);
     }//dronadrona_1200am
    Temp=pidProfile->I8[PIDALT];
    barometerConfig->baro_cf_alt=1-Temp/1000 ;
    accZ_old = accZ_tmp;
}
Пример #3
0
void calculateEstimatedAltitude(timeUs_t currentTimeUs)
{
    static timeUs_t previousTimeUs = 0;
    const uint32_t dTime = currentTimeUs - previousTimeUs;
    if (dTime < BARO_UPDATE_FREQUENCY_40HZ) {
        return;
    }
    previousTimeUs = currentTimeUs;

    static float vel = 0.0f;
    static float accAlt = 0.0f;

    int32_t baroAlt = 0;
#ifdef BARO
    if (sensors(SENSOR_BARO)) {
        if (!isBaroCalibrationComplete()) {
            performBaroCalibrationCycle();
            vel = 0;
            accAlt = 0;
        } else {
            baroAlt = baroCalculateAltitude();
            estimatedAltitude = baroAlt;
        }
    }
#endif

#ifdef SONAR
    if (sensors(SENSOR_SONAR)) {
        int32_t sonarAlt = sonarCalculateAltitude(sonarRead(), getCosTiltAngle());
        if (sonarAlt > 0 && sonarAlt >= sonarCfAltCm && sonarAlt <= sonarMaxAltWithTiltCm) {
            // SONAR in range, so use complementary filter
            float sonarTransition = (float)(sonarMaxAltWithTiltCm - sonarAlt) / (sonarMaxAltWithTiltCm - sonarCfAltCm);
            sonarAlt = (float)sonarAlt * sonarTransition + baroAlt * (1.0f - sonarTransition);
            estimatedAltitude = sonarAlt;
        }
    }
#endif

    float accZ_tmp = 0;
#ifdef ACC
    if (sensors(SENSOR_ACC)) {
        const float dt = accTimeSum * 1e-6f; // delta acc reading time in seconds

        // Integrator - velocity, cm/sec
        if (accSumCount) {
            accZ_tmp = (float)accSum[2] / accSumCount;
        }
        const float vel_acc = accZ_tmp * accVelScale * (float)accTimeSum;

        // Integrator - Altitude in cm
        accAlt += (vel_acc * 0.5f) * dt + vel * dt;  // integrate velocity to get distance (x= a/2 * t^2)
        accAlt = accAlt * CONVERT_PARAMETER_TO_FLOAT(barometerConfig()->baro_cf_alt) + (float)baro.BaroAlt * (1.0f - CONVERT_PARAMETER_TO_FLOAT(barometerConfig()->baro_cf_alt));    // complementary filter for altitude estimation (baro & acc)
        vel += vel_acc;
        estimatedAltitude = accAlt;
    }
#endif

    DEBUG_SET(DEBUG_ALTITUDE, DEBUG_ALTITUDE_ACC, accSum[2] / accSumCount);
    DEBUG_SET(DEBUG_ALTITUDE, DEBUG_ALTITUDE_VEL, vel);
    DEBUG_SET(DEBUG_ALTITUDE, DEBUG_ALTITUDE_HEIGHT, accAlt);

    imuResetAccelerationSum();

    int32_t baroVel = 0;
#ifdef BARO
    if (sensors(SENSOR_BARO)) {
        if (!isBaroCalibrationComplete()) {
            return;
        }

        static int32_t lastBaroAlt = 0;
        baroVel = (baroAlt - lastBaroAlt) * 1000000.0f / dTime;
        lastBaroAlt = baroAlt;

        baroVel = constrain(baroVel, -1500, 1500);  // constrain baro velocity +/- 1500cm/s
        baroVel = applyDeadband(baroVel, 10);       // to reduce noise near zero
    }
#endif

    // apply Complimentary Filter to keep the calculated velocity based on baro velocity (i.e. near real velocity).
    // By using CF it's possible to correct the drift of integrated accZ (velocity) without loosing the phase, i.e without delay
    vel = vel * CONVERT_PARAMETER_TO_FLOAT(barometerConfig()->baro_cf_vel) + baroVel * (1.0f - CONVERT_PARAMETER_TO_FLOAT(barometerConfig()->baro_cf_vel));
    int32_t vel_tmp = lrintf(vel);

    // set vario
    estimatedVario = applyDeadband(vel_tmp, 5);

    static float accZ_old = 0.0f;
    altHoldThrottleAdjustment = calculateAltHoldThrottleAdjustment(vel_tmp, accZ_tmp, accZ_old);
    accZ_old = accZ_tmp;
}