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mtecs: add altitude prefiltering
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@@ -59,6 +59,7 @@ mTecs::mTecs() :
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_controlAltitude(this, "FPA", true),
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_controlAirSpeed(this, "ACC"),
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_flightPathAngleLowpass(this, "FPA_LP"),
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_altitudeLowpass(this, "ALT_LP"),
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_airspeedLowpass(this, "A_LP"),
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_airspeedDerivative(this, "AD"),
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_throttleSp(0.0f),
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@@ -93,18 +94,23 @@ int mTecs::updateAltitudeSpeed(float flightPathAngle, float altitude, float alti
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/* time measurement */
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updateTimeMeasurement();
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/* Filter altitude */
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float altitudeFiltered = _altitudeLowpass.update(altitude);
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/* calculate flight path angle setpoint from altitude setpoint */
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float flightPathAngleSp = _controlAltitude.update(altitudeSp - altitude);
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float flightPathAngleSp = _controlAltitude.update(altitudeSp - altitudeFiltered);
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/* Debug output */
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if (_counter % 10 == 0) {
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debug("***");
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debug("updateAltitudeSpeed: altitudeSp %.4f, altitude %.4f, flightPathAngleSp %.4f", (double)altitudeSp, (double)altitude, (double)flightPathAngleSp);
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debug("updateAltitudeSpeed: altitudeSp %.4f, altitude %.4f, altitude filtered %.4f, flightPathAngleSp %.4f", (double)altitudeSp, (double)altitude, (double)altitudeFiltered, (double)flightPathAngleSp);
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}
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/* Write part of the status message */
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_status.altitudeSp = altitudeSp;
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_status.altitude = altitude;
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_status.altitudeFiltered = altitudeFiltered;
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/* use flightpath angle setpoint for total energy control */
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@@ -115,6 +115,7 @@ protected:
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/* Other calculation Blocks */
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control::BlockLowPass _flightPathAngleLowpass; /**< low pass filter for the flight path angle */
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control::BlockLowPass _altitudeLowpass; /**< low pass filter for altitude */
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control::BlockLowPass _airspeedLowpass; /**< low pass filter for airspeed */
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control::BlockDerivative _airspeedDerivative; /**< airspeed derivative calulation */
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@@ -174,6 +174,13 @@ PARAM_DEFINE_FLOAT(MT_PIT_MIN, -45.0f);
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*/
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PARAM_DEFINE_FLOAT(MT_PIT_MAX, 20.0f);
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/**
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* Lowpass (cutoff freq.) for altitude
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*
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* @group mTECS
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*/
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PARAM_DEFINE_FLOAT(MT_ALT_LP, 1.0f);
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/**
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* Lowpass (cutoff freq.) for the flight path angle
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*
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