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Remove airspeed and altitude raw data from TECS log, as we have these quantities already in the system log
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@@ -109,8 +109,7 @@ int mTecs::updateAltitudeSpeed(float flightPathAngle, float altitude, float alti
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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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_status.altitude_filtered = altitudeFiltered;
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/* use flightpath angle setpoint for total energy control */
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@@ -146,8 +145,7 @@ int mTecs::updateFlightPathAngleSpeed(float flightPathAngle, float flightPathAng
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/* Write part of the status message */
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_status.airspeedSp = airspeedSp;
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_status.airspeed = airspeed;
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_status.airspeedFiltered = airspeedFiltered;
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_status.airspeed_filtered = airspeedFiltered;
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/* use longitudinal acceleration setpoint for total energy control */
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