forked from Archive/PX4-Autopilot
Remove output argument from calcEarthRateNed
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@ -641,7 +641,7 @@ private:
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void fuse(float *K, float innovation);
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// calculate the earth rotation vector from a given latitude
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void calcEarthRateNED(Vector3f &omega, float lat_rad) const;
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Vector3f calcEarthRateNED(float lat_rad) const;
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// return true id the GPS quality is good enough to set an origin and start aiding
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bool gps_is_good(const gps_message &gps);
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@ -791,11 +791,11 @@ void Ekf::constrainStates()
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}
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// calculate the earth rotation vector
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void Ekf::calcEarthRateNED(Vector3f &omega, float lat_rad) const
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Vector3f Ekf::calcEarthRateNED(float lat_rad) const
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{
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omega(0) = CONSTANTS_EARTH_SPIN_RATE * cosf(lat_rad);
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omega(1) = 0.0f;
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omega(2) = -CONSTANTS_EARTH_SPIN_RATE * sinf(lat_rad);
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return Vector3f{CONSTANTS_EARTH_SPIN_RATE * cosf(lat_rad),
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0.0f,
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-CONSTANTS_EARTH_SPIN_RATE * sinf(lat_rad)};
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}
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void Ekf::getGpsVelPosInnov(float hvel[2], float &vvel, float hpos[2], float &vpos)
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@ -76,7 +76,7 @@ bool Ekf::collect_gps(const gps_message &gps)
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// Take the current GPS height and subtract the filter height above origin to estimate the GPS height of the origin
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_gps_alt_ref = 1e-3f * (float)gps.alt + _state.pos(2);
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_NED_origin_initialised = true;
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calcEarthRateNED(_earth_rate_NED, (float)_pos_ref.lat_rad);
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_earth_rate_NED = calcEarthRateNED((float)_pos_ref.lat_rad);
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_last_gps_origin_time_us = _time_last_imu;
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// set the magnetic field data returned by the geo library using the current GPS position
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