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https://github.com/ArduPilot/ardupilot
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AP_NavEKF3: CorrectGPSForAntennaOffset made const
also reduce scope of call to slightly reduce CPU load
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@ -28,9 +28,6 @@ void NavEKF3_core::ResetVelocity(void)
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zeroRows(P,4,5);
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zeroRows(P,4,5);
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zeroCols(P,4,5);
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zeroCols(P,4,5);
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gps_elements gps_corrected = gpsDataNew;
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CorrectGPSForAntennaOffset(gps_corrected);
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if (PV_AidingMode != AID_ABSOLUTE) {
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if (PV_AidingMode != AID_ABSOLUTE) {
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stateStruct.velocity.zero();
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stateStruct.velocity.zero();
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// set the variances using the measurement noise parameter
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// set the variances using the measurement noise parameter
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@ -38,6 +35,9 @@ void NavEKF3_core::ResetVelocity(void)
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} else {
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} else {
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// reset horizontal velocity states to the GPS velocity if available
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// reset horizontal velocity states to the GPS velocity if available
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if ((imuSampleTime_ms - lastTimeGpsReceived_ms < 250 && velResetSource == DEFAULT) || velResetSource == GPS) {
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if ((imuSampleTime_ms - lastTimeGpsReceived_ms < 250 && velResetSource == DEFAULT) || velResetSource == GPS) {
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// correct for antenna position
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gps_elements gps_corrected = gpsDataNew;
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CorrectGPSForAntennaOffset(gps_corrected);
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stateStruct.velocity.x = gps_corrected.vel.x;
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stateStruct.velocity.x = gps_corrected.vel.x;
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stateStruct.velocity.y = gps_corrected.vel.y;
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stateStruct.velocity.y = gps_corrected.vel.y;
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// set the variances using the reported GPS speed accuracy
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// set the variances using the reported GPS speed accuracy
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@ -94,11 +94,11 @@ void NavEKF3_core::ResetPosition(void)
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// set the variances using the position measurement noise parameter
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// set the variances using the position measurement noise parameter
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P[7][7] = P[8][8] = sq(frontend->_gpsHorizPosNoise);
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P[7][7] = P[8][8] = sq(frontend->_gpsHorizPosNoise);
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} else {
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} else {
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gps_elements gps_corrected = gpsDataNew;
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CorrectGPSForAntennaOffset(gps_corrected);
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// Use GPS data as first preference if fresh data is available
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// Use GPS data as first preference if fresh data is available
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if ((imuSampleTime_ms - lastTimeGpsReceived_ms < 250 && posResetSource == DEFAULT) || posResetSource == GPS) {
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if ((imuSampleTime_ms - lastTimeGpsReceived_ms < 250 && posResetSource == DEFAULT) || posResetSource == GPS) {
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// correct for antenna position
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gps_elements gps_corrected = gpsDataNew;
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CorrectGPSForAntennaOffset(gps_corrected);
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// record the ID of the GPS for the data we are using for the reset
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// record the ID of the GPS for the data we are using for the reset
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last_gps_idx = gps_corrected.sensor_idx;
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last_gps_idx = gps_corrected.sensor_idx;
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// write to state vector and compensate for offset between last GPS measurement and the EKF time horizon
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// write to state vector and compensate for offset between last GPS measurement and the EKF time horizon
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@ -249,7 +249,7 @@ bool NavEKF3_core::resetHeightDatum(void)
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/*
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/*
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correct GPS data for position offset of antenna phase centre relative to the IMU
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correct GPS data for position offset of antenna phase centre relative to the IMU
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*/
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*/
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void NavEKF3_core::CorrectGPSForAntennaOffset(gps_elements &gps_data)
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void NavEKF3_core::CorrectGPSForAntennaOffset(gps_elements &gps_data) const
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{
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{
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const Vector3f &posOffsetBody = AP::gps().get_antenna_offset(gps_data.sensor_idx) - accelPosOffset;
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const Vector3f &posOffsetBody = AP::gps().get_antenna_offset(gps_data.sensor_idx) - accelPosOffset;
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if (posOffsetBody.is_zero()) {
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if (posOffsetBody.is_zero()) {
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@ -865,7 +865,7 @@ private:
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void updateStateIndexLim(void);
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void updateStateIndexLim(void);
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// correct GPS data for antenna position
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// correct GPS data for antenna position
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void CorrectGPSForAntennaOffset(gps_elements &gps_data);
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void CorrectGPSForAntennaOffset(gps_elements &gps_data) const;
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// Variables
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// Variables
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bool statesInitialised; // boolean true when filter states have been initialised
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bool statesInitialised; // boolean true when filter states have been initialised
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