mirror of https://github.com/ArduPilot/ardupilot
AP_NavEKF2: remove internal-only getTiltError method
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5ad0ac6727
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@ -988,15 +988,6 @@ void NavEKF2::getGyroScaleErrorPercentage(int8_t instance, Vector3f &gyroScale)
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}
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}
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// return tilt error convergence metric for the specified instance
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void NavEKF2::getTiltError(int8_t instance, float &ang) const
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{
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if (instance < 0 || instance >= num_cores) instance = primary;
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if (core) {
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core[instance].getTiltError(ang);
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}
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}
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// reset body axis gyro bias estimates
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void NavEKF2::resetGyroBias(void)
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{
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@ -102,10 +102,6 @@ public:
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// An out of range instance (eg -1) returns data for the primary instance
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void getGyroScaleErrorPercentage(int8_t instance, Vector3f &gyroScale) const;
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// return tilt error convergence metric for the specified instance
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// An out of range instance (eg -1) returns data for the primary instance
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void getTiltError(int8_t instance, float &ang) const;
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// reset body axis gyro bias estimates
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void resetGyroBias(void);
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@ -128,8 +128,6 @@ void NavEKF2_core::Log_Write_NKF4(uint64_t time_us) const
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getFilterTimeouts(timeoutStatus);
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getFilterStatus(solutionStatus);
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getFilterGpsStatus(gpsStatus);
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float tiltError;
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getTiltError(tiltError);
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const struct log_NKF4 pkt4{
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LOG_PACKET_HEADER_INIT(LOG_NKF4_MSG),
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time_us : time_us,
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@ -139,7 +137,7 @@ void NavEKF2_core::Log_Write_NKF4(uint64_t time_us) const
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sqrtvarH : (int16_t)(100*hgtVar),
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sqrtvarM : (int16_t)(100*tempVar),
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sqrtvarVT : (int16_t)(100*tasVar),
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tiltErr : (float)tiltError,
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tiltErr : tiltErrFilt, // tilt error convergence metric
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offsetNorth : (int8_t)(offset.x),
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offsetEast : (int8_t)(offset.y),
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faults : _faultStatus,
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@ -105,12 +105,6 @@ void NavEKF2_core::getGyroScaleErrorPercentage(Vector3f &gyroScale) const
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gyroScale.z = 100.0f/stateStruct.gyro_scale.z - 100.0f;
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}
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// return tilt error convergence metric
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void NavEKF2_core::getTiltError(float &ang) const
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{
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ang = tiltErrFilt;
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}
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// return the transformation matrix from XYZ (body) to NED axes
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void NavEKF2_core::getRotationBodyToNED(Matrix3f &mat) const
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{
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@ -117,9 +117,6 @@ public:
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// return body axis gyro scale factor error as a percentage
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void getGyroScaleErrorPercentage(Vector3f &gyroScale) const;
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// return tilt error convergence metric
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void getTiltError(float &ang) const;
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// reset body axis gyro bias estimates
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void resetGyroBias(void);
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