mirror of https://github.com/ArduPilot/ardupilot
AP_NavEKF3: remove unused getAccelNED method
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@ -1170,14 +1170,6 @@ float NavEKF3::getPosDownDerivative(int8_t instance) const
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return 0.0f;
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}
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// This returns the specific forces in the NED frame
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void NavEKF3::getAccelNED(Vector3f &accelNED) const
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{
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if (core) {
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core[primary].getAccelNED(accelNED);
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}
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}
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// return body axis gyro bias estimates in rad/sec
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void NavEKF3::getGyroBias(int8_t instance, Vector3f &gyroBias) const
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{
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@ -93,9 +93,6 @@ public:
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// but will always be kinematically consistent with the z component of the EKF position state
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float getPosDownDerivative(int8_t instance) const;
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// This returns the specific forces in the NED frame
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void getAccelNED(Vector3f &accelNED) const;
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// return body axis gyro bias estimates in rad/sec 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 getGyroBias(int8_t instance, Vector3f &gyroBias) const;
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@ -216,12 +216,6 @@ float NavEKF3_core::getPosDownDerivative(void) const
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return vertCompFiltState.vel + velOffsetNED.z;
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}
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// This returns the specific forces in the NED frame
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void NavEKF3_core::getAccelNED(Vector3f &accelNED) const {
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accelNED = velDotNED;
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accelNED.z -= GRAVITY_MSS;
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}
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// Write the last estimated NE position of the body frame origin relative to the reference point (m).
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// Return true if the estimate is valid
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bool NavEKF3_core::getPosNE(Vector2f &posNE) const
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@ -125,9 +125,6 @@ public:
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// but will always be kinematically consistent with the z component of the EKF position state
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float getPosDownDerivative(void) const;
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// This returns the specific forces in the NED frame
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void getAccelNED(Vector3f &accelNED) const;
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// return body axis gyro bias estimates in rad/sec
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void getGyroBias(Vector3f &gyroBias) const;
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