mirror of https://github.com/ArduPilot/ardupilot
AP_InertialNav: Use separated EKF horiz/vert position interfaces
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@ -16,19 +16,27 @@
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*/
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void AP_InertialNav_NavEKF::update(float dt)
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{
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// get the position relative to the local earth frame origin
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if (_ahrs_ekf.get_relative_position_NED(_relpos_cm)) {
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_relpos_cm *= 100; // convert to cm
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_relpos_cm.z = - _relpos_cm.z; // InertialNav is NEU
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// get the NE position relative to the local earth frame origin
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Vector2f posNE;
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if (_ahrs_ekf.get_relative_position_NE(posNE)) {
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_relpos_cm.x = posNE.x * 100; // convert from m to cm
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_relpos_cm.y = posNE.y * 100; // convert from m to cm
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}
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// get the D position relative to the local earth frame origin
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float posD;
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if (_ahrs_ekf.get_relative_position_D(posD)) {
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_relpos_cm.z = - posD * 100; // convert from m in NED to cm in NEU
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}
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// get the absolute WGS-84 position
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_haveabspos = _ahrs_ekf.get_position(_abspos);
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// get the velocity relative to the local earth frame
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if (_ahrs_ekf.get_velocity_NED(_velocity_cm)) {
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_velocity_cm *= 100; // convert to cm/s
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_velocity_cm.z = -_velocity_cm.z; // InertialNav is NEU
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Vector3f velNED;
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if (_ahrs_ekf.get_velocity_NED(velNED)) {
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_velocity_cm = velNED * 100; // convert to cm/s
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_velocity_cm.z = -_velocity_cm.z; // convert from NED to NEU
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}
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// Get a derivative of the vertical position which is kinematically consistent with the vertical position is required by some control loops.
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