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https://github.com/ArduPilot/ardupilot
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AP_NavEKF2: Remove unused function
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@ -768,19 +768,6 @@ bool NavEKF2::getHeightControlLimit(float &height) const
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return core->getHeightControlLimit(height);
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return core->getHeightControlLimit(height);
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}
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}
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// provides the quaternion that was used by the INS calculation to
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// rotate from the previous orientation to the orientaion at the
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// current time step
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// returns a zero rotation quaternion if the INS
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// calculation was not performed on that time step.
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Quaternion NavEKF2::getDeltaQuaternion(void) const
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{
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if (!core) {
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return Quaternion();
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}
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return core->getDeltaQuaternion();
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}
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// return the amount of yaw angle change due to the last yaw angle reset in radians
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// return the amount of yaw angle change due to the last yaw angle reset in radians
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// returns true if a reset yaw angle has been updated and not queried
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// returns true if a reset yaw angle has been updated and not queried
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// this function should not have more than one client
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// this function should not have more than one client
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@ -216,10 +216,6 @@ public:
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// this is needed to ensure the vehicle does not fly too high when using optical flow navigation
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// this is needed to ensure the vehicle does not fly too high when using optical flow navigation
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bool getHeightControlLimit(float &height) const;
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bool getHeightControlLimit(float &height) const;
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// provides the quaternion that was used by the INS calculation to rotate from the previous orientation to the orientaion at the current time step
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// returns a zero rotation quaternion if the INS calculation was not performed on that time step.
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Quaternion getDeltaQuaternion(void) const;
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// return the amount of yaw angle change due to the last yaw angle reset in radians
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// return the amount of yaw angle change due to the last yaw angle reset in radians
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// returns true if a reset yaw angle has been updated and not queried
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// returns true if a reset yaw angle has been updated and not queried
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// this function should not have more than one client
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// this function should not have more than one client
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@ -4807,14 +4807,6 @@ bool NavEKF2_core::getHeightControlLimit(float &height) const
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}
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}
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}
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}
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// provides the delta quaternion that was used by the INS calculation to rotate from the previous orientation to the orientation at the current time
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// the delta quaternion returned will be a zero rotation if the INS calculation was not performed on that time step
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Quaternion NavEKF2_core::getDeltaQuaternion(void) const
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{
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// Note: correctedDelAngQuat is reset to a zero rotation at the start of every update cycle in UpdateFilter()
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return correctedDelAngQuat;
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}
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// return the quaternions defining the rotation from NED to XYZ (body) axes
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// return the quaternions defining the rotation from NED to XYZ (body) axes
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void NavEKF2_core::getQuaternion(Quaternion& ret) const
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void NavEKF2_core::getQuaternion(Quaternion& ret) const
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{
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{
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@ -209,10 +209,6 @@ public:
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// this is needed to ensure the vehicle does not fly too high when using optical flow navigation
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// this is needed to ensure the vehicle does not fly too high when using optical flow navigation
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bool getHeightControlLimit(float &height) const;
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bool getHeightControlLimit(float &height) const;
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// provides the quaternion that was used by the INS calculation to rotate from the previous orientation to the orientaion at the current time step
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// returns a zero rotation quaternion if the INS calculation was not performed on that time step.
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Quaternion getDeltaQuaternion(void) const;
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// return the amount of yaw angle change due to the last yaw angle reset in radians
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// return the amount of yaw angle change due to the last yaw angle reset in radians
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// returns true if a reset yaw angle has been updated and not queried
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// returns true if a reset yaw angle has been updated and not queried
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// this function should not have more than one client
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// this function should not have more than one client
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