mirror of https://github.com/ArduPilot/ardupilot
AP_InertialNav: remove unused get_hgt_ctrl_limit
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@ -104,14 +104,6 @@ public:
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*/
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virtual float get_altitude() const = 0;
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/**
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* get_hgt_ctrl_limit - get maximum height to be observed by the control loops in cm and a validity flag
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* this is used to limit height during optical flow navigation
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* it will return invalid when no limiting is required
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* @return
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*/
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virtual bool get_hgt_ctrl_limit(float& limit) const = 0;
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/**
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* get_velocity_z - returns the current climbrate.
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*
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@ -158,23 +158,6 @@ bool AP_InertialNav_NavEKF::get_hagl(float &height) const
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return valid;
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}
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/**
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* get_hgt_ctrl_limit - get maximum height to be observed by the control loops in cm and a validity flag
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* this is used to limit height during optical flow navigation
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* it will return invalid when no limiting is required
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* @return
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*/
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bool AP_InertialNav_NavEKF::get_hgt_ctrl_limit(float& limit) const
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{
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// true when estimate is valid
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if (_ahrs_ekf.get_hgt_ctrl_limit(limit)) {
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// convert height from m to cm
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limit *= 100.0f;
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return true;
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}
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return false;
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}
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/**
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* get_velocity_z - returns the current climbrate.
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*
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@ -94,14 +94,6 @@ public:
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*/
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bool get_hagl(float &hagl) const;
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/**
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* get_hgt_ctrl_limit - get maximum height to be observed by the control loops in cm and a validity flag
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* this is used to limit height during optical flow navigation
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* it will return invalid when no limiting is required
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* @return
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*/
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bool get_hgt_ctrl_limit(float& limit) const;
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/**
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* get_velocity_z - returns the current climbrate.
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*
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