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AP_NavEKF2: fix documentation errors
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@ -673,7 +673,7 @@ int8_t NavEKF2::getPrimaryCoreIndex(void) const
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return primary;
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return primary;
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}
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}
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// Return the last calculated NE position relative to the reference point (m).
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// Write the last calculated NE position relative to the reference point (m).
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// If a calculated solution is not available, use the best available data and return false
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// If a calculated solution is not available, use the best available data and return false
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// If false returned, do not use for flight control
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// If false returned, do not use for flight control
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bool NavEKF2::getPosNE(int8_t instance, Vector2f &posNE)
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bool NavEKF2::getPosNE(int8_t instance, Vector2f &posNE)
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@ -685,7 +685,7 @@ bool NavEKF2::getPosNE(int8_t instance, Vector2f &posNE)
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return core[instance].getPosNE(posNE);
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return core[instance].getPosNE(posNE);
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}
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}
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// Return the last calculated D position relative to the reference point (m).
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// Write the last calculated D position relative to the reference point (m).
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// If a calculated solution is not available, use the best available data and return false
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// If a calculated solution is not available, use the best available data and return false
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// If false returned, do not use for flight control
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// If false returned, do not use for flight control
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bool NavEKF2::getPosD(int8_t instance, float &posD)
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bool NavEKF2::getPosD(int8_t instance, float &posD)
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@ -62,13 +62,13 @@ public:
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// return -1 if no primary core selected
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// return -1 if no primary core selected
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int8_t getPrimaryCoreIndex(void) const;
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int8_t getPrimaryCoreIndex(void) const;
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// Return the last calculated NE position relative to the reference point (m) for the specified instance.
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// Write the last calculated NE position relative to the reference point (m) for the specified instance.
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// An out of range instance (eg -1) returns data for the the primary instance
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// An out of range instance (eg -1) returns data for the the primary instance
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// If a calculated solution is not available, use the best available data and return false
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// If a calculated solution is not available, use the best available data and return false
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// If false returned, do not use for flight control
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// If false returned, do not use for flight control
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bool getPosNE(int8_t instance, Vector2f &posNE);
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bool getPosNE(int8_t instance, Vector2f &posNE);
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// Return the last calculated D position relative to the reference point (m) for the specified instance.
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// Write the last calculated D position relative to the reference point (m) for the specified instance.
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// An out of range instance (eg -1) returns data for the the primary instance
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// An out of range instance (eg -1) returns data for the the primary instance
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// If a calculated solution is not available, use the best available data and return false
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// If a calculated solution is not available, use the best available data and return false
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// If false returned, do not use for flight control
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// If false returned, do not use for flight control
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@ -209,7 +209,7 @@ void NavEKF2_core::getAccelZBias(float &zbias) const {
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}
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}
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}
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}
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// Return the last estimated NE position relative to the reference point (m).
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// Write the last estimated NE position relative to the reference point (m).
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// Return true if the estimate is valid
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// Return true if the estimate is valid
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bool NavEKF2_core::getPosNE(Vector2f &posNE) const
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bool NavEKF2_core::getPosNE(Vector2f &posNE) const
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{
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{
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@ -245,7 +245,7 @@ bool NavEKF2_core::getPosNE(Vector2f &posNE) const
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return false;
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return false;
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}
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}
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// Return the last calculated D position relative to the reference point (m).
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// Write the last calculated D position relative to the reference point (m).
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// Return true if the estimte is valid
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// Return true if the estimte is valid
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bool NavEKF2_core::getPosD(float &posD) const
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bool NavEKF2_core::getPosD(float &posD) const
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{
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{
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@ -66,12 +66,12 @@ public:
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// Intended to be used by the front-end to determine which is the primary EKF
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// Intended to be used by the front-end to determine which is the primary EKF
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float faultScore(void) const;
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float faultScore(void) const;
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// Return the last calculated NE position relative to the reference point (m).
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// Write the last calculated NE position relative to the reference point (m).
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// If a calculated solution is not available, use the best available data and return false
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// If a calculated solution is not available, use the best available data and return false
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// If false returned, do not use for flight control
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// If false returned, do not use for flight control
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bool getPosNE(Vector2f &posNE) const;
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bool getPosNE(Vector2f &posNE) const;
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// Return the last calculated D position relative to the reference point (m).
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// Write the last calculated D position relative to the reference point (m).
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// If a calculated solution is not available, use the best available data and return false
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// If a calculated solution is not available, use the best available data and return false
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// If false returned, do not use for flight control
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// If false returned, do not use for flight control
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bool getPosD(float &posD) const;
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bool getPosD(float &posD) const;
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