/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- /* A wrapper around the AP_InertialNav class which uses the NavEKF filter if available, and falls back to the AP_InertialNav filter when EKF is not available */ #ifndef __AP_INERTIALNAV_NAVEKF_H__ #define __AP_INERTIALNAV_NAVEKF_H__ #include // definitions shared by inertial and ekf nav filters class AP_InertialNav_NavEKF : public AP_InertialNav { public: // Constructor AP_InertialNav_NavEKF(AP_AHRS_NavEKF &ahrs) : AP_InertialNav(), _haveabspos(false), _ahrs_ekf(ahrs) {} /** update internal state */ void update(float dt); /** * get_filter_status - returns filter status as a series of flags */ nav_filter_status get_filter_status() const; /** * get_origin - returns the inertial navigation origin in lat/lon/alt * * @return origin Location */ struct Location get_origin() const; /** * get_position - returns the current position relative to the home location in cm. * * the home location was set with AP_InertialNav::set_home_position(int32_t, int32_t) * * @return */ const Vector3f& get_position() const; /** * get_llh - updates the provided location with the latest calculated location including absolute altitude * returns true on success (i.e. the EKF knows it's latest position), false on failure */ bool get_location(struct Location &loc) const; /** * get_latitude - returns the latitude of the current position estimation in 100 nano degrees (i.e. degree value multiplied by 10,000,000) */ int32_t get_latitude() const; /** * get_longitude - returns the longitude of the current position estimation in 100 nano degrees (i.e. degree value multiplied by 10,000,000) * @return */ int32_t get_longitude() const; /** * get_velocity - returns the current velocity in cm/s * * @return velocity vector: * .x : latitude velocity in cm/s * .y : longitude velocity in cm/s * .z : vertical velocity in cm/s */ const Vector3f& get_velocity() const; /** * get_velocity_xy - returns the current horizontal velocity in cm/s * * @returns the current horizontal velocity in cm/s */ float get_velocity_xy() const; /** * get_altitude - get latest altitude estimate in cm * @return */ float get_altitude() const; /** * getHgtAboveGnd - get latest altitude estimate above ground level in centimetres and validity flag * @return */ bool get_hagl(float hagl) const; /** * get_hgt_ctrl_limit - get maximum height to be observed by the control loops in cm and a validity flag * this is used to limit height during optical flow navigation * it will return invalid when no limiting is required * @return */ bool get_hgt_ctrl_limit(float& limit) const; /** * get_velocity_z - returns the current climbrate. * * @see get_velocity().z * * @return climbrate in cm/s */ float get_velocity_z() const; private: Vector3f _relpos_cm; // NEU Vector3f _velocity_cm; // NEU struct Location _abspos; bool _haveabspos; AP_AHRS_NavEKF &_ahrs_ekf; }; #endif // __AP_INERTIALNAV_NAVEKF_H__