/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #include #include "AP_InertialNav.h" #if AP_AHRS_NAVEKF_AVAILABLE /* 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 */ /** update internal state */ void AP_InertialNav_NavEKF::update(float dt) { _ahrs_ekf.get_NavEKF().getPosNED(_relpos_cm); _relpos_cm *= 100; // convert to cm _haveabspos = _ahrs_ekf.get_position(_abspos); _ahrs_ekf.get_NavEKF().getVelNED(_velocity_cm); _velocity_cm *= 100; // convert to cm/s // InertialNav is NEU _relpos_cm.z = - _relpos_cm.z; _velocity_cm.z = -_velocity_cm.z; } /** * get_filter_status : returns filter status as a series of flags */ nav_filter_status AP_InertialNav_NavEKF::get_filter_status() const { nav_filter_status ret; _ahrs_ekf.get_NavEKF().getFilterStatus(ret); return ret; } /** * get_origin - returns the inertial navigation origin in lat/lon/alt */ struct Location AP_InertialNav_NavEKF::get_origin() const { struct Location ret; if (!_ahrs_ekf.get_NavEKF().getOriginLLH(ret)) { // initialise location to all zeros if origin not yet set memset(&ret, 0, sizeof(ret)); } return ret; } /** * get_position - returns the current position relative to the home location in cm. * * @return */ const Vector3f &AP_InertialNav_NavEKF::get_position(void) const { return _relpos_cm; } /** * get_location - updates the provided location with the latest calculated locatoin * returns true on success (i.e. the EKF knows it's latest position), false on failure */ bool AP_InertialNav_NavEKF::get_location(struct Location &loc) const { return _ahrs_ekf.get_NavEKF().getLLH(loc); } /** * 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 AP_InertialNav_NavEKF::get_latitude() const { return _abspos.lat; } /** * 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 AP_InertialNav_NavEKF::get_longitude() const { return _abspos.lng; } /** * 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 &AP_InertialNav_NavEKF::get_velocity() const { return _velocity_cm; } /** * get_velocity_xy - returns the current horizontal velocity in cm/s * * @returns the current horizontal velocity in cm/s */ float AP_InertialNav_NavEKF::get_velocity_xy() const { return pythagorous2(_velocity_cm.x, _velocity_cm.y); } /** * get_altitude - get latest altitude estimate in cm * @return */ float AP_InertialNav_NavEKF::get_altitude() const { return _relpos_cm.z; } /** * getHgtAboveGnd - get latest height above ground level estimate in cm and a validity flag * * @return */ bool AP_InertialNav_NavEKF::get_hagl(float height) const { // true when estimate is valid bool valid = _ahrs_ekf.get_NavEKF().getHAGL(height); // convert height from m to cm height *= 100.0f; return valid; } /** * 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 AP_InertialNav_NavEKF::get_hgt_ctrl_limit(float& limit) const { // true when estimate is valid if (_ahrs_ekf.get_NavEKF().getHeightControlLimit(limit)) { // convert height from m to cm limit *= 100.0f; return true; } return false; } /** * get_velocity_z - returns the current climbrate. * * @see get_velocity().z * * @return climbrate in cm/s */ float AP_InertialNav_NavEKF::get_velocity_z() const { return _velocity_cm.z; } #endif // AP_AHRS_NAVEKF_AVAILABLE