/// -*- 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 */ /** * initializes the object. */ void AP_InertialNav_NavEKF::init() { AP_InertialNav::init(); } /** update internal state */ void AP_InertialNav_NavEKF::update(float dt) { AP_InertialNav::update(dt); _ahrs.get_relative_position_NED(_relpos_cm); _relpos_cm *= 100; // convert to cm _haveabspos = _ahrs.get_position(_abspos); _ahrs.get_velocity_NED(_velocity_cm); _velocity_cm *= 100; // convert to cm/s // InertialNav is NEU _relpos_cm.z = - _relpos_cm.z; _velocity_cm.z = -_velocity_cm.z; } /** * position_ok - true if inertial based altitude and position can be trusted * @return */ bool AP_InertialNav_NavEKF::position_ok() const { if (_ahrs.have_inertial_nav() && _haveabspos) { return true; } return AP_InertialNav::position_ok(); } /** * 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 &AP_InertialNav_NavEKF::get_position(void) const { if (_ahrs.have_inertial_nav()) { return _relpos_cm; } return AP_InertialNav::get_position(); } /** * 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 { if (_ahrs.have_inertial_nav() && _haveabspos) { return _abspos.lat; } return AP_InertialNav::get_latitude(); } /** * 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 { if (_ahrs.have_inertial_nav() && _haveabspos) { return _abspos.lng; } return AP_InertialNav::get_longitude(); } /** * get_latitude_diff - returns the current latitude difference from the home location. * * @return difference in 100 nano degrees (i.e. degree value multiplied by 10,000,000) */ float AP_InertialNav_NavEKF::get_latitude_diff() const { if (_ahrs.have_inertial_nav()) { return _relpos_cm.x / LATLON_TO_CM; } return AP_InertialNav::get_latitude_diff(); } /** * get_longitude_diff - returns the current longitude difference from the home location. * * @return difference in 100 nano degrees (i.e. degree value multiplied by 10,000,000) */ float AP_InertialNav_NavEKF::get_longitude_diff() const { if (_ahrs.have_inertial_nav()) { return _relpos_cm.y / _lon_to_cm_scaling; } return AP_InertialNav::get_longitude_diff(); } /** * 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 { if (_ahrs.have_inertial_nav()) { return _velocity_cm; } return AP_InertialNav::get_velocity(); } /** * 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 { if (_ahrs.have_inertial_nav()) { return pythagorous2(_velocity_cm.x, _velocity_cm.y); } return AP_InertialNav::get_velocity_xy(); } /** * altitude_ok - returns true if inertial based altitude and position can be trusted * @return */ bool AP_InertialNav_NavEKF::altitude_ok() const { if (_ahrs.have_inertial_nav() && _haveabspos) { return true; } return AP_InertialNav::altitude_ok(); } /** * get_altitude - get latest altitude estimate in cm * @return */ float AP_InertialNav_NavEKF::get_altitude() const { if (_ahrs.have_inertial_nav()) { return _relpos_cm.z; } return AP_InertialNav::get_altitude(); } /** * get_velocity_z - returns the current climbrate. * * @see get_velocity().z * * @return climbrate in cm/s */ float AP_InertialNav_NavEKF::get_velocity_z() const { if (_ahrs.have_inertial_nav()) { return _velocity_cm.z; } return AP_InertialNav::get_velocity_z(); } #endif // AP_AHRS_NAVEKF_AVAILABLE