diff options
Diffstat (limited to 'src/modules/fw_pos_control_l1')
| -rw-r--r-- | src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp | 44 |
1 files changed, 22 insertions, 22 deletions
diff --git a/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp b/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp index ee0aca69e..5699fa1bb 100644 --- a/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp +++ b/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp @@ -183,7 +183,7 @@ private: uint64_t _airspeed_last_valid; ///< last time airspeed was valid. Used to detect sensor failures float _groundspeed_undershoot; ///< ground speed error to min. speed in m/s bool _global_pos_valid; ///< global position is valid - math::Dcm _R_nb; ///< current attitude + math::Matrix<3, 3> _R_nb; ///< current attitude ECL_L1_Pos_Controller _l1_control; TECS _tecs; @@ -322,11 +322,11 @@ private: /** * Control position. */ - bool control_position(const math::Vector2f &global_pos, const math::Vector2f &ground_speed, + bool control_position(const math::Vector<2> &global_pos, const math::Vector<2> &ground_speed, const struct mission_item_triplet_s &_mission_item_triplet); float calculate_target_airspeed(float airspeed_demand); - void calculate_gndspeed_undershoot(const math::Vector2f ¤t_position, const math::Vector2f &ground_speed, const struct mission_item_triplet_s &mission_item_triplet); + void calculate_gndspeed_undershoot(const math::Vector<2> ¤t_position, const math::Vector<2> &ground_speed, const struct mission_item_triplet_s &mission_item_triplet); /** * Shim for calling task_main from task_create. @@ -685,13 +685,13 @@ FixedwingPositionControl::calculate_target_airspeed(float airspeed_demand) } void -FixedwingPositionControl::calculate_gndspeed_undershoot(const math::Vector2f ¤t_position, const math::Vector2f &ground_speed, const struct mission_item_triplet_s &mission_item_triplet) +FixedwingPositionControl::calculate_gndspeed_undershoot(const math::Vector<2> ¤t_position, const math::Vector<2> &ground_speed, const struct mission_item_triplet_s &mission_item_triplet) { if (_global_pos_valid) { /* rotate ground speed vector with current attitude */ - math::Vector2f yaw_vector(_R_nb(0, 0), _R_nb(1, 0)); + math::Vector<2> yaw_vector(_R_nb(0, 0), _R_nb(1, 0)); yaw_vector.normalize(); float ground_speed_body = yaw_vector * ground_speed; @@ -702,7 +702,7 @@ FixedwingPositionControl::calculate_gndspeed_undershoot(const math::Vector2f &cu distance = get_distance_to_next_waypoint(mission_item_triplet.previous.lat, mission_item_triplet.previous.lon, mission_item_triplet.current.lat, mission_item_triplet.current.lon); delta_altitude = mission_item_triplet.current.altitude - mission_item_triplet.previous.altitude; } else { - distance = get_distance_to_next_waypoint(current_position.getX(), current_position.getY(), mission_item_triplet.current.lat, mission_item_triplet.current.lon); + distance = get_distance_to_next_waypoint(current_position(0), current_position(1), mission_item_triplet.current.lat, mission_item_triplet.current.lon); delta_altitude = mission_item_triplet.current.altitude - _global_pos.alt; } @@ -735,7 +735,7 @@ void FixedwingPositionControl::navigation_capabilities_publish() } bool -FixedwingPositionControl::control_position(const math::Vector2f ¤t_position, const math::Vector2f &ground_speed, +FixedwingPositionControl::control_position(const math::Vector<2> ¤t_position, const math::Vector<2> &ground_speed, const struct mission_item_triplet_s &mission_item_triplet) { bool setpoint = true; @@ -748,8 +748,8 @@ FixedwingPositionControl::control_position(const math::Vector2f ¤t_positio float baro_altitude = _global_pos.alt; /* filter speed and altitude for controller */ - math::Vector3 accel_body(_accel.x, _accel.y, _accel.z); - math::Vector3 accel_earth = _R_nb.transpose() * accel_body; + math::Vector<3> accel_body(_accel.x, _accel.y, _accel.z); + math::Vector<3> accel_earth = _R_nb.transposed() * accel_body; _tecs.update_50hz(baro_altitude, _airspeed.indicated_airspeed_m_s, _R_nb, accel_body, accel_earth); float altitude_error = _mission_item_triplet.current.altitude - _global_pos.alt; @@ -770,26 +770,26 @@ FixedwingPositionControl::control_position(const math::Vector2f ¤t_positio _tecs.set_speed_weight(_parameters.speed_weight); /* current waypoint (the one currently heading for) */ - math::Vector2f next_wp(mission_item_triplet.current.lat, mission_item_triplet.current.lon); + math::Vector<2> next_wp(mission_item_triplet.current.lat, mission_item_triplet.current.lon); /* current waypoint (the one currently heading for) */ - math::Vector2f curr_wp(mission_item_triplet.current.lat, mission_item_triplet.current.lon); + math::Vector<2> curr_wp(mission_item_triplet.current.lat, mission_item_triplet.current.lon); /* previous waypoint */ - math::Vector2f prev_wp; + math::Vector<2> prev_wp; if (mission_item_triplet.previous_valid) { - prev_wp.setX(mission_item_triplet.previous.lat); - prev_wp.setY(mission_item_triplet.previous.lon); + prev_wp(0) = mission_item_triplet.previous.lat; + prev_wp(1) = mission_item_triplet.previous.lon; } else { /* * No valid previous waypoint, go for the current wp. * This is automatically handled by the L1 library. */ - prev_wp.setX(mission_item_triplet.current.lat); - prev_wp.setY(mission_item_triplet.current.lon); + prev_wp(0) = mission_item_triplet.current.lat; + prev_wp(1) = mission_item_triplet.current.lon; } @@ -825,7 +825,7 @@ FixedwingPositionControl::control_position(const math::Vector2f ¤t_positio /* Horizontal landing control */ /* switch to heading hold for the last meters, continue heading hold after */ - float wp_distance = get_distance_to_next_waypoint(current_position.getX(), current_position.getY(), curr_wp.getX(), curr_wp.getY()); + float wp_distance = get_distance_to_next_waypoint(current_position(0), current_position(1), curr_wp(0), curr_wp(1)); //warnx("wp dist: %d, alt err: %d, noret: %s", (int)wp_distance, (int)altitude_error, (land_noreturn) ? "YES" : "NO"); if (wp_distance < _parameters.land_heading_hold_horizontal_distance || land_noreturn_horizontal) { @@ -874,7 +874,7 @@ FixedwingPositionControl::control_position(const math::Vector2f ¤t_positio float airspeed_land = 1.3f * _parameters.airspeed_min; float airspeed_approach = 1.3f * _parameters.airspeed_min; - float L_wp_distance = get_distance_to_next_waypoint(prev_wp.getX(), prev_wp.getY(), curr_wp.getX(), curr_wp.getY()) * _parameters.land_slope_length; + float L_wp_distance = get_distance_to_next_waypoint(prev_wp(0), prev_wp(1), curr_wp(0), curr_wp(1)) * _parameters.land_slope_length; float L_altitude = landingslope.getLandingSlopeAbsoluteAltitude(L_wp_distance, _mission_item_triplet.current.altitude);//getLandingSlopeAbsoluteAltitude(L_wp_distance, _mission_item_triplet.current.altitude, landing_slope_angle_rad, horizontal_slope_displacement); float landing_slope_alt_desired = landingslope.getLandingSlopeAbsoluteAltitude(wp_distance, _mission_item_triplet.current.altitude);//getLandingSlopeAbsoluteAltitude(wp_distance, _mission_item_triplet.current.altitude, landing_slope_angle_rad, horizontal_slope_displacement); @@ -993,8 +993,8 @@ FixedwingPositionControl::control_position(const math::Vector2f ¤t_positio // warnx("nav bearing: %8.4f bearing err: %8.4f target bearing: %8.4f", (double)_l1_control.nav_bearing(), // (double)_l1_control.bearing_error(), (double)_l1_control.target_bearing()); - // warnx("prev wp: %8.4f/%8.4f, next wp: %8.4f/%8.4f prev:%s", (double)prev_wp.getX(), (double)prev_wp.getY(), - // (double)next_wp.getX(), (double)next_wp.getY(), (mission_item_triplet.previous_valid) ? "valid" : "invalid"); + // warnx("prev wp: %8.4f/%8.4f, next wp: %8.4f/%8.4f prev:%s", (double)prev_wp(0), (double)prev_wp(1), + // (double)next_wp(0), (double)next_wp(1), (mission_item_triplet.previous_valid) ? "valid" : "invalid"); // XXX at this point we always want no loiter hold if a // mission is active @@ -1209,8 +1209,8 @@ FixedwingPositionControl::task_main() vehicle_airspeed_poll(); // vehicle_baro_poll(); - math::Vector2f ground_speed(_global_pos.vx, _global_pos.vy); - math::Vector2f current_position(_global_pos.lat / 1e7f, _global_pos.lon / 1e7f); + math::Vector<2> ground_speed(_global_pos.vx, _global_pos.vy); + math::Vector<2> current_position(_global_pos.lat / 1e7f, _global_pos.lon / 1e7f); /* * Attempt to control position, on success (= sensors present and not in manual mode), |