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| Both sides previous revision Previous revision Next revision | Previous revision | ||
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px4-analyse-position [2018/10/27 21:57] natwati [calculate_target_airspeed()] |
px4-analyse-position [2018/10/27 22:02] (current) natwati |
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| Line 326: | Line 326: | ||
| If flag_init is false the passed waypoint_next and waypoint_prev are used to generate a line. The waypoint_prev is generated on the line 1100 meters behind waypoint_next and the new waypoint_next is generated on the line 4000 meters ahead of the old waypoint_next.\\ | If flag_init is false the passed waypoint_next and waypoint_prev are used to generate a line. The waypoint_prev is generated on the line 1100 meters behind waypoint_next and the new waypoint_next is generated on the line 4000 meters ahead of the old waypoint_next.\\ | ||
| _hold_alt is used for all waypoints. | _hold_alt is used for all waypoints. | ||
| + | |||
| + | ==== update_desired_altitude() ==== | ||
| <code c++ FixedwingPositionControl.hpp> | <code c++ FixedwingPositionControl.hpp> | ||
| bool update_desired_altitude(float dt); | bool update_desired_altitude(float dt); | ||
| Line 331: | Line 333: | ||
| Update desired altitude base on user pitch stick input based on _manual.x (from manual_control_setpoint) and a dt (delta time) argument. | Update desired altitude base on user pitch stick input based on _manual.x (from manual_control_setpoint) and a dt (delta time) argument. | ||
| - | ==== control_takeoff() ==== | ||
| - | Not examined yet | ||
| - | ==== control_landing() ==== | ||
| - | Not examined yet | ||
| ==== handle_command() ==== | ==== handle_command() ==== | ||
| - | Not examined yetÌý | + | This funcion solely handles the VEHICLE_CMD_DO_GO_AROUND.Ìý |
| - | ==== tecs_update_pitch_throttle() ====Ìý | + | It abort landing before point of no return (horizontal and vertical) by setting _fw_pos_ctrl_status.abort_landing to true.Ìý |
| - | Not examined yet | + | |
| ==== airspeed_poll() ==== | ==== airspeed_poll() ==== | ||
| Line 348: | Line 346: | ||
| TECS is notified if airspeed is still valid by calling _tecs.enable_airspeed(_airspeed_valid). | TECS is notified if airspeed is still valid by calling _tecs.enable_airspeed(_airspeed_valid). | ||
| - | ===== Copyright ===== | ||
| + | ==== control_takeoff() ==== | ||
| + | Not examined yet | ||
| + | ==== control_landing() ==== | ||
| + | Not examined yet | ||
| + | ==== tecs_update_pitch_throttle() ==== | ||
| + | Not examined yet | ||
| + | |||
| + | ===== Copyright ===== | ||
| The following copyright applies to all sourcecode shown on this page: | The following copyright applies to all sourcecode shown on this page: | ||