Differences
This shows you the differences between two versions of the page.
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px4-analyse-position [2018/10/27 22:02] natwati [handle_command()] |
px4-analyse-position [2018/10/27 22:02] (current) natwati |
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| 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() ==== | ||
| This funcion solely handles the VEHICLE_CMD_DO_GO_AROUND. | This funcion solely handles the VEHICLE_CMD_DO_GO_AROUND. | ||
| It abort landing before point of no return (horizontal and vertical) by setting _fw_pos_ctrl_status.abort_landing to true. | It abort landing before point of no return (horizontal and vertical) by setting _fw_pos_ctrl_status.abort_landing to true. | ||
| - | ==== tecs_update_pitch_throttle() ====Â | + | |
| - | Not examined yet | + | |
| ==== airspeed_poll() ==== | ==== airspeed_poll() ==== | ||
| Line 351: | 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: | ||