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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
Line 333: 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() ====
 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() ==== +
-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:
  • px4-analyse-position.txt
  • Last modified: 2018/10/27 22:02
  • by natwati