calculate total airflow over elevons using physical of flow behind propeller. read local position topic for future use.

2026-10-16 11:03:34 +08:00 · 2015-01-18 18:00:14 +01:00
parent fd1f36c3a1
commit beab89367f
3 changed files with 129 additions and 11 deletions
@@ -55,6 +55,7 @@ struct vtol_vehicle_status_s {
 	uint64_t	timestamp;	/**< Microseconds since system boot */
 	bool vtol_in_rw_mode;	/*true: vtol vehicle is in rotating wing mode */
 	bool fw_permanent_stab;	/**< In fw mode stabilize attitude even if in manual mode*/
+	float airspeed_tot;		/*< Estimated airspeed over control surfaces */
 };

 /**