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authortumbili <bapstr@ethz.ch>2015-01-18 17:46:01 +0100
committertumbili <bapstr@ethz.ch>2015-01-18 18:00:14 +0100
commitbeab89367f5cc2765c747fb463a27ce001206dd9 (patch)
treecc0e224ebd3a9a00c45bd9a7165531afe5749db8 /src/modules/uORB
parentfd1f36c3a18355c94df0795156a0fe4341513e86 (diff)
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calculate total airflow over elevons using physical of flow behind propeller. read local position topic for future use.
Diffstat (limited to 'src/modules/uORB')
-rw-r--r--src/modules/uORB/topics/vtol_vehicle_status.h1
1 files changed, 1 insertions, 0 deletions
diff --git a/src/modules/uORB/topics/vtol_vehicle_status.h b/src/modules/uORB/topics/vtol_vehicle_status.h
index 7b4e22bc8..968c2b6bd 100644
--- a/src/modules/uORB/topics/vtol_vehicle_status.h
+++ b/src/modules/uORB/topics/vtol_vehicle_status.h
@@ -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 */
};
/**