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Position control needs to be deactivated during the transition otherwise it will fight itself.
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@@ -1,4 +1,5 @@
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uint64 timestamp # Microseconds since system boot
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bool vtol_in_rw_mode # true: vtol vehicle is in rotating wing mode
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bool vtol_in_trans_mode
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bool fw_permanent_stab # In fw mode stabilize attitude even if in manual mode
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float32 airspeed_tot # Estimated airspeed over control surfaces
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