The present disclosure provides various embodiments of a rotocraft-assisted launch and retrieval system, and a method for controlling an airborne rotorcraft which includes controlling by a controller a first feedback loop about a longitudinal roll axis of the airborne rotocraft and controlling by the controller a second feedback loop about a horizontal pitch axis of the airborne rotocraft, without controlling a vertical yaw axis of the airborne rotocraft.
ROTORCRAFT-ASSISTED SYSTEM AND METHOD FOR LAUNCHING AND RETRIEVING A FIXED-WING AIRCRAFT
2019-01-31
Patent
Elektronische Ressource
Englisch
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