ROTORCRAFT-ASSISTED SYSTEM AND METHOD FOR LAUNCHING AND RETRIEVING A FIXED-WING AIRCRAFT

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 th...

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Bibliographische Detailangaben
Hauptverfasser: Reiss, Daniel Pepin, Woodruff, Caleb Andrew, von Flotow, Andreas H, Roeseler, Corydon C
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung: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.