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Velocity Command/Position Hold: A New Flight Control Concept for Hovering VTOL Aircraft

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Stapleford, Robert L., author.
Conference Name:
Aerospace Congress & Exposition (1980-10-13 : Los Angeles, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1980
Summary:
A new flight control concept for a hovering VTOL aircraft has been developed. The main feature of this system is that deflection of a pilot's controller produces a linear velocity command with position hold when the controller is centered. Another novel feature is that horizontal commands both tilt the aircraft and deflect the thrust vector, while the position feedbacks only deflect the thrust vector. This system has been evaluated in two piloted simulations of landing a VTOL aircraft on a small ship. The pilots consistently rated this system better than three other, more conventional, control systems
Notes:
Vendor supplied data
Publisher Number:
801206
Access Restriction:
Restricted for use by site license

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