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

801206

09/01/1980

Authors
Abstract
Content
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.
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DOI
https://doi.org/10.4271/801206
Pages
12
Citation
Stapleford, R., "Velocity Command/Position Hold: A New Flight Control Concept for Hovering VTOL Aircraft," SAE Technical Paper 801206, 1980, https://doi.org/10.4271/801206.
Additional Details
Publisher
Published
Sep 1, 1980
Product Code
801206
Content Type
Technical Paper
Language
English