The existing body of research to investigate airworthiness, performance, handling, and operational requirements for STOL and V/STOL aircraft was reviewed for its applicability to the tiltrotor and tiltwing design concepts. The objective of this study was to help determine the needs for developing civil certification criteria for these aircraft concepts. Piloting tasks that were considered included configuration and thrust vector management, glidepath control, deceleration to hover, and engine failure procedures. Flight control and cockpit display systems that have been found necessary to exploit the low-speed operating characteristics of these aircraft are described, and beneficial future developments are proposed.
Piloting Considerations for Terminal Area Operations of Civil Tiltwing and Tiltrotor Aircraft
1993
18 pages
Report
Keine Angabe
Englisch
Aircraft , Aeronautics , Aircraft control , Aircraft performance , Flight characteristics , Flight control , Pilot performance , Tilt rotor aircraft , Tilt wing aircraft , Civil aviation , Certification , Cockpits , Configuration management , Deceleration , Display devices , Engine failure , Hovering , Tasks , Thrust vector control , V/stol aircraft
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