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Handling Qualities Specifications for U.S. Military HelicoptersInadequacies in the military specification for helicopter handling qualities, MIL-H-8501A, have long been recognized, and the latest procurements by the U.S. Army used special Prime Item Development Specifications (PIDS). This paper assesses the efficacy of these PIDS and suggests that changes should be made. In particular, the structure developed in MIL-F-8785B (ASG) (the specification for flying qualities of piloted airplanes) should be incorporated. Improved requirements must be based on a systematic data base and concentrated on topics most important in preliminary design: static and dynamic stability, control power and sensitivity, and interaction with controllers and displays. Emphasis should be on current military helicopter missions and helicopter idiosyncrasies such as cross-coupling, nonlinearities, and higher-order dynamics.
Document ID
19990028220
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
Key, David L.
(Army Research and Technology Labs. Moffett Field, CA United States)
Date Acquired
August 19, 2013
Publication Date
February 1, 1982
Publication Information
Publication: Journal of Aircraft
Publisher: American Institute of Aeronautics and Astronautics
Volume: 19
Issue: 2
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA Paper 80-1592R
Meeting Information
Meeting: Atmospheric Flight Mechanics Conference
Location: Danvers, MA
Country: United States
Start Date: August 11, 1980
End Date: August 13, 1980
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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