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Design and Pilot Evaluation of the RAH-66 Comanche Core AFCSThis paper addresses the design and pilot evaluation of the Core Automatic Flight Control System (AFCS) for the Reconnaissance/Attack Helicopter (RAH-66) Comanche. During the period from November 1991 through February 1992, the RAH-66 Comanche control laws were evaluated through a structured pilot acceptance test using a motion base simulator. Design requirements, descriptions of the control law design, and handling qualities data collected from ADS-33 maneuvers are presented.
Document ID
19940008848
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Donald L Fogler, Jr. (United Technologies Corporation (United States) Windsor Locks, Connecticut, United States)
James F Keller (Boeing Defense and Space Group Philadelphia, PA., United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1993
Publication Information
Publication: Piloting Vertical Flight Aircraft: A Conference on Flying Qualities and Human Factors
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Stability and Control
Report/Patent Number
NASA/CP-3220
Meeting Information
Meeting: Piloting Vertical Flight Aircraft: A Conference on Flying Qualities and Human Factors
Location: San Francisco, CA
Country: US
Start Date: January 20, 1993
End Date: January 22, 1993
Sponsors: American Helicopter Society, National Aeronautics and Space Administration
Accession Number
94N13321
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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