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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
Legacy CDMS
Document Type
Conference Paper
Authors
Fogler, Donald L., Jr. (Sikorsky Aircraft Stratford, CT, United States)
Keller, James F. (Boeing Defense and Space Group Philadelphia, PA., United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1993
Publication Information
Publication: NASA. Ames Research Center, Piloting Vertical Flight Aircraft: A Conference on Flying Qualities and Human Factors
Subject Category
Aircraft Stability And Control
Accession Number
94N13321
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19940007812Collected WorksAnnual Research Briefs, 1992
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