This 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.


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    Title :

    Design and Pilot Evaluation of the RAH-66 Comanche Core AFCS


    Contributors:
    D. L. Fogler (author) / J. F. Keller (author)

    Publication date :

    1993


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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