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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    Titel :

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


    Beteiligte:
    D. L. Fogler (Autor:in) / J. F. Keller (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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