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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design and pilot evaluation of the RAH-66 Comanche Core AFCS


    Beteiligte:


    Erscheinungsdatum :

    01.07.1993


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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

    D. L. Fogler / J. F. Keller | NTIS | 1993


    RAH-66 COMANCHE CORE AFCS CONTROL LAW DEVELOPMENT: DEMVAL TO EMD

    Kothmann, B. D. / Armbrust, J. / American Helicopter Society | British Library Conference Proceedings | 2002


    AFCS Integration Requirements

    Chmaruk, B. H. / Lamb, T. R. | SAE Technical Papers | 1981


    Pilot Workload Assessment for NO AFCS Mission Helicopter Dispatch

    Afruni, G. / Castelli, A. / Cattaneo, D. et al. | British Library Conference Proceedings | 2011