Analyses of design variations on a pitch axis stabilization and command augmentation system (SCAS) for a STOVL fighter aircraft are performed in a moving base simulation experiment. The primary goal of this study is to determine if turbulence-induced control activity could be reduced by modifying SCAS parameters while keeping the response-to-command characteristics of the baseline system that provide Level 1 flying qualities. Pilot ratings and control utilization statistics for the baseline system are in agreement with similar data gathered in a prior simulation test involving the same aircraft and control system.


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    Titel :

    Piloted simulation evaluation of pitch control designs for highly augmented STOVL aircraft


    Beteiligte:
    Engelland, S. A. (Autor:in) / Franklin, J. A. (Autor:in) / Stortz, M. W. (Autor:in) / Hardy, G. H. (Autor:in)

    Kongress:

    AIAA, Aircraft Design Systems Meeting ; 1992 ; Hilton Head Island, SC, United States


    Erscheinungsdatum :

    01.08.1992


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Piloted simulation evaluation of pitch control designs for highly augmented STOVL aircraft

    ENGELLAND, S. / FRANKLIN, J. / STORTZ, M. et al. | AIAA | 1992


    Piloted simulation developments of STOVL aircraft handling qualities

    Fielding, Chris / Southworth, Mike | AIAA | 2001


    Highly Augmented Control Mode Concepts and Simulation Evaluation for STOVL Aircraft

    Bodden, D. / Virnig, J. / AIAA | British Library Conference Proceedings | 1994