Piloted simulations were conducted to investigate flying qualities requirements for longitudinal maneuvering at 30° angle of attack. Pilot evaluations of various longitudinal dynamics were gathered using acquisition and tracking tasks representative of future fighter air combat maneuvering. Pilot comments and Cooper-Harper Ratings were used to define desired regions of aircraft dynamics. These criteria were then compared to previously developed 30° angle of attack criteria for a lower speed flight condition to determine airspeed effects. The desired region of dynamics was found to depend on equivalent airspeed. This dependency can be used to help design control law gain schedules which provide good high angle of attack flying qualities over a wide speed range.


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    Titel :

    Velocity Dependence of High Angle of Attack Longitudinal Flying Qualities Criteria


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Wilson, David J. (Autor:in) / Riley, David R. (Autor:in) / Hall, Neil S. (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 1991



    Erscheinungsdatum :

    1991-09-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    Wilson, D.J. / Hall, N.S. / Riley, D.R. | Tema Archiv | 1991


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    KREKELER, JR., GREGORY / WILSON, DAVID / RILEY, DAVID | AIAA | 1990


    High Angle of Attack Flying Qualities Criteria for Longitudinal Rate Command Systems

    D. J. Wilson / K. D. Citurs / J. B. Davidson | NTIS | 1994


    High angle of attack flying qualities criteria for longitudinal rate command systems

    Wilson, David J. / Citurs, Kevin D. / Davidson, John B. | NTRS | 1994


    Development of Flying Qualities Criteria for 60 Degree Angle of Attack

    Wilson, D. / Citurs, K. / Davidson, J. et al. | British Library Conference Proceedings | 1994