A methodology is described for the development of flight test trajectory control laws based on singular perturbation methodology and nonlinear dynamic modeling. The control design methodology is applied to a detailed nonlinear six degree-of-freedom simulation of the F-15 and results for a level accelerations, pushover/pullup maneuver, zoom and pushover maneuver, excess thrust windup turn, constant thrust windup turn, and a constant dynamic pressure/constant load factor trajectory are presented.


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    Titel :

    Nonlinear Maneuver Autopilot for the F-15 Aircraft


    Beteiligte:
    P. K. A. Menon (Autor:in) / M. E. Badgett (Autor:in) / R. A. Walker (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    90 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Nonlinear Maneuver Autopilot

    Menon, P. K. A. / Badgett, M. E. / Walker, R. A. | NTRS | 1992


    Nonlinear maneuver autopilot for the F-15 aircraft

    Menon, P. K. A. / Badgett, M. E. / Walker, R. A. | NTRS | 1989