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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Nonlinear maneuver autopilot for the F-15 aircraft


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

    Erscheinungsdatum :

    1989-06-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Nonlinear Maneuver Autopilot

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


    Nonlinear Maneuver Autopilot for the F-15 Aircraft

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