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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    Title :

    Nonlinear maneuver autopilot for the F-15 aircraft


    Contributors:

    Publication date :

    1989-06-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


    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