Two control law design techniques are compared and the performance of the resulting controllers evaluated. The design requirement is for a flight test trajectory controller (FTTC) capable of closed-loop, outer-loop control of an F-15 aircraft performing high-quality research flight test maneuvers. The maneuver modeling, linearization, and design methodologies utilized in this research, are detailed. The results of applying these FTTCs to a nonlinear F-15 simulation are presented.


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    Title :

    Aircraft flight test trajectory control


    Contributors:

    Publication date :

    1988-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Aircraft flight test trajectory control

    Menon, P. K. A. / Walker, R. A. | NTRS | 1988


    Aircraft Flight Test Trajectory Control

    P. K. A. Menon / R. A. Walker | NTIS | 1988


    Aircraft Flight Test Trajectory Control

    P. K. A. Menon / R. A. Walker | NTIS | 1988


    Nonlinear flight test trajectory controllers for aircraft

    Menon, P. K. A. / Badgett, M. E. / Walker, R. A. et al. | NTRS | 1987


    Nonlinear flight test trajectory controllers for aircraft

    MENON, P. K. A. / BADGETT, M. E. / WALKER, R. A. et al. | AIAA | 1987