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Filtering by: Alternative title ssim Circular of information no. 77 Remove constraint Alternative title ssim: Circular of information no. 77 Committee Member Tadepalli, Prasad Remove constraint Committee Member: Tadepalli, Prasad Degree Field Electrical and Computer Engineering Remove constraint Degree Field: Electrical and Computer Engineering Rights Statement Copyright Not Evaluated Remove constraint Rights Statement: Copyright Not Evaluated

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  • Sliding-mode control of the super maneuverable aircraft

    Creator:
    Koo, Chang Sul
    Abstract:
    In this thesis, A nonlinear methodology for the control of the highly maneuverable, high performance aircraft HARV (F-18) is studied by using sliding-mode control (SMC). This control law, which takes a continuous function when the input constraints are not considered, satisfies the reachability condition by which concerned states are driven...
    Resource Type:
    Dissertation
    Full Text:
    ) rersponse for maneuver from a0=4.3° to a=80° through a=25° 77 52 Angle of attack (deg) response for