A technique is described which can be used for design of feedback controllers for high-performance aircraft operating in flight conditions in which nonlinearities significantly affect performance. Designs are performed on a mathematical model of the longitudinal dynamics of a hypothetical aircraft similar to proposed supermaneuverable flight test vehicles. Nonlinear controller designs are performed using truncated solutions of the Hamilton-Jacobi-Bellman equation. Preliminary results show that the method yields promising results.


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    Titel :

    Nonlinear longitudinal control of a supermaneuverable aircraft


    Beteiligte:
    Garrard, William L. (Autor:in) / Snell, Anthony (Autor:in) / Enns, Dale F. (Autor:in)

    Kongress:

    1989 American Control Conference ; 1989 ; Pittsburgh, PA, United States


    Erscheinungsdatum :

    1989-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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