A complete nonlinear control law is derived for guiding an aircraft in minimum time from an arbitrary initial position and heading to a prescribed terminal position and heading in the horizontal plane. The solution is obtained with the aid of the maximum principle, and is implemented by constructing a digital-computer program for the resulting switching logic.


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    Titel :

    Optimal horizontal guidance law for aircraft in the terminal area.


    Beteiligte:
    Pecsvaradi, T. (Autor:in)

    Kongress:

    Hawaii International Conference on System Sciences, 5th, University of Hawaii ; 1972 ; Honolulu, HI


    Erscheinungsdatum :

    01.01.1972


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Optimal horizontal guidance for aircraft in bounded state-space

    Arimoto, S. / Gaafar, M.Y. / Nakai, T. et al. | Tema Archiv | 1976


    Optimum horizontal guidance techniques for aircraft

    Erzberger, H. / Lee, H. Q. | NTRS | 1978


    Optimum horizontal guidance techniques for aircraft

    Erzberger, H. / Lee, H. Q. | NTRS | 1971