Paper shows that it appears possible to realize real-time optimal control by in-flight guidance computers; proposed method is discussed and illustrated by two examples; in case of arbitrary inclined flight, control variable can be expressed as function of state variables; in case of zero-lift flight control variable can be expressed as function of state variables and two unknown constants; constants can be determined by steep descent search in parameter space; modified method of steepest descent appears suitable for use by simple guidance computer. (In English with French and German abstracts)


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    Titel :

    Synthesis of real-time optimal controllers for rockets


    Weitere Titelangaben:

    Astronautica Acta


    Beteiligte:
    Bohn, E.V. (Autor:in) / Chan, W.C. (Autor:in) / Sutherland, J.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Optimal Guidance of Rockets

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    ROCKETS

    Durant, F. C., III | NTRS | 1959


    Rockets

    Szebehely, Victor G. / Mark, Hans | Wiley | 1998


    Discrete-Time Optimal Pulsed Guidance and its Application to Artillery Rockets

    Gendler, B. / Yaesh, I. / Ben-Asher, J. et al. | British Library Conference Proceedings | 2007


    Rockets

    Goddard, Robert Hutchings | SLUB | 2002