Various techniques for devising control law to steer rocket vehicle to thrust termination are discussed; consistent with present practice in space vehicle design, rational scheme is sought for relaxing constraints at thrust termination; introducing geometrical interpretation of optimality, "least-Squares" control scheme is obtained; it is shown that control scheme is stable at final time, and relationship to well-known velocity-to-be-gained steering scheme is pointed out; example of ascent guidance into near-earth satellite orbit is presented and simple technique for approximating optimal control law suggested.


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    Titel :

    Technique for optimal final value control of powered flight trajectories


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Pfeiffer, C.G. (Autor:in)

    Erschienen in:

    AIAA Journal ; 4 , n 2


    Erscheinungsdatum :

    1966


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :