Simplified version of midcourse guidance problem for space vehicle with low-thrust control rocket is posed as stochastic optimal control problem; control decision process is continuous in time; control magnitude is bounded in instantaneous value and in integrated value; state of system is observed in noisy measurements and governed by linear dynamics; numerical solutions are generated by procedure based on dynamic programming and checked by Monte Carlo simulation; numerical solutions of related problem, analyzed by C.T. Striebel and J.V.Breakwell, are also generated and compared. (03723)


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    Titel :

    Final value optimization of systems with bounded controller and noisy measurements


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Van Gelder, A. (Autor:in)

    Erschienen in:

    AIAA Journal ; 6 , n 10


    Erscheinungsdatum :

    1968


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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