The problem of determining the optimal impulsive guidance policy for an interplanetary spacecraft is studied. The problem is treated as a stochastic optimal control problem with control-dependent errors. The performance index gives an upper bound for the probability that the mission fails. The results obtained here are applied to a Jupiter planetary fly-by, and the numerical results indicate that consideration of the control dependent errors is considerably significant.


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    Title :

    Optimum midcourse guidance with control dependent errors


    Additional title:

    Optimale Mittenkurs-Lenkung mit einer Steuerung, die abhaengig von Fehlern ist
    Titel japanisch


    Contributors:
    Inaba, H. (author)


    Publication date :

    1975


    Size :

    , 8 Quellen


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Japanese




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