Description and numerical results of Monte Carlo simulation to determine fuel requirements and final accuracy of midcourse phase is presented; example applies two midcourse corrections to null errors in 3 terminal variables; proposed simulation for missions in which burnout errors are so large that nonlinear effects are important also is described; aspects presented are basic system for fuel and accuracy analysis, technique used for trajectory computations, determination of minimum velocity increment computation of midcourse correction errors, and estimated machine time/run.


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    Titel :

    Monte Carlo simulation of midcourse guidance for lunar flights


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Skidmore, L.J. (Autor:in) / Penzo, P.A. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 4


    Erscheinungsdatum :

    1963


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :