Monte Carlo technique was used to study relative performance of three methods of scheduling corrective thrust impulses in presence of various assumed inaccuracies in measuring velocity and flight-path angle and in obtaining desired thrust impulse; comparison of methods and results.


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    Titel :

    Study of guidance of space vehicle returning to braking ellipse about earth


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    White, J.A. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    65 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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