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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    Title :

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


    Additional title:

    NASA -- Tech Note


    Contributors:
    White, J.A. (author)


    Publication date :

    1960


    Size :

    65 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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