Problem of rendezvous is studied from point of view of injection into sufficiently precise trajectory; in event of primary guidance mode failure, simple secondary guidance technique is needed to satisfy rendezvous objective; guidance law is developed which uses predetermined compensation; 4 measurements are made during powered flight of vehicle, and simple calculations and corrective actions are used to adjust vehicle motion.


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    Title :

    "t1 compensation" guidance law for launch of space vehicles


    Additional title:

    Am Astronautical Soc -- Advances Astronautical Sciences


    Contributors:
    Chomak, S. (author) / Haggerty, T. (author) / Rothstein, H. (author)


    Publication date :

    1963


    Size :

    28 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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