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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    Titel :

    "t1 compensation" guidance law for launch of space vehicles


    Weitere Titelangaben:

    Am Astronautical Soc -- Advances Astronautical Sciences


    Beteiligte:
    Chomak, S. (Autor:in) / Haggerty, T. (Autor:in) / Rothstein, H. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    28 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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