Paper derives and analyzes method of steering rocket vehicle so as to achieve ballistic trajectory that arrives at specific position at specific time; result contained is substantial refinement of fly-by-wire method for exoatmospheric steering; simulation results show that since steering equation is sufficiently accurate, no trajectory-dependent preflight calculations need be done when simple in-flight choice of certain constants is made.


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    Titel :

    Steering law satisfying constant total time of flight constraint


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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