Three translational and 3 rotational equilibrium equations for orbital vehicle subject to aerodynamic and jet reaction forces are derived using modified flight-path axis system for translational equations; analog computer mechanization of these equations in both real and fast time; novel technique for division which preserves favorable multiplier scaling; specific machine results demonstrate accurate solution of close-satellite trajectories, including re-entry from satellite altitudes to sea level.


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    Titel :

    Flight simulation of orbital and re-entry vehicles


    Weitere Titelangaben:

    IRE -- Trans Electronic Computers


    Beteiligte:
    Fogarty, L.E. (Autor:in) / Howe, R.M. (Autor:in)


    Erscheinungsdatum :

    1962


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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