Precision gyroscopes, accelerometers and stabilized platforms described; guidance schemes appropriate to ballistic missiles; problem of gravity computation and effect of instrument errors; missile steering computer and rocket motor shutoff computer given for German V-2 rocket used as example; numerical values of coefficients calculated for sample trajectory.


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    Titel :

    Inertial guidance for rocket-propelled missiles


    Weitere Titelangaben:

    Jet Propulsion


    Beteiligte:
    Russell, W.T. (Autor:in)

    Erschienen in:

    Jet Propulsion ; 28 , n 1


    Erscheinungsdatum :

    1958


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Inertial Guidance of Ballistic Missiles

    A. Y. Ishlinskii | NTIS | 1971


    Inertial guidance for air force high-punch missiles

    Slater, J.M. | Engineering Index Backfile | 1957


    Optimal Mid-Course Guidance of Variable Flow Ducted Rocket Missiles

    Kuroda, T. / Mihara, S. / Matsuda, H. et al. | British Library Conference Proceedings | 1998


    Antitank Rocket Missiles

    B. I. Evdokimov | NTIS | 1967


    Optimal Mid-Course Guidance of Variable Flow Ducted Rocket Missiles

    Kuroda, T. / Mihara, S. / Matsuda, H. et al. | British Library Conference Proceedings | 1998