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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    Title :

    Inertial guidance for rocket-propelled missiles


    Additional title:

    Jet Propulsion


    Contributors:

    Published in:

    Jet Propulsion ; 28 , n 1


    Publication date :

    1958


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Inertial Guidance of Ballistic Missiles

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    Optimal Mid-Course Guidance of Variable Flow Ducted Rocket Missiles

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