Fundamentals of inertia navigation and measurement of acceleration required by means of force feed-back accelerometer; in place of separate accelerometer and integrator, many systems use integrating gyro accelerometer which measures speed directly; types of gyroscopes; detailed design of inertia navigation system will depend on operational requirements of missile; example of Thor navigation system.


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    Title :

    Inertial navigation


    Additional title:

    Aeroplane Astronautics


    Contributors:

    Published in:

    Publication date :

    1960


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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