Guidance consists of directing missile to predetermined point in space and is subdivided into navigation, computation, and control; inertially guided missile systems can be divided into 2 classes, depending upon type of guidance equations used to define error signals to drive control systems, explicit and delta guidance equations; one method of simplifying mechanization is to decrease rigor of solution of navigation and guidance problems; major sources of error are inertial measurement errors, equation and computation errors, control system errors, gravitational anomalies, and free-flight dispersion errors; guidance and system accuracy.


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    Title :

    Guidance concepts for tactical missiles


    Additional title:

    Sperry Eng Rev


    Contributors:

    Published in:

    Publication date :

    1964


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English






    Guidance and control of tactical missiles

    NATO, Advisory Group for Aerospace Research and Development | TIBKAT | 1972