Analysis is made of command errors and performance degradation resulting from tracker errors and angles of attack in two types of systems employing roll autopilot control equation; it is shown that much smaller command errors are expected to occur in system in which roll autopilot keeps time integral of roll rate equal to zero.


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    Title :

    Missile orientation errors in command guidance systems


    Additional title:

    ARS -- J


    Contributors:

    Published in:

    ARS Journal ; 30 , n 1


    Publication date :

    1960


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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