In a previous paper, the author obtained conditions for the acceleration of a missile pursuing a maneuvering target according to proportional navigation, to be bounded. This correspondence extends previous work, and new boundaries are obtained for the missile acceleration.


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    Title :

    Missile Acceleration in Proportional Navigation


    Contributors:
    Guelman, M. (author)


    Publication date :

    1973-05-01


    Size :

    297365 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English