A qualitative analysis of the trajectories of a missile pursuing a maneuvering target according to the proportional navigation law is presented. Conditions for a missile to reach the target from any initial state are determined. The existence of a boundary for the required missile acceleration is demonstrated.


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    Title :

    Proportional Navigation with a Maneuvering Target


    Contributors:
    Guelman, M. (author)


    Publication date :

    1972-05-01


    Size :

    2176499 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English