In this paper we develop an optimal mid-course strategy for guiding an interceptor. We assume that the target is outside of the sensible atmosphere and is not maneuvering throughout the engagement, and the thrust vector controlled interceptor has a fixed maneuvering time which ends well before the actual intercept. We will later extend the optimal solution to a family of guidance laws that guarantee perfect intercept for the fixed-interval maneuvering problems.


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    Title :

    An Optimal Mid-Course Guidance Law For Fixed-Interval Propulsive Maneuvers


    Contributors:


    Publication date :

    1993-06-01


    Size :

    293991 byte



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English