This work describes a new guidance algorithm against maneuvering decelerating target based on the concept of information sets (IS). As an example of guidance problem, a model of defense scenario against reentering ballistic missile is considered. In this scenario, a maneuverable decelerating target is to be destroyed by a hit-to-kill interceptor outfitted with an infrared (IR) array seeker and lateral impulse thrusters. The key element of the proposed approach is a description of the "interceptor-target" system state by means of IS. The results of Monte Carlo (MC) tests of the developed algorithm are presented.


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    Titel :

    Information set-based guidance algorithm against a decelerating maneuvering target


    Beteiligte:
    Emeliyanov, D. (Autor:in) / Rubinovich, E. (Autor:in) / Miller, B. (Autor:in)


    Erscheinungsdatum :

    01.01.2005


    Format / Umfang :

    2574224 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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