This article develops a missile guidance technique for a ‘defense missile’ trying to protect a cooperative aircraft from guided munitions which have the same thrust and maneuvering capabilities as that of the defense missile. A novel guidance law for the missile-to-missile intercept is developed via a geometrical approach. Performance of the guidance law is analysed in detail and its potential is demonstrated with results from a six degrees-of-freedom simulation and comparison with a conventional guidance law.


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    Titel :

    Geometrical approach-based defense-missile intercept guidance for aircraft protection against missile attack


    Beteiligte:
    Yamasaki, T (Autor:in) / Balakrishnan, S N (Autor:in) / Takano, H (Autor:in)


    Erscheinungsdatum :

    2012-08-01


    Format / Umfang :

    15 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt





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