In a missile system, a simple way to guide a missile in a predetermined trajectory from launch to the impacting with a target for optimum warhead penetration of armor by a guided missile. Initially, the missile is guided in yaw by proportional navigation. Subsequently it is guided in pitch first by a pitch programmer until the missile reaches a predetermined gimbal angle between a line of sight of a seeker of the missile and a centerline of the missile, then in pitch by a pseudo-time-optimal closed loop controller to direct the missile pitch attitude at a predetermined rate toward a target until said missile reaches another predetermined gimbal angle, and finally by proportional navigation in pitch of the missile to the target. (Author)


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    Titel :

    Trajectory Shaping of Anti-Armor Missiles via Tri-Mode Guidance


    Beteiligte:
    R. E. Yates (Autor:in) / J. P. Leonard (Autor:in) / R. E. Alongi (Autor:in) / W. V. Albanes (Autor:in) / C. M. Bishop (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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