The transfer function of an air-launched missile is obtained for a wide range of operating conditions. A linear control system is designed. The use of the missile against both airborne and surface targets is shown to be feasible from the standpoint of control-system requirements. Launch envelopes for the missile with a proportional navigation guidance system are obtained in the horizontal and vertical planes. The effects of various constraints on the missile are determined. Analysis of representative missile-target characteristics at different altitudes demonstrates that the missile can be effective against both airborne and surface targets. (Author)


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    Titel :

    Analysis of an Air-TO-Air, Air-TO-Surface Missile


    Beteiligte:
    E. Hymas (Autor:in)

    Erscheinungsdatum :

    1964


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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