The paper presents a physical and mathematical model of a short range missile launcher based onboard a warship. The conducted numerical simulation allowed for developing an analysis of the anti-aircraft assembly dynamics. The selected responses of the system are demonstrated in the form of physical values characterizing the launcher motion.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Elements of Dynamics Analysis of the Warship Launcher of Anti-Aircraft Short Range Homing Missiles


    Contributors:


    Publication date :

    2013


    Size :

    15 Seiten




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English






    Hyperstable range in homing missiles

    TANAKA, TOSHIYUKI / EGUCHI, HIROFUMI | AIAA | 1990



    Miss distance dynamics in homing missiles

    NESLINE, F. / ZARCHAN, P. | AIAA | 1984