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    IJIT
    2004
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    Fuzzy Guidance In The Aerodynamic Homing Missiles
    14 years 26 days ago
    Fuzzy Guidance In The Aerodynamic Homing Missiles
    Download  metalab.uniten.edu.my
    A fuzzy tail pursuit guidance algorithm is proposed as an alternative to the conventional guidance methods. The purpose of this scheme is to obtain an control agains to the changin...
    Mustafa Resa Becan
    claim paper
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