Fuzzy Logic-based Terminal Guidance with Impact Angle Control
نویسندگان
چکیده
This paper presents a new formulation of terminal guidance law which controls the impact attitude angle while minimising the miss distance. The formulation is based on the fuzzy logiccontrol approach. Unlike many prevalent designs, the proposed guidance law does not require linearisation of missile-target engagement model. Numerical simulation results demonstrate that the proposed guidance law offers satisfactory performance, fulfilling its design goals.
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