Abstract:IntroductionThe missile guidance is a well-known nonlinear control engineering area of research. Since the basic principles were extensively covered The variable structure control law has been applied to many guidance Recently, Chen et al.[10] derived a new nonlinear fuzzy H ∞ guidance law with a saturation of actuators against maneuvering targets. They first approximated the nonlinear missile target pursuit dynamics with the Takagi -Sugeno linear fuzzy models. Then, based on this, they constructed a H ∞ contr… Show more
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