Li-ying Yuan

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This paper is concerned with the design of missile guidance law based on robust output regulation theory and Takagi-Sugeno fuzzy model. In this design, the guidance problem is converted to the nonlinear regulator problem. The three-dimensional (3-D) command to line-of-sight (CLOS) guidance problem is formulated as a tracking problem of a time-varying(More)
A fuzzy logic controllers based on Proportional Navigation Guidance law with minimal rule base was proposed in this study. The fuzzy logic controller is a knowledge based controller, which alters the value of the equivalent navigational constant to reap the maximum benefits in terms of the missile performance. Genetic algorithm was employed to optimize the(More)
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