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Fuzzy model reference learning control for aircraft pitch autopilot design

In this paper, the idea of fuzzy model reference learning control(FMRLC) technique for missile autopilot design is introduced. This controller utilizes a learning mechanism, which observes the plant outputs and adjusts the rules in a direct fuzzy controller, so that the overall system behaves like a "reference model" which characterizes the desired behaviour. The performance of the FMRLC based missile autopilot is demonstrated by simulation for various conditions with structure uncertainties.