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• W1869792111 startingPage "118" @default.
• W1869792111 abstract "Aircraft dynamics are in general nonlinear, time varying, and uncertain. A control system (classical control systems) designed for a flight condition, may not provide the desired stability and performance characteristics in case of deviation from the equilibrium point. There are numerous studies regarding flight control in the literature. One of them is fuzzy flight control system. In this study an aircraft pitch rate damping is evaluated by using a fuzzy PD controller." @default.
• W1869792111 created "2016-06-24" @default.
• W1869792111 creator A5054431257 @default.
• W1869792111 date "2010-05-03" @default.
• W1869792111 modified "2023-09-27" @default.
• W1869792111 title "Pitch rate damping of an aircraft by a fuzzy PD controller" @default.
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