作者: P.P. Mohanlal , M.R. Kaimal , S. Dasgupta
DOI: 10.1109/ICARCV.2002.1234956
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摘要: This paper presents a novel method of Exact Fuzzy Modeling and Optimal control Launch Vehicle in the atmospheric phase. Time varying plant is considered with power nonlinearity. Plant modeling, controller design analysis are carried out for Rigid Body Actuator dynamics. The results compared classical design. Conventionally, TSK fuzzy modeling blends local linear models to represent nonlinear system, which general does not exactly system under consideration. Here, instead models, set 'boundary models' associated membership-functions so chosen that blending these result an exact representation overall time system. laws designed each subsystems, again individual laws. procedure optimal solution