Optimal stabilization of Takagi-Sugeno fuzzy systems with application to spacecraft control

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A new design methodology is proposed for the optimal control of nonlinear systems described by the Takagi-Sugeno (TS) fuzzy model. The TS fuzzy systems are first classified into two families based on how diverse their input matrices are and then a controller synthesis procedure based on the inverse optimal approach is given for each family, We also show that the optimal controller can he found by solving a linear matrix inequality problem, The optimal controllers have robustness with respect to a class of input uncertainties. The proposed method is applied to the attitude control of a rigid spacecraft to demonstrate its validity.
Publisher
AMER INST AERONAUT ASTRONAUT
Issue Date
2001-07
Language
English
Article Type
Article
Keywords

ATTITUDE MANEUVERS; ROBUST STABILIZATION; INVERSE OPTIMALITY; NONLINEAR-SYSTEMS; ANGULAR VELOCITY; STABILITY; STABILIZABILITY; SATELLITE; VEHICLES; DESIGN

Citation

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.24, no.4, pp.767 - 777

ISSN
0731-5090
URI
http://hdl.handle.net/10203/78989
Appears in Collection
AE-Journal Papers(저널논문)
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