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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1998, Vol. 19 ›› Issue (1): 58-61.
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Gong Cheng1, Lu Guangshan2, Wang Yongnian2
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Abstract:
An approach to stabilize a family of nonlinear systems via feedback nonlinearization is presented. A dummy output mapping is constructed so that the zero dynamics are made asymptotically stable and the system is of relative degree{1,…,1};then a group of controllers are designed that guarantee the exponential attractivity of the zeroing output manifold. Using tools in nonlinear H ∞ control theory, it is shown that under mild conditions, the resulting closed loop system is locally asymptotically stable. Finally, these results are used to the attitude control problem for a rigid body to design detumbling controllers that only require knowledge of relative value of the system inertial parameters. This technique seems attractive in that, to a certain extent, it may lessen the need of precise system knowledge required by the feedback linearization technique.
Key words: nonlinear systems, geometr ic approach, attitude contr ol
CLC Number:
TP271.62
V249.1
Gong Cheng;Lu Guangshan;Wang Yongnian. STABILIZATION OF A FAMILY OF NONLINEAR SYSTEMS VIA FEEDBACK NONLINEARIZATION[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1998, 19(1): 58-61.
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