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dc.contributor.authorChiou, JCen_US
dc.contributor.authorHwang, MCen_US
dc.contributor.authorWu, SDen_US
dc.contributor.authorYang, JYen_US
dc.date.accessioned2014-12-08T15:01:48Z-
dc.date.available2014-12-08T15:01:48Z-
dc.date.issued1997-05-01en_US
dc.identifier.issn0020-7721en_US
dc.identifier.urihttp://hdl.handle.net/11536/566-
dc.description.abstractA new robust attitude control design of spacecraft is proposed by combining sliding mode control (SMC) and productive networks (PN). Essentially, the sliding mode control uses discontinuous control action to drive state trajectories toward a specific hyperplane in the state space, and to maintain the state trajectories sliding on the specific hyperplane. This principle provides a guideline to design a robust controller. Productive networks, which are a special type of artificial neural network, are then used to implement reaching and sliding conditions, and tackle the drawbacks of SMC such as chattering and high control gains. Attractive features of the proposed method include a systematic procedure of controller design, a reduction in chattering, robustness against model uncertainties and external disturbances. An inverted pendulum and a spacecraft attitude control problem are given to deomonstrate the effectiveness of the proposed method.en_US
dc.language.isoen_USen_US
dc.titleRobust attitude control of spacecraft using sliding mode control and productive networksen_US
dc.typeArticleen_US
dc.identifier.journalINTERNATIONAL JOURNAL OF SYSTEMS SCIENCEen_US
dc.citation.volume28en_US
dc.citation.issue5en_US
dc.citation.spage435en_US
dc.citation.epage446en_US
dc.contributor.department交大名義發表zh_TW
dc.contributor.department電控工程研究所zh_TW
dc.contributor.departmentNational Chiao Tung Universityen_US
dc.contributor.departmentInstitute of Electrical and Control Engineeringen_US
Appears in Collections:Articles


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