Takagi-Sugeno fuzzy model based robust dissipative control for uncertain flexible spacecraft with saturated time-delay input

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• 作者：Shidong Xu ^{shidongxu@hit.edu.cn shidongxuhit@gmail.com} ; Guanghui Sun ; ^{guanghuisun@hit.edu.cn} ; Weichao Sun ^{1984sunweichao@gmail.com}
• 关键词：Takagi&ndash ; Sugeno fuzzy system ; Flexible spacecraft ; Robust dissipative control ; Saturated time-delay input ; Convex optimization technique
• 刊名：ISA Transactions
• 出版年：2017
• 出版时间：January 2017
• 年：2017
• 卷：66
• 期：Complete
• 页码：105-121
• 全文大小：4414 K
• 卷排序：66

文摘

T-S fuzzy approach is used to model flexible spacecraft. Dissipative performance is ensured to attenuate disturbances and vibration. Time delay, saturation, and uncertainty are simultaneously considered. A novel robust control strategy is developed. Performance comparison is performed.