CN108549225B - 基于增强型幂次趋近律和快速终端滑模面的刚性航天飞行器有限时间自适应容错控制方法 - Google Patents
基于增强型幂次趋近律和快速终端滑模面的刚性航天飞行器有限时间自适应容错控制方法 Download PDFInfo
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- G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
- G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
- G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
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Effective date of registration: 20230307 Address after: No.1 Zhengxue Road, Qinhuai District, Nanjing, Jiangsu 210001 Patentee after: NANJING CHENGUANG GROUP Co.,Ltd. Address before: B-2704, Woye Garden Business Office Building, No. 81, Ganquan Road, Shushan District, Hefei City, Anhui Province, 230088 Patentee before: HEFEI LONGZHI ELECTROMECHANICAL TECHNOLOGY Co.,Ltd. Effective date of registration: 20230307 Address after: B-2704, Woye Garden Business Office Building, No. 81, Ganquan Road, Shushan District, Hefei City, Anhui Province, 230088 Patentee after: HEFEI LONGZHI ELECTROMECHANICAL TECHNOLOGY Co.,Ltd. Address before: 310014 science and technology office, Zhejiang University of Technology, No. 18 Chao Wang Road, Xiacheng District, Hangzhou, Zhejiang Patentee before: JIANG University OF TECHNOLOGY |