Fixed-Time Attitude Control for Rigid Spacecraft With Actuator Saturation and Faults

标题
Fixed-Time Attitude Control for Rigid Spacecraft With Actuator Saturation and Faults
作者
关键词
-
出版物
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY
Volume 24, Issue 5, Pages 1892-1898
出版商
Institute of Electrical and Electronics Engineers (IEEE)
发表日期
2016-02-04
DOI
10.1109/tcst.2016.2519838

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