Fault-Tolerant Prescribed Performance Attitude Tracking Control for Spacecraft Under Input Saturation

This brief examines the problem of attitude tracking control with prescribed performance guarantees for a spacecraft subjected to actuator faults and input saturation. To pursue this, the open-loop tracking error dynamics with certain designer-specified performance constraints is first transformed i...

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Bibliographic Details
Published inIEEE transactions on control systems technology Vol. 28; no. 2; pp. 574 - 582
Main Authors Shao, Xiaodong, Hu, Qinglei, Shi, Yang, Jiang, Boyan
Format Journal Article
LanguageEnglish
Published New York IEEE 01.03.2020
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
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