Hybrid Attitude Saturation and Fault-Tolerant Control for Rigid Spacecraft without Unwinding

Hybrid Attitude Saturation and Fault-Tolerant Control for Rigid Spacecraft without Unwinding

This paper tackles the saturation and fault-tolerant attitude tracking problem without unwinding for rigid spacecraft with external disturbances and partial loss of actuator effectiveness faults. A hybrid saturation and fault-tolerant attitude control (HSFC) is proposed. The Lyapunov method is emplo...

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Bibliographic Details
Main Authors: Jun Ma, Zeng Wang, Chang Wang
Format: Article
Language:English
Published: MDPI AG 2023-08-01
Series:Mathematics
Subjects:
spacecraft attitude control
saturation control
unwinding
fault tolerant
Online Access:https://www.mdpi.com/2227-7390/11/15/3431

Internet

https://www.mdpi.com/2227-7390/11/15/3431

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