Active fault-tolerant control system design for spacecraft attitude maneuvers with actuator saturation and faults

• Main Authors: Shen, Qiang, Yue, Chengfei, Goh, Cher Hiang, Wang, Danwei
• Other Authors: School of Electrical and Electronic Engineering
• Format: Article
• Language: English
• Published: 2020
• Subjects: Engineering::Electrical and electronic engineering; Actuators; Fault Detection and Identification
• Online Access: https://hdl.handle.net/10356/140487
• Institution: Nanyang Technological University

This paper designs an active fault-tolerant control system for spacecraft attitude control in the presence of actuator faults, fault estimation errors, and control input constraints. The developed fault-tolerant control system is able to detect the actuator fault without false alarms caused by exter...