Integral-type sliding mode fault-tolerant control for attitude stabilization of spacecraft

• Main Authors: Zhu, Senqiang, Shen, Qiang, Wang, Danwei, Poh, Eng Kee
• Other Authors: School of Electrical and Electronic Engineering
• Format: Article
• Language: English
• Published: 2015
• Online Access: https://hdl.handle.net/10356/79311; http://hdl.handle.net/10220/38578
• Institution: Nanyang Technological University

Two fault-tolerant control (FTC) schemes for spacecraft attitude stabilization with external disturbances are proposed in this brief. The approach is based on integral-type sliding mode control strategy to compensate for actuator faults without controller reconfiguration. First, a basic integral-typ...