Reconfigurability Analysis for Satellite Attitude Control System

摘要：

Reconfigurability represents the potential of the system to tolerate faults under resources constraints. This paper provides an approach to evaluate and analyze the reconfigurability of satellite attitude control system (ACS) with respect to actuator faults under a certain configuration. The common configurations of ACS are presented. And the controllability and energy consumption of control are analyzed. Then the smallest eigenvalue of controllability Gramian is utilized to measure the level of reconfigurability. Simulation results are given to demonstrate the effectiveness of the proposed approach.

关键词： Satellite attitude control system Reconfigurability Fault tolerant control Actuator faults

作者: FAN Wen CHENG Yuehua JIANG Bin LIU Wenjing

作者单位: College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 21001 College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 21001 Beijing Institute of Control Engineering, Beijing 100190 National Laboratory of Space Intelligent Co

会议类型: 国际会议

会议名称: The 31st Chinese Control Conference(第三十一届中国控制会议)

会议地点: 合肥

会议语种:英文

页码: 5285-5289

在线出版日期: 2012-07-01（万方平台首次上网日期，不代表论文的发表时间）