Fault detection and diagnosis for reaction wheels of satellite's attitude control system using a bank of Kalman filters

被引：0
|
作者：
Tudoroiu, N [1 ]
Khorasani, K [1 ]
机构：
[1] Concordia Univ, Dept Elect & Comp Engn, Montreal, PQ H3G 1M8, Canada
来源：
ISSCS 2005: International Symposium on Signals, Circuits and Systems, Vols 1 and 2, Proceedings | 2005年
关键词：
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
The main objective of this research is the development of an isolation and detection interacting multiple model (IMM) algorithm for partial (soft) or total (hard) reaction wheel failures in the spacecraft attitude control system (ACS). Based on different scenarios and assumptions we develop healthy models of the ACS under various operating conditions and construct faulty modes with respect to temperature changes, power supply line voltage changes, torque variations, and unexpected current variations in each motor axis windings of the reaction wheels. Once a fault mode is detected and isolated we will be able to develop in certain conditions the recovery procedure through feedback control strategies for the ACS.
引用
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页码：199 / 202
页数：4
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