System-level prognostics approach for failure prediction of reaction wheel motor in satellites

被引:5
作者
Park, Hyung Jun [1 ]
Kim, Seokgoo [2 ]
Lee, Junyoung [3 ]
Kim, Nam Ho [2 ]
Choi, Joo-Ho [4 ]
机构
[1] Korea Aerosp Univ, Dept Smart Air Mobil, Goyang 10540, Gyeong Gi Do, South Korea
[2] Univ Florida, Dept Mech & Aerosp Engn, Gainesville, FL 32611 USA
[3] Korea Aerosp Univ, Dept Aerosp & Mech Engn, Goyang 10540, Gyeong Gi Do, South Korea
[4] Korea Aerosp Univ, Sch Aerosp & Mech Engn, Goyang 10540, Gyeong Gi Do, South Korea
基金
新加坡国家研究基金会;
关键词
Accelerated life test; Extended Kalman filter; Particle filter; Prognostics; Reaction wheel motor; Satellite; FAULT-DIAGNOSIS; LIFE PREDICTION; DEGRADATION;
D O I
10.1016/j.asr.2022.11.028
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The reaction wheels actuated by motors are widely used for advanced attitude control of satellites. During the satellite operation, the performance of reaction wheel motor degrades and results in unexpected failures. To guarantee the reliability and safety of satellites, it is important to predict its remaining useful life while it is in operation. To address this issue, this study presents a system-level prognostics approach for the reaction wheel motor, by regarding it as a system composed of multiple components. The approach is demonstrated by using the motor operation data obtained during the accelerated-life tests on ground for 3 years. Health degradation of each components of the motor are estimated using the adaptive extended Kalman filter. Failure threshold of the motor performance is established by the design requirement on characteristic curve. The anomaly detection and failure prediction are performed using the shifting kernel particle filter. (c) 2022 COSPAR. Published by Elsevier B.V. All rights reserved.
引用
收藏
页码:2691 / 2701
页数:11
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