Fault diagnosis of satellite actuator based on bias-separated theory

	Fault diagnosis of satellite actuator based on bias-separated theory
	Li, D.-B.; X.-Q. Chen and C.-L. Li
	2015
发表期刊	Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics
卷号	37 期号:3 页码:606-612
摘要	An estimation method of input delay and control input fault is proposed. At first, based on the bias-separated theory, a normal control system model and a satellite attitude control system model with input delay and control input fault are set up respectively. Then, the input delay and control input fault can be estimated by the two-stage Kaman filter. Finally, the simulation of the method in a satellite attitude control system with actuator fault and input time delay illustrates the effectiveness of the proposed approach. Mathematical simulation and a real-time simulation based on the "KUAIZHOU-1" satellite control system hardware-in-the-loop simulation platform are performed to validate that the method is suitable and effective respectively. , 2015, Chinese Institute of Electronics. All right reserved.
文章类型	期刊论文
收录类别	EI
文献类型	期刊论文
条目标识符	http://ir.ciomp.ac.cn/handle/181722/56348
专题	中科院长春光机所知识产出
推荐引用方式 GB/T 7714	Li, D.-B.,X.-Q. Chen and C.-L. Li. Fault diagnosis of satellite actuator based on bias-separated theory[J]. Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics,2015,37(3):606-612.
APA	Li, D.-B.,&X.-Q. Chen and C.-L. Li.(2015).Fault diagnosis of satellite actuator based on bias-separated theory.Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics,37(3),606-612.
MLA	Li, D.-B.,et al."Fault diagnosis of satellite actuator based on bias-separated theory".Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics 37.3(2015):606-612.

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