A novel approach for satellite attitude reconfigurable fault-tolerant control

Y. Ch Zhang; X. Q. Chen; M. Chen; Y. H. Geng

doi:10.1109/ICIEA.2007.4318886

A novel approach for satellite attitude reconfigurable fault-tolerant control

Y. Ch Zhang^*
, X. Q. Chen
, M. Chen
, Y. H. Geng

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology
China Aerospace Science and Technology Corporation

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

4 Scopus citations

Abstract

This paper investigates the reconfiguration faulttolerant control method of the on-orbit satellite attitude control system with recovered faults. A novel integrated approach is proposed includes a control effectiveness factor and a reconfigurable fault-tolerant controller. A two-stage Kalman filtering algorithm is developed to estimate the size of control effectiveness factor in the closed-loop attitude control system. From the size of control effectiveness factor, a statistical hypothesis tests is developed to replace the fault detection and diagnosis (FDD) frame to diagnose whether there is some fault happened. Then, a reconfiguration fault-tolerant controller is utilized to compensate the primary controller by using the size of control effectiveness factor if some fault has happened. Finally, simulation is carried out and the results indicate the validation and effectiveness of the proposed solution.

Original language	English
Title of host publication	ICIEA 2007
Subtitle of host publication	2007 Second IEEE Conference on Industrial Electronics and Applications
Pages	2612-2616
Number of pages	5
DOIs	https://doi.org/10.1109/ICIEA.2007.4318886
State	Published - 2007
Event	2007 2nd IEEE Conference on Industrial Electronics and Applications, ICIEA 2007 - Harbin, China Duration: 23 May 2007 → 25 May 2007

Publication series

Name	ICIEA 2007: 2007 Second IEEE Conference on Industrial Electronics and Applications

Conference

Conference	2007 2nd IEEE Conference on Industrial Electronics and Applications, ICIEA 2007
Country/Territory	China
City	Harbin
Period	23/05/07 → 25/05/07

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10.1109/ICIEA.2007.4318886

Cite this

Zhang, Y. C., Chen, X. Q., Chen, M., & Geng, Y. H. (2007). A novel approach for satellite attitude reconfigurable fault-tolerant control. In ICIEA 2007: 2007 Second IEEE Conference on Industrial Electronics and Applications (pp. 2612-2616). Article 4318886 (ICIEA 2007: 2007 Second IEEE Conference on Industrial Electronics and Applications). https://doi.org/10.1109/ICIEA.2007.4318886

@inproceedings{ced757552c2947a3b5551976e1a4d751,

title = "A novel approach for satellite attitude reconfigurable fault-tolerant control",

abstract = "This paper investigates the reconfiguration faulttolerant control method of the on-orbit satellite attitude control system with recovered faults. A novel integrated approach is proposed includes a control effectiveness factor and a reconfigurable fault-tolerant controller. A two-stage Kalman filtering algorithm is developed to estimate the size of control effectiveness factor in the closed-loop attitude control system. From the size of control effectiveness factor, a statistical hypothesis tests is developed to replace the fault detection and diagnosis (FDD) frame to diagnose whether there is some fault happened. Then, a reconfiguration fault-tolerant controller is utilized to compensate the primary controller by using the size of control effectiveness factor if some fault has happened. Finally, simulation is carried out and the results indicate the validation and effectiveness of the proposed solution.",

author = "Zhang, \{Y. Ch\} and Chen, \{X. Q.\} and M. Chen and Geng, \{Y. H.\}",

year = "2007",

doi = "10.1109/ICIEA.2007.4318886",

language = "英语",

isbn = "1424407370",

series = "ICIEA 2007: 2007 Second IEEE Conference on Industrial Electronics and Applications",

pages = "2612--2616",

booktitle = "ICIEA 2007",

note = "2007 2nd IEEE Conference on Industrial Electronics and Applications, ICIEA 2007 ; Conference date: 23-05-2007 Through 25-05-2007",

}

Zhang, YC, Chen, XQ, Chen, M & Geng, YH 2007, A novel approach for satellite attitude reconfigurable fault-tolerant control. in ICIEA 2007: 2007 Second IEEE Conference on Industrial Electronics and Applications., 4318886, ICIEA 2007: 2007 Second IEEE Conference on Industrial Electronics and Applications, pp. 2612-2616, 2007 2nd IEEE Conference on Industrial Electronics and Applications, ICIEA 2007, Harbin, China, 23/05/07. https://doi.org/10.1109/ICIEA.2007.4318886

A novel approach for satellite attitude reconfigurable fault-tolerant control. / Zhang, Y. Ch; Chen, X. Q.; Chen, M. et al.
ICIEA 2007: 2007 Second IEEE Conference on Industrial Electronics and Applications. 2007. p. 2612-2616 4318886 (ICIEA 2007: 2007 Second IEEE Conference on Industrial Electronics and Applications).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - Zhang, Y. Ch

AU - Chen, X. Q.

AU - Chen, M.

AU - Geng, Y. H.

PY - 2007

Y1 - 2007

N2 - This paper investigates the reconfiguration faulttolerant control method of the on-orbit satellite attitude control system with recovered faults. A novel integrated approach is proposed includes a control effectiveness factor and a reconfigurable fault-tolerant controller. A two-stage Kalman filtering algorithm is developed to estimate the size of control effectiveness factor in the closed-loop attitude control system. From the size of control effectiveness factor, a statistical hypothesis tests is developed to replace the fault detection and diagnosis (FDD) frame to diagnose whether there is some fault happened. Then, a reconfiguration fault-tolerant controller is utilized to compensate the primary controller by using the size of control effectiveness factor if some fault has happened. Finally, simulation is carried out and the results indicate the validation and effectiveness of the proposed solution.

AB - This paper investigates the reconfiguration faulttolerant control method of the on-orbit satellite attitude control system with recovered faults. A novel integrated approach is proposed includes a control effectiveness factor and a reconfigurable fault-tolerant controller. A two-stage Kalman filtering algorithm is developed to estimate the size of control effectiveness factor in the closed-loop attitude control system. From the size of control effectiveness factor, a statistical hypothesis tests is developed to replace the fault detection and diagnosis (FDD) frame to diagnose whether there is some fault happened. Then, a reconfiguration fault-tolerant controller is utilized to compensate the primary controller by using the size of control effectiveness factor if some fault has happened. Finally, simulation is carried out and the results indicate the validation and effectiveness of the proposed solution.

UR - https://www.scopus.com/pages/publications/35248831161

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DO - 10.1109/ICIEA.2007.4318886

M3 - 会议稿件

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SN - 1424407370

SN - 9781424407378

T3 - ICIEA 2007: 2007 Second IEEE Conference on Industrial Electronics and Applications

SP - 2612

EP - 2616

BT - ICIEA 2007

T2 - 2007 2nd IEEE Conference on Industrial Electronics and Applications, ICIEA 2007

Y2 - 23 May 2007 through 25 May 2007

ER -

A novel approach for satellite attitude reconfigurable fault-tolerant control

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