Fault Diagnosis and Fault-Tolerant Control of Micro-Satellite Propulsion Mode Attitude Control

Ho Nien Shou

doi:10.4028/www.scientific.net/AMM.764-765.607

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 764-765Fault Diagnosis and Fault-Tolerant Control of...

Fault Diagnosis and Fault-Tolerant Control of Micro-Satellite Propulsion Mode Attitude Control

Abstract:

Micro-satellite has long-term in-orbit work in the harsh environment of space, the components such as actuators and sensors in the attitude control system continue to perform in-orbit control operations, therefore are prone to faults. In practical mission, such as formation flying, orbital transfer, de-tumbing and attitude control need to use thruster to control. As the thrust control is fail, the entire mission fails. In the paper, the two-stage unscented kalman filter is used to obtain the effectiveness factor value and system estimated states are obtained. Meanwhile, a robust thruster controller is designed with the estimated results to accomplish the joint design of Fault Detection and Diagnosis and Fault-Tolerant Control.

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Periodical:

Applied Mechanics and Materials (Volumes 764-765)

Pages:

607-612

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.764-765.607

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Online since:

May 2015

Authors:

Ho Nien Shou*

Keywords:

Fault Detection, Fault Diagnosis, Fault-Tolerant Control, Robust Thruster Controller, Two-Stage Unscented Kalman Filter

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* - Corresponding Author

References

[1] R. Bucy: Nonlinear Filtering Theory, IEEE Transactions on Automatic Control, 10(2)(1965)198.

Google Scholar

[2] K. Xiong , H. Zhang and L. Liu: Adaptive robust extended Kalman filter for nonlinear stochastic systems, IET Control Theory & Applications, 2(3)(2008)239–250.

DOI: 10.1049/iet-cta:20070096

Google Scholar

[3] H.Z. Qiu, H.Y. Zhang and X.F. Sun: Solution of two-stage Kalman filter, IEE Proceedings - Control Theory and Applications, 152(2)(2005)152-156.

DOI: 10.1049/ip-cta:20045014

Google Scholar

[4] H.N. Shou: Micro-satellite Attitude Determination and Control Subsystem Design and Implementation: Software-in-the-loop Approach, Mathematical Problems in Engineering, (2014) Article ID 904708, 12 pages. http: /dx. doi. org/10. 1155/2014/904708.

DOI: 10.1155/2014/904708

Google Scholar

[5] H.N. Shou, Y. N. Liu, F. H. Liu and L. F. Lin: Micro-Satellite Robust Attitude Fault Tolerant Control, Journal of Air Force Institute of Technology, 10(1)(2011)103-114.

Google Scholar

[6] A. Isidori, and A. Astolfi: Disturbance Attenuation and Control via Measurement Feedback in Nonlinear Systems, IEEE Transaction on Automatic Control, 37(9)(1992) 1283-1293.

DOI: 10.1109/9.159566

Google Scholar