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10000951
Fault Detection and Isolation in Attitude Control Subsystem of Spacecraft Formation Flying Using Extended Kalman Filters
Abstract:
In this paper, the problem of fault detection and isolation in the attitude control subsystem of spacecraft formation flying is considered. In order to design the fault detection method, an extended Kalman filter is utilized which is a nonlinear stochastic state estimation method. Three fault detection architectures, namely, centralized, decentralized, and semi-decentralized are designed based on the extended Kalman filters. Moreover, the residual generation and threshold selection techniques are proposed for these architectures.
Digital Object Identifier (DOI):

References:

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[2] Scharf, D.P.; Hadaegh, F.Y.; Ploen, S.R.; "A survey of spacecraft formation flying guidance and control. Part II: control," American Control Conference, 2004. Proceedings of the 2004, vol.4, no., pp.2976- 2985 vol.4, June 30 2004-July 2 2004.
[3] Jia Qing-xian; Zhang Ying-chun; Guan Yu; Wu Li-na; "Robust nonlinear unknown input observer-based fault diagnosis for satellite attitude control system," Intelligent Control and Information Processing 2011 2nd International Conference on , vol.1, no., pp.345-350, 2011.
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[11] P. C. Hughes, Spacecraft attitude Dynamics, John Wiley & Sons Inc., 1986.
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