Paper Title:
Satellite Fault Detection and Isolation through Decoupling Parity Space
  Abstract

In order to detect and isolate orbiting satellite actuator faults, a decoupling parity space method was extended. The decoupling parity vector was obtained using this method by singular value decomposition. Sometimes this vector may not exist, then by singular value substitution or generalized Eigen value method was used for solving the optimal approximation. The vector can easily make satellite actuator fault detected and isolated. The simulation results showed the effectiveness of the proposed algorithm.

  Info
Periodical
Chapter
Chapter 22: Metrology and Measurement
Edited by
Wu Fan
Pages
4406-4414
DOI
10.4028/www.scientific.net/AMM.110-116.4406
Citation
Z. Wang, Y. J. Li, X. W. Sun, "Satellite Fault Detection and Isolation through Decoupling Parity Space", Applied Mechanics and Materials, Vols. 110-116, pp. 4406-4414, 2012
Online since
October 2011
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