A New Decoupling Matrix Construction Method for Fault Detection and Isolation of a Redundant Strapdown Inertial Measurement Unit-Reference-Cited by-同舟云学术

A New Decoupling Matrix Construction Method for Fault Detection and Isolation of a Redundant Strapdown Inertial Measurement Unit

Published:2017 Issue:1 Volume:60 Page:60-63
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

FU Wen Xing¹,ZHANG Tong¹,REN Zi Jun¹

Affiliation:

1. School of Astronautics, Northwestern Polytechnical University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/60/1/60_T-16-7/_pdf

Reference10 articles.

1. 1) Kim, S., Kim, Y., Park, C. G., and Jung, I.: Hybrid Fault Detection and Isolation Techniques for Aircraft Inertial Measurement Sensors, AIAA Guidance, Navigation, and Control Conference and Exhibit, Providence, Rhode Island, August 2004.

2. 2) Kim, K. H. and Lee, J. G.: Extension of Parity Space Approach for Two-Fault Detection and Isolation, AIAA Guidance, Navigation, and Control Conference and Exhibit, San Francisco, California, August 2005.

3. 3) Potter, J. E. and Suman, M. C.: Thresholdless Redundancy Management with Arrays of Skewed Instruments, Integrity in Electronic Flight Control Systems, 15, 1 (1977), pp. 15–25.

4. 4) Daly, K. C., Gai, E., and Harrison, J. V.: Generalized Likelihood Test for FDI in Redundant Sensor Configurations, Guidance and Control, 2, 1 (1978), pp. 9–17.

5. 5) Jin, H. and Zhang, H.: Optimal Parity Vector Sensitive to Designated Sensor Fault, IEEE Trans. Aerospace Electronic Syst., 35, 4 (1999), pp. 1122–1128.

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