NDLI: Fault Detection and Isolation of Actuator Faults in Spacecraft Formation Flight

Content Provider	IEEE Xplore Digital Library
Author	Meskin, N. Khorasani, K.
Copyright Year	2006
Description	Author affiliation: Dept. of Electr. & Comput. Eng., Concordia Univ. (Meskin, N.; Khorasani, K.)
Abstract	This paper investigates the development of fault detection and isolation (FDI) filters for spacecraft formation flight. A MIMO architecture for formation flying control is considered. By utilizing a geometric FDI methodology, a local/decentralized detection filter is developed for detecting faults in other spacecraft by determining the required unobservability subspace of the local system. In the case when such an unobservability subspace does not exist, the required communication links between the spacecraft are specified. Simulation results presented demonstrate the effectiveness of our proposed methodology for FDI of formation flying systems
Starting Page	1159
Ending Page	1164
File Size	182230
Page Count	6
File Format	PDF
ISBN	1424401712
DOI	10.1109/CDC.2006.376679
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2006-12-13
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Fault detection Actuators Space vehicles Filters MIMO Control systems Robustness Electrical fault detection Communication system control Fault tolerant systems Geometric FDI Spacecraft formation flying Fault detection and isolation (FDI) Unobservability subspace
Content Type	Text
Resource Type	Article

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