DocumentCode
1828589
Title
A method for multiple fault isolation: Application to the rendez-vous phase of the Mars Sample Return mission
Author
Issury, I. ; Henry, David ; Olive, X.
Author_Institution
LAPS, Univ. Bordeaux 1, Bordeaux, France
fYear
2010
fDate
7-10 Sept. 2010
Firstpage
1
Lastpage
6
Abstract
This paper presents a formalized diagnosis technique for the isolation of multiple faults occurring in the orbiter´s measurement unit of the Mars Sample Return mission. The Mars Sample Return (MSR) mission is a flagship mission undertaken jointly by the National Aeronautics and Space Administration (NASA) and the European Space Agency (ESA). The goal is to return tangible samples from Mars atmosphere and ground to Earth for analysis. A key feature of the proposed method is that available hardware-based fault indicating signals are judiciously used with analytic-based fault indicating signals in order to construct the fault diagnosis scheme. The main advantage of the technique is that the number of fault indicating signals is guaranteed to be minimal for the given isolation task. The proposed method is based on logical tools derived from the set theory. Simulation results from a ”high-fidelity” industrial simulator demonstrate that the proposed method is able to diagnose multiple faults.
Keywords
Mars; aerospace instrumentation; fault diagnosis; set theory; space research; units (measurement); European Space Agency; Mars sample return mission; National Aeronautics and Space Administration; formalized diagnosis technique; hardware-based fault; multiple fault isolation; orbiter measurement unit; rendez-vous phase; set theory; Fault diagnosis; model-based residuals; multiple faults; set-based theory; spatial mission;
fLanguage
English
Publisher
iet
Conference_Titel
Control 2010, UKACC International Conference on
Conference_Location
Coventry
Electronic_ISBN
978-1-84600-038-6
Type
conf
DOI
10.1049/ic.2010.0330
Filename
6490788
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