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A method for interactive satellite failure diagnosis: Towards a connectionist solutionVarious kinds of processes which allow one to make a diagnosis are analyzed. The analyses then focuses on one of these processes used for satellite failure diagnosis. This process consists of sending the satellite instructions about system status alterations: to mask the effects of one possible component failure or to look for additional abnormal measures. A formal model of this process is given. This model is an extension of a previously defined connectionist model which allows computation of ratios between the likelihoods of observed manifestations according to various diagnostic hypotheses. The expected mean value of these likelihood measures for each possible status of the satellite can be computed in a similar way. Therefore, it is possible to select the most appropriate status according to three different purposes: to confirm an hypothesis, to eliminate an hypothesis, or to choose between two hypotheses. Finally, a first connectionist schema of computation of these expected mean values is given.
Document ID
19890017219
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bourret, P.
(Centre d'Etudes et de Recherches Toulouse (France)., United States)
Reggia, James A.
(Maryland Univ. College Park., United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1989
Publication Information
Publication: NASA. Goddard Space Flight Center, The 1989 Goddard Conference on Space Applications of Artificial Intelligence
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
89N26590
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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