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AMFESYS: Modelling and diagnosis functions for operations supportPacketized telemetry, combined with low station coverage for close-earth satellites, may introduce new problems in presenting to the operator a clear picture of what the spacecraft is doing. A recent ESOC study has gone some way to show, by means of a practical demonstration, how the use of subsystem models combined with artificial intelligence techniques, within a real-time spacecraft control system (SCS), can help to overcome these problems. A spin-off from using these techniques can be an improvement in the reliability of the telemetry (TM) limit-checking function, as well as the telecommand verification function, of the Spacecraft Control systems (SCS). The problem and how it was addressed, including an overview of the 'AMF Expert System' prototype are described, and proposes further work which needs to be done to prove the concept. The Automatic Mirror Furnace is part of the payload of the European Retrievable Carrier (EURECA) spacecraft, which was launched in July 1992.
Document ID
19940019414
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wheadon, J.
(European Space Agency. European Space Operations Center Darmstadt, Germany)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Publication Information
Publication: JPL, SpaceOps 1992: Proceedings of the Second International Symposium on Ground Data Systems for Space Mission Operations
Subject Category
Systems Analysis
Accession Number
94N23887
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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