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The Ulysses spacecraft control and monitoring concepts and realitiesUlysses is a joint ESA-NASA mission, the primary purpose of the mission is to make scientific measurements of the Sun outside the plane of the ecliptic. The delay in launching Ulysses, due to the Challenger disaster, meant that the hardware on which the Spacecraft Control and Monitoring System (SCMS) resides was becoming obsolete, and it was decided to convert SCMS to run on a DEC/VAX machine under VMS. The paper will cover the spacecraft, the conversion, the converted SCMS, problems found, and the upgrades implemented for solutions. It will also discuss the future for and enhancements already made to the converted SCMS.
Document ID
19940019389
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hamer, Paul
(Cray Systems Bristol, United Kingdom)
Angold, Nigel
(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
94N23862
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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