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Galileo spacecraft modeling for orbital operationsThe Galileo Jupiter orbital mission using the Low Gain Antenna (LGA) requires a higher degree of spacecraft state knowledge than was originally anticipated. Key elements of the revised design include onboard buffering of science and engineering data and extensive processing of data prior to downlink. In order to prevent loss of data resulting from overflow of the buffers and to allow efficient use of the spacecraft resources, ground based models of the spacecraft processes will be implemented. These models will be integral tools in the development of satellite encounter sequences and the cruise/playback sequences where recorded data is retrieved.
Document ID
19950011159
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mclaughlin, Bruce A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Nilsen, Erik N.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Publication Information
Publication: NASA. Goddard Space Flight Center, Third International Symposium on Space Mission Operations and Ground Data Systems, Part 2
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
95N17574
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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