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Satellite ephemerides for Voyager Saturn encounterSatellite ephemerides played an important role in the navigation of the Voyager 1 and 2 Saturn encounters. They were used in the models of the gravitational forces acting on the spacecraft and of the onboard optical navigation measurements. They also were used in predicting the pointing directions of the onboard instruments for satellite scientific observations. This paper describes the form of the Voyager Saturn satellite ephemerides and gives the values of the parameters used in the ephemeris generation. The update of those parameters as part of the optical navigation process is also discussed, and the best Voyager ephemerides are presented and compared to those based on earlier Saturn satellite theories.
Document ID
19820055357
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jacobson, R. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Campbell, J. K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Synnott, S. P.
(NASA Jet Propulsion Laboratory Pasadena, CA, United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1982
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AIAA PAPER 82-1472
Meeting Information
Meeting: Astrodynamics Conference
Location: San Diego, CA
Start Date: August 9, 1982
End Date: August 11, 1982
Sponsors: American Institute of Aeronautics and Astronautics and American Astronautical Society
Accession Number
82A38892
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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