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The processing of the Viking Orbiter range data and its contribution to Mars gravity solutionsThe processing of Doppler data has been the primary method for deriving models of the Mars gravity field. Since the Mariner 9 and Viking spacecraft were placed in orbit about Mars, many models from degree and order 6 to degree and order 50 have been developed. However, during the Viking mission, some 26,000 range measurements to the two Viking Orbiters were also obtained. These data have not previously been used in the derivation of Mars gravity models. A portion of these range data have been processed simultaneously with the Doppler data. Normal equations were generated for both sets of data and were used to create two solutions complete to degree and order 30: a nominal solution including both the range and the Doppler data (MGM-R100), and another solution including only the Doppler data (MGM-R101). Tests with the covariances of these solutions, as well as with orbit overlap tests indicate that the interplanetary range data can be used to improve the modeling of the Mars gravity field.
Document ID
19930064430
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lemoine, Frank G.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Rosborough, George W.
(Colorado Univ. Boulder, United States)
Smith, David E.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: Spaceflight mechanics 1992; Proceedings of the 2nd AAS(AIAA Meeting, Colorado Springs, CO, Feb. 24-26, 1992. Pt. 1 (A93-48426 20-12)
Publisher: Univelt, Inc.
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AAS PAPER 92-108
Accession Number
93A48427
Funding Number(s)
CONTRACT_GRANT: NGT-50329
Distribution Limits
Public
Copyright
Other

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