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Orbit determination strategy and results for the Pioneer 10 Jupiter missionPioneer 10 is the first earth-based vehicle to encounter Jupiter and occult its moon, Io. In contributing to the success of the mission, the Orbit Determination Group evaluated the effects of the dominant error sources on the spacecraft's computed orbit and devised an encounter strategy minimizing the effects of these error sources. The encounter results indicated that: (1) errors in the satellite model played a very important role in the accuracy of the computed orbit, (2) encounter strategy was sound, (3) all mission objectives were met, and (4) Jupiter-Saturn mission for Pioneer 11 is within the navigation capability.
Document ID
19740059055
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wong, S. K.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Lubeley, A. J.
(Philco-Ford Corp. Newport Beach, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
August 1, 1974
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 74-845
Meeting Information
Meeting: Mechanics and Control of Flight Conference
Location: Anaheim, CA
Start Date: August 5, 1974
End Date: August 9, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A41805
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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