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Voyager 2 Neptune navigation resultsThe Voyager 2 spacecraft encounter with the planet Neptune on Aug. 25, 1989 presented a difficult but interesting challenge for navigation. Final plans and strategies are compared with the actual performance obtained during the encounter in three areas. First, the orbit determination experience during encounter is reviewed, and the expected accuracy compared with the history of encounter period orbit estimates. Second, the trajectory correction maneuver history is outlined to show how the planned strategy was carried out to achieve desired science zones while assuring spacecraft safety. Third, the late update strategy is outlined and it is shown how this custom designed, complex procedure was used to support the near encounter science observations.
Document ID
19900065913
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gray, D. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Matousek, S. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Francis, K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Potts, C. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Cesarone, R. J.
(JPL Pasadena, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Astrodynamics
Report/Patent Number
AIAA PAPER 90-2876
Report Number: AIAA PAPER 90-2876
Meeting Information
Meeting: AIAA/AAS Astrodynamics Conference
Location: Portland, OR
Country: United States
Start Date: August 20, 1990
End Date: August 22, 1990
Accession Number
90A52968
Distribution Limits
Public
Copyright
Other

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