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Voyager 2 Uranus targeting strategyOne of the major challenges involved in the Voyager 2 Uranus flyby is to deliver the spacecraft to an appropriate aimpoint at the optimum time, so as to maximize the science return of the mission, while yet keeping propellant expenditure low. An unusual targeting strategy has been devised to satisfy these requirements. Its complexity arises from the great distance of the planet Uranus and the limited performance capabilities of Voyager. This selected strategy is developed in relation to a set of candidate strategies, mission requirements and shifting science objectives. The analysis of these candidates is conducted via a Monte Carlo simulation, the results of which yield data for the comparative evaluation and eventual and selection of the actual targeting strategy to be employed.
Document ID
Document Type
Conference Paper
Cesarone, R. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Gray, D. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Potts, C. L.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Francis, K.
(California Institute of Technology, Jet Propulsion Laboratory; Federal Electric Corp. Pasadena, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AAS PAPER 85-379
Accession Number
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