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JUNO navigation for Jupiter orbit insertion

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dc.contributor.author Thompson, Paul F.
dc.contributor.author Ardalan, Shadan
dc.contributor.author Bordi, John
dc.contributor.author Bradley, Nicholas
dc.contributor.author Farnocchia, Davide
dc.contributor.author Takahashi, Yu
dc.date.accessioned 2020-03-11T18:23:05Z
dc.date.available 2020-03-11T18:23:05Z
dc.date.issued 2017-02-05
dc.identifier.citation 27th AAS/AIAA Space Flight Mechanics Meeting, San Antonio, Texas, February 5-9, 2017 en_US
dc.identifier.clearanceno CL#17-0486
dc.identifier.uri http://hdl.handle.net/2014/47504
dc.description.abstract Juno arrived at Jupiter on 05 July 2016 UTC, achieving orbit with the execution of the Jupiter Orbit Insertion (JOI) maneuver. Thanks to a dynamically wellbehaved spacecraft, the delivery of Juno to JOI was done largely with only a maneuver to setup and Earth gravity assist (EGA), an EGA, an EGA clean-up maneuver, and a JOI targeting maneuver. During the last several weeks of the approach to JOI, the dominant uncertainties in the predicted trajectory were from the Jupiter barycenter ephemeris. In this paper, we discuss the maneuver and orbit determination (OD) strategy for successfully arriving at JOI, the the challenges of calculating a correction to the Jupiter barycenter ephemeris using only radiometric data types, and how the ephemeris estimates during approach to JOI compare to a post-JOI trajectory reconstruction. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2017 en_US
dc.title JUNO navigation for Jupiter orbit insertion en_US
dc.type Preprint en_US


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