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Orbit Determination Covariance Analyses for the Parker Solar Probe Mission

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dc.contributor.author Jones, Drew Ryan
dc.contributor.author Thompson, Paul
dc.contributor.author Valerino, Powtawche
dc.contributor.author Lau, Eunice
dc.contributor.author Goodson, Troy
dc.contributor.author Chung, Min-Kun
dc.contributor.author Mottinger, Neil
dc.date.accessioned 2019-07-02T21:14:34Z
dc.date.available 2019-07-02T21:14:34Z
dc.date.issued 2017-08-24
dc.identifier.citation AAS/AIAA Astrodynamics Specialist Conference, Stevenson, Washington, August 20-24, 2017 en_US
dc.identifier.clearanceno CL#17-3920
dc.identifier.uri http://hdl.handle.net/2014/46419
dc.description.abstract This paper details pre-launch navigation covariance analyses for the Parker Solar Probe mission. Baseline models and error assumptions are outlined. The results demonstrate how navigation will satisfy requirements and are used to define operational plans. A few sensitivities are identified and the accompanying investigations are described. Predicted state uncertainty results show that most requirements are met with substantial margin. Moreover, navigation sensitivities may be accommodated operationally and this has been incorporated into project planning. Detailed results are presented only for select launch dates, however twenty unique trajectories (one per launch opportunity) have been assessed. 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 Orbit Determination Covariance Analyses for the Parker Solar Probe Mission en_US
dc.type Preprint en_US


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