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Filter strategies for Mars Science Laboratory Orbit determination

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dc.contributor.author Thompson, Paul F.
dc.contributor.author Gustafson, Eric D.
dc.contributor.author Kruizinga, Gerhard L.
dc.contributor.author Martin-Mur, Tomas J.
dc.date.accessioned 2013-12-10T23:20:30Z
dc.date.available 2013-12-10T23:20:30Z
dc.date.issued 2013-02-10
dc.identifier.citation 23rd AAS/AIAA Spaceflight Mechanics Meeting, Kauai, Hawaii, February 10-14 2013 en_US
dc.identifier.clearanceno 13-0650
dc.identifier.uri http://hdl.handle.net/2014/44060
dc.description.abstract The Mars Science Laboratory (MSL) spacecraft had ambitious navigation delivery and knowledge accuracy requirements for landing inside Gale Crater. Confidence in the orbit determination (OD) solutions was increased by investigating numerous filter strategies for solving the orbit determination problem. We will discuss the strategy for the different types of variations: for example, data types, data weights, solar pressure model covariance, and estimating versus considering model parameters. This process generated a set of plausible OD solutions that were compared to the baseline OD strategy. Even implausible or unrealistic results were helpful in isolating sensitivities in the OD solutions to certain model parameterizations or data types. 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, 2013 en_US
dc.subject orbit determination en_US
dc.subject Mars Science Laboratory (MSL) en_US
dc.subject navigation en_US
dc.title Filter strategies for Mars Science Laboratory Orbit determination en_US
dc.type Preprint en_US


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