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Metrology, Attitude, and Orbit Determination for Spaceborne Interferometric Synthetic Aperture Radar

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dc.contributor.author Duren, R. en_US
dc.contributor.author Wong, E. en_US
dc.contributor.author Breckenridge, B. en_US
dc.contributor.author Shaffer, S. en_US
dc.contributor.author Duncan, C. en_US
dc.contributor.author Tubbs, E. en_US
dc.contributor.author Salomon, P. en_US
dc.date.accessioned 2004-09-24T20:21:45Z
dc.date.available 2004-09-24T20:21:45Z
dc.date.issued 1998-04-13 en_US
dc.identifier.citation Proc. of the Society of Photo-Optical Instrumentation Engineers, AeroSense'98 Meeting en_US
dc.identifier.citation Orlando, FL, U.S.A. en_US
dc.identifier.clearanceno 98-0367 en_US
dc.identifier.uri http://hdl.handle.net/2014/19131
dc.description.abstract The Shuttle Radar Topography Mission (SRTM), scheduled for a 10 day Space Shuttle flight in 1999, will use an Interferometric Synthetic Aperture Radar (IFSAR) instrument to produce a near-global digital elevation map of the earth's land surface with 16 m absolute vertical height accuracy at 30 meter postings. en_US
dc.format.extent 942595 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other metrology attitude determination orbit determination spacecraft guidance and control IFSAR en_US
dc.title Metrology, Attitude, and Orbit Determination for Spaceborne Interferometric Synthetic Aperture Radar en_US


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