Please use this identifier to cite or link to this item: https://hdl.handle.net/11681/3214
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dc.contributor.authorTodd, Mark-
dc.date.accessioned2016-03-16T15:01:47Z-
dc.date.available2016-03-16T15:01:47Z-
dc.date.issued1982-10-
dc.identifier.urihttp://hdl.handle.net/11681/3214-
dc.descriptionReport-
dc.descriptionAbstract: This report documents the tests and results obtained with the Rapid Geodetic Survey System (RGSS) at White Sands Missile Range in 1980. The performance capability of the system in the ground vehicle and helicopter modes is statistically characterized.-
dc.publisherU.S. Army Engineer Topographic Laboratories.-
dc.publisherEngineer Research and Development Center (U.S.)-
dc.relationhttp://acwc.sdp.sirsi.net/client/en_US/search/asset/1047611-
dc.relation.ispartofseriesETL ; 0308.-
dc.rightsApproved for public release; distribution is unlimited.-
dc.sourceThis Digital Resource was created from scans of the Print Resource.-
dc.subjectAnomaly-
dc.subjectDeflections-
dc.subjectDensification-
dc.subjectGravity-
dc.subjectGround vehicle-
dc.subjectHelicopter-
dc.subjectInertial-
dc.subjectRapid geodetic survey system-
dc.titleRapid geodetic survey system (RGSS) deflection of the vertical and gravity anomaly tests at White Sands Missile Range, 1980-
dc.typeReporten_US
Appears in Collections:Technical Report

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