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The influence of orbit selection on the accuracy of the Stanford Relativity gyroscope experimentThis paper discusses an error analysis for the Stanford Relativity experiment, designed to measure the precession of a gyroscope's spin-axis predicted by general relativity. Measurements will be made of the spin-axis orientations of 4 superconducting spherical gyroscopes carried by an earth-satellite. Two relativistic precessions are predicted: a 'geodetic' precession associated with the satellite's orbital motion and a 'motional' precession due to the earth's rotation. Using a Kalman filter covariance analysis with a realistic error model we have computed the error in determining the relativistic precession rates. Studies show that a slightly off-polar orbit is better than a polar orbit for determining the 'motional' drift.
Document ID
19800060873
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vassar, R.
(Stanford Univ. CA, United States)
Everitt, C. W. F.
(Stanford Univ. CA, United States)
Vanpatten, R. A.
(Stanford Univ. CA, United States)
Breakwell, J. V.
(Stanford University Stanford, Calif., United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1980
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AIAA PAPER 80-1671
Meeting Information
Meeting: Astrodynamics Conference
Location: Danvers, MA
Start Date: August 11, 1980
End Date: August 13, 1980
Sponsors: American Institute of Aeronautics and Astronautics and American Astronautical Society
Accession Number
80A45043
Funding Number(s)
CONTRACT_GRANT: NAS8-32605
Distribution Limits
Public
Copyright
Other

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