DocumentCode
1009553
Title
Superconducting techniques for gravity survey and inertial navigation
Author
Chan, H.A. ; Aik, H. J P ; Moody, M.V. ; Parke, J.W.
Author_Institution
University of Maryland, College Park, Maryland
Volume
21
Issue
2
fYear
1985
fDate
3/1/1985 12:00:00 AM
Firstpage
411
Lastpage
414
Abstract
Major improvements in sensitivity and drift can be made in inertial instruments by utilizing benign properties of materials available at liquid helium temperatures. We are developing a three-axis gravity gradiometer in which magnetic fields produced by persistent currents are modulated by motions of superconducting proof masses. Signals arising from both differential and common mode motions of the proof masses are detected by SQUIDs. The present design parameters give an intrinsic gravity gradient noise of 2 × 10-12s-2Hz-1/2, subject to improvements with new superconducting techniques under tests. A demonstration of such high sensitivity requires a very strict control of all error sources. The performance of our prototype gravity gradiometer when tested in a noisy terrestrial environment with its sensitive axis tilted at an angle of
with respect to Earth\´s gravity is degraded to an error level of 7× 10-10s-2Hz-1/2. In order to compensate for common-acceleration induced errors, we are also developing a six-axis superconducting, accelerometer, based on a similar principle, which can detect the linear and angular acceleration vectors of the gradiometer platform simultaneously. Motion of a single, magnetically levitated, proof mass is monitored to resolve linear acceleration components to 4× 10-12m s-2Hz-1/2and angular acceleration components to 3 × 10-11rad s-2Hz-1/2. This accelerometer, combined with the gradiometer, represents a gradiometer-aided inertial navigation/survey system.
with respect to Earth\´s gravity is degraded to an error level of 7× 10-10s-2Hz-1/2. In order to compensate for common-acceleration induced errors, we are also developing a six-axis superconducting, accelerometer, based on a similar principle, which can detect the linear and angular acceleration vectors of the gradiometer platform simultaneously. Motion of a single, magnetically levitated, proof mass is monitored to resolve linear acceleration components to 4× 10-12m s-2Hz-1/2and angular acceleration components to 3 × 10-11rad s-2Hz-1/2. This accelerometer, combined with the gradiometer, represents a gradiometer-aided inertial navigation/survey system.Keywords
Gravity measurement; Inertial navigation; Superconducting devices; Acceleration; Accelerometers; Gravity; Inertial navigation; Instruments; Magnetic levitation; Magnetic materials; Superconducting device noise; Superconducting materials; Testing;
fLanguage
English
Journal_Title
Magnetics, IEEE Transactions on
Publisher
ieee
ISSN
0018-9464
Type
jour
DOI
10.1109/TMAG.1985.1063756
Filename
1063756
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