DocumentCode :
3113703
Title :
A Superconducting Gravity Gradiometer for inertial navigation
Author :
Moody, M.V. ; Paik, H.J.
Author_Institution :
Dept. of Phys., Maryland Univ., College Park, MD, USA
fYear :
2004
fDate :
26-29 April 2004
Firstpage :
775
Lastpage :
781
Abstract :
A sensitive gravity gradiometer suitable for operation on an aircraft or ship is being constructed. The design is based on superconducting accelerometer technology developed at the University of Maryland over the past two decades. A cryogenic instrument not only benefits from reduced thermal noise, but more importantly from the extraordinary stability of superconducting circuits and material properties at near-zero temperatures. The latter permits precise matching of scale factors and accurate rejection of dynamic errors. One of the main perceived drawbacks of the Superconducting Gravity Gradiometer (SGG) has been the necessity for a liquid helium cryostat. To avoid this constraint, the SGG is being integrated with a closed-cycle refrigerator for operation at 3 K.
Keywords :
gravimeters; inertial navigation; superconducting devices; 3 K; Superconducting Gravity Gradiometer; aircraft; closed-cycle refrigerator; cryogenic instrument; dynamic errors accurate rejection; inertial navigation; near-zero temperatures; precise matching; reduced thermal noise; scale factors; ship; Accelerometers; Aircraft manufacture; Aircraft navigation; Cryogenics; Gravity; Inertial navigation; Instruments; Marine vehicles; Noise reduction; Superconducting device noise;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Position Location and Navigation Symposium, 2004. PLANS 2004
Print_ISBN :
0-7803-8416-4
Type :
conf
DOI :
10.1109/PLANS.2004.1309073
Filename :
1309073
Link To Document :
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