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