• 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