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FR2621702A1 Expired / Lapsed FR ⏱️ 0.0 years remaining

Method and device compensating for gyromagnetic effects on a nuclear gyromagnetic resonance magnetometer

Assignee: Thales Avionics SAS
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Filing: 1987-10-13
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Granted: —
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Expires: 2007-10-13
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Abstract

Abstract The rotation of the magnetometer 100 with respect to the magnetic field @ to be measured is split into elementary rotations about three axes; for each axis around which a rotation of the magnetometer 100 induces a rotation of its liquids 2, 2', the corresponding speed of rotation P, Q, R of the magnetometer 100 is measured. Using an auxiliary magnetometer 7, the components Hx, Hy, Hz of the magnetic field @ are measured; a signal SE forming an estimate of the error is subtracted from the signal SH measuring the strength H of the magnetic field @ arising from the magnetometer 100, SE being equal to the sum of the products P.hx + Q.hy + R.hz of each measured speed of rotation and the projection on the corresponding axis of a unit vector having the direction of the said magnetic field. The invention finds application particularly in the measurement of variations in the earth's magnetic field.

Inventors

  • 👤 Jean-Louis Lescourret
  • 👤 Claude Sonrel

Bibliographic Details

Application Number —
Jurisdiction FR
Data Source google_patents
Last Synchronized 2026-11-10 02:00
CPC Classifications
G; G01; G01R; G01R33/00; G01R33/20; G01R33/24

Claims Analysis

Total Claims: 0
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References Cited (Backward Citations)

US2899637A Cited
US3697869A Cited
FR2132588A1 Cited
EP0067338A2 Cited
EP0206931A1 Cited

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