The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 15, 2026

Filed:

Mar. 01, 2022
Applicant:

Office National D'etudes ET DE Recherches Aérospatiales, Palaiseau, FR;

Inventors:

Olivier Le Traon, Palaiseau, FR;

Raphaël Levy, Palaiseau, FR;

Jean Guerard, Palaiseau, FR;

Thomas Perrier, Palaiseau, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 19/5733 (2012.01); G01C 19/5607 (2012.01); G01C 19/5621 (2012.01); G01C 19/5656 (2012.01);
U.S. Cl.
CPC ...
G01C 19/5733 (2013.01); G01C 19/5607 (2013.01); G01C 19/5621 (2013.01); G01C 19/5656 (2013.01);
Abstract

An inertial angular position sensor includes at least three identical resonators which are arranged symmetrically about a sensitive axis of the sensor, so that a rate gyro constructed from the sensor has an integrating operation. The sensor further includes a coupling element which connects a vibrating portion of each resonator to the vibrating portions of all other resonators of the sensor. Preferred configurations for the inertial angular position sensor allow obtaining integrating rate gyros with high sensitivity and low production cost.


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