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:
Jun. 06, 2017

Filed:

Jul. 16, 2014
Applicant:

Innalabs Limited, Dublin, IE;

Inventors:

Isaak Markovich Okon, Brooklyn, NY (US);

Alain Renault, Le Cannet, FR;

Jose Beitia, Dublin, IE;

Assignee:

Innalabs Limited, Dublin, IE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 19/00 (2013.01); G01C 19/567 (2012.01); G01C 25/00 (2006.01); G01C 19/56 (2012.01); G01C 19/5776 (2012.01); G01C 19/5614 (2012.01); G01C 19/5649 (2012.01); G01C 19/5726 (2012.01);
U.S. Cl.
CPC ...
G01C 25/00 (2013.01); G01C 19/56 (2013.01); G01C 19/5776 (2013.01); G01C 25/005 (2013.01); G01C 19/567 (2013.01); G01C 19/5614 (2013.01); G01C 19/5649 (2013.01); G01C 19/5726 (2013.01);
Abstract

The present invention is concerned with a method of calibrating a vibrating gyroscope. The method comprises exciting a vibration along an excitation axis of a resonant structure wherein the excitation axis is positioned at a first angular position, sensing the vibration of the resonant structure on a first sensing axis of the resonant structure while the excitation axis is positioned at the first angular position, generating a first sensing signal indicative of the sensed vibration of the resonant structure on the first sensing axis, rotating the excitation axis in a continuous manner around the resonant structure to a second angular position, sensing the vibration of the resonant structure on a second sensing axis of the resonant structure while the excitation axis is positioned at the second angular position, generating a second sensing signal indicative of the sensed vibration of the resonant structure on the second sensing axis and adding the first sensing signal to the second sensing signal in order to derive a bias of the gyroscope.


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