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:
May. 12, 2020

Filed:

Dec. 01, 2017
Applicants:

Alexander A. Trusov, Studio City, CA (US);

Youngmin Albert Choi, Agoura Hills, CA (US);

David Dexter Lynch, Santa Barbara, CA (US);

Inventors:

Alexander A. Trusov, Studio City, CA (US);

Youngmin Albert Choi, Agoura Hills, CA (US);

David Dexter Lynch, Santa Barbara, CA (US);

Assignee:

NORTHROP GRUMMAN SYSTEMS CORPORATION, Falls Church, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 19/5726 (2012.01); G01C 25/00 (2006.01); G01C 19/5755 (2012.01); G01C 19/574 (2012.01); G01P 15/18 (2013.01); G01P 15/13 (2006.01);
U.S. Cl.
CPC ...
G01C 19/5726 (2013.01); G01C 19/574 (2013.01); G01C 19/5755 (2013.01); G01C 25/005 (2013.01); G01P 15/132 (2013.01); G01P 15/18 (2013.01);
Abstract

One embodiment includes a gyroscope system. The system includes a sensor system comprising a vibrating-mass and electrodes each arranged to provide one of a driving force and a force-rebalance to the vibrating-mass in each of three orthogonal axes. The system also includes a gyroscope controller that generates a drive signal provided to a first electrode of the electrodes to provide the driving force to facilitate an in-plane periodic oscillatory motion of the vibrating-mass along a first axis of the three orthogonal axes. The gyroscope controller also generates a force-rebalance signal provided to each of a second electrode and a third electrode of the plurality of electrodes associated with a respective second axis and a respective third axis of the three orthogonal axes to calculate a rotation of the gyroscope system about the respective second axis and the respective third axis of the three orthogonal axes.


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