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:
Mar. 12, 2019

Filed:

Sep. 02, 2016
Applicants:

Alexander Trusov, Woodland Hills, CA (US);

Mark R. Phillips, Chardon, OH (US);

George H. Mccammon, Moorpark, CA (US);

Inventors:

Alexander Trusov, Woodland Hills, CA (US);

Mark R. Phillips, Chardon, OH (US);

George H. McCammon, Moorpark, CA (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01C 25/00 (2006.01); G01C 21/18 (2006.01);
U.S. Cl.
CPC ...
G01C 25/00 (2013.01); G01C 21/18 (2013.01); G01C 25/005 (2013.01);
Abstract

One embodiment describes an inertial system. The system includes a gyroscope system comprising a plurality of gyroscopes. The gyroscope system can be configured to provide rotation rate data associated with rotation of the plurality of gyroscopes about a respective plurality of sensitive axes. The system also includes a rotation sensor system configured to calculate navigation data based on the rotation rate data. The rotation sensor system includes a self-calibration component configured to designate a first gyroscope of the plurality of gyroscopes for self-calibration during operation of the inertial system and to inject a calibration input signal into the first gyroscope. The self-calibration component being configured to calibrate the first gyroscope based on the rotation rate data of the first gyroscope corresponding to the calibration input signal relative to the rotation rate data associated with a remaining at least one of the plurality of gyroscopes.


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