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:
Nov. 03, 2020

Filed:

Mar. 26, 2018
Applicant:

Tata Consutancy Services Limited, Maharashtra, IN;

Inventors:

Vivek Chandel, Gurgaon, IN;

Kartik Muralidharan, Bangaluru, IN;

Avik Ghose, Kolkata, IN;

Archan Misra, Singapore, SG;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01P 21/00 (2006.01); G01C 19/5776 (2012.01); G01P 3/44 (2006.01); G01C 19/00 (2013.01); G01C 25/00 (2006.01);
U.S. Cl.
CPC ...
G01P 21/00 (2013.01); G01C 19/00 (2013.01); G01C 19/5776 (2013.01); G01C 25/005 (2013.01); G01P 3/44 (2013.01);
Abstract

Embodiments of the present disclosure provide systems and methods that establish non-linear components of gyroscope errors which have not been studied or explored earlier. These errors include but are not limited to non-linear dynamic error which is a function of the angular velocity itself. Bias instability has been observed within the same environment of temperature and atmospheric pressure. In other words, the embodiments of the present disclosure analyse and models static bias errors and dynamic non-linear errors in the gyroscope sensor which may be used to model and correct errors accordingly In subsequent measurements. The system provide solution(s) when there is no way of directly estimating temperature for bias correction of gyroscope, by estimating a temperature change by considering indirect measurements from other sensors present onboard the device.


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