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. 24, 2019

Filed:

Mar. 27, 2017
Applicant:

Intel Corporation, Santa Clara, CA (US);

Inventors:

Narayan Sundararajan, Palo Alto, CA (US);

Xue Yang, Arcadia, CA (US);

Suresh V. Golwalkar, Phoenix, AZ (US);

Mahanth Gowda, Urbana, IL (US);

Romit Roy Choudhury, Urbana, IL (US);

Assignee:

Intel Corporation, Santa Clara, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
A63B 69/36 (2006.01); G01P 15/08 (2006.01); A63B 24/00 (2006.01); A63B 69/00 (2006.01); A63B 43/00 (2006.01); G09B 9/00 (2006.01); G09B 19/00 (2006.01);
U.S. Cl.
CPC ...
A63B 69/3658 (2013.01); A63B 24/0021 (2013.01); A63B 43/004 (2013.01); A63B 69/0002 (2013.01); G01P 15/0885 (2013.01); G09B 9/00 (2013.01); G09B 19/0038 (2013.01); A63B 2024/0028 (2013.01); A63B 2209/08 (2013.01);
Abstract

Systems and techniques for sensor-derived object flight performance tracking are described herein. A set of magnetometer readings may be obtained from a magnetometer included with an object. A local rotation axis of the object may be determined at a time using the set of magnetometer readings. The local rotation axis may describe rotation of the object around a local magnetic target. A global rotation axis may be calculated based on an initial orientation of the object. The global rotation axis may describe a fixed rotation axis of the object during flight in a global coordinate frame, wherein an angle between the global rotation axis and magnetic north remains constant during the flight. An orientation of the object may be determined for the time using the global rotation axis and the local rotation axis of the object at the time.


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