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:
Feb. 21, 2023

Filed:

Oct. 15, 2020
Applicant:

Skydio, Inc., Redwood City, CA (US);

Inventors:

Anurag Makineni, San Jose, CA (US);

Kristen Marie Holtz, Redwood City, CA (US);

Gareth Benoit Cross, San Carlos, CA (US);

Hayk Martirosyan, San Francisco, CA (US);

Assignee:

SKYDIO, INC., Redwood City, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01S 19/47 (2010.01); B64C 39/02 (2023.01); G08G 5/00 (2006.01); G01P 15/18 (2013.01); G01C 19/00 (2013.01); G01P 15/08 (2006.01);
U.S. Cl.
CPC ...
G01S 19/47 (2013.01); B64C 39/024 (2013.01); G01C 19/00 (2013.01); G01P 15/08 (2013.01); G01P 15/18 (2013.01); G08G 5/0065 (2013.01); G08G 5/0069 (2013.01); B64C 2201/027 (2013.01); B64C 2201/145 (2013.01);
Abstract

In some examples, an unmanned aerial vehicle (UAV) may receive location information via the global navigation satellite system (GNSS) receiver and may receive acceleration information via an onboard accelerometer. The UAV may determine a first measurement of acceleration of the UAV in a navigation frame of reference based on information from the accelerometer prior to or during takeoff. In addition, the UAV may determine a second measurement of acceleration of the UAV in a world frame of reference based on the location information received via the GNSS receiver prior to or during takeoff. The UAV may determine a relative heading of the UAV based on the first and second acceleration measurements. The determined relative heading may be used for navigation of the UAV at least one of during or after takeoff of the UAV.


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