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:
Jan. 14, 2020

Filed:

May. 07, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Brendan Blanton, Wilmington, DE (US);

Deanna Dibernardi, Newtown Square, PA (US);

Robert Allen, Glen Mills, PA (US);

Katherine Gresko, Abington, PA (US);

Timothy Paul, Gilbertsville, PA (US);

Joseph Kenney, Media, PA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64F 1/20 (2006.01); G08G 5/00 (2006.01); B64D 1/22 (2006.01); B64D 47/08 (2006.01); B64C 27/06 (2006.01); G06K 9/00 (2006.01);
U.S. Cl.
CPC ...
B64F 1/20 (2013.01); B64C 27/06 (2013.01); B64D 1/22 (2013.01); B64D 47/08 (2013.01); G06K 9/0063 (2013.01); G08G 5/0047 (2013.01);
Abstract

Disclosed herein is a method that comprises acquiring one or more images of a plurality of markers of an off-board target using a camera onboard a rotorcraft, the plurality of markers arranged in a predefined pattern. The method also comprises processing, using an image processor, the one or more images of the plurality of markers to identify the predefined pattern of the plurality of markers. The method further comprises determining guidance information for the rotorcraft relative to the off-board target based on the identified predefined pattern of the plurality of markers, an orientation of the plurality of markers and a relative spacing of the plurality of markers. The method additionally comprises providing the determined guidance information to a display device within a field of view of an operator of the rotorcraft.


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