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:
May. 09, 2017

Filed:

Nov. 02, 2015
Applicant:

Orbital Atk, Inc., Dulles, VA (US);

Inventors:

Thomas Reinke, Clearwater, FL (US);

John R. Kenyon, Safety Harbor, FL (US);

Assignee:

Orbital ATK, Inc., Plymouth, MN (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G08G 5/04 (2006.01); G06T 7/20 (2006.01); G06K 9/00 (2006.01); G06T 7/60 (2017.01); G08G 5/00 (2006.01); G06K 9/62 (2006.01); G06K 9/20 (2006.01);
U.S. Cl.
CPC ...
G08G 5/04 (2013.01); G06K 9/00624 (2013.01); G06K 9/6202 (2013.01); G06T 7/20 (2013.01); G06T 7/60 (2013.01); G08G 5/0008 (2013.01); G08G 5/045 (2013.01); G06K 9/00785 (2013.01); G06K 9/00805 (2013.01); G06K 9/2018 (2013.01); G06T 2210/21 (2013.01);
Abstract

A method of operating a rotorcraft collision avoidance system is provided. The method includes determining a unique characteristic of a detected rotorcraft, determining the actual length of a first rotor based at least in part on the determined unique characteristic of the rotorcraft, locating a major axis of the first rotor of the rotorcraft from a perspective of a home unit, from the perspective of the home unit, determining an angular extent of the major axis of the first rotor, and determining the then current distance from the home unit to the rotorcraft based at least in part on the determined actual length of the first rotor and the corresponding angular extent.


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