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:
Jul. 13, 2021

Filed:

Jul. 05, 2018
Applicant:

Aurora Flight Sciences Corporation, Manassas, VA (US);

Inventors:

Jae-Woo Choi, Manassas, VA (US);

James D. Paduano, Boston, MA (US);

Assignee:
Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G06K 9/00 (2006.01); H04N 13/239 (2018.01); G03B 15/00 (2021.01); G02B 26/08 (2006.01); B64C 39/02 (2006.01); F41H 13/00 (2006.01); G01S 17/89 (2020.01); G01B 11/25 (2006.01); G05D 1/00 (2006.01); G01S 17/66 (2006.01); F41H 11/04 (2006.01); G01S 17/86 (2020.01); F41H 11/02 (2006.01);
U.S. Cl.
CPC ...
H04N 13/239 (2018.05); B64C 39/024 (2013.01); F41H 11/02 (2013.01); F41H 11/04 (2013.01); F41H 13/00 (2013.01); F41H 13/005 (2013.01); G01B 11/25 (2013.01); G01B 11/2545 (2013.01); G01S 17/66 (2013.01); G01S 17/86 (2020.01); G01S 17/89 (2013.01); G02B 26/0833 (2013.01); G03B 15/006 (2013.01); G05D 1/0094 (2013.01); G06K 9/00671 (2013.01); B64C 2201/024 (2013.01); B64C 2201/127 (2013.01);
Abstract

The subject disclosure relates to a tracking system to mount to an aircraft and to image and track a target aircraft. The tracking system may include a structured light source operatively coupled to a processor, an inertial measurement unit (IMU) operatively coupled with the processor, a mirror to steer light from the light source toward the target aircraft, and a stereo-vision system having a first camera and a second camera. The IMU may be configured to generate position data representing a position of the aircraft. The stereo-vision system may be operatively coupled to the processor and configured to determine a 3D position of the target aircraft as a function of the position data. The processor may be configured to adjust the mirror position as a function of a mirror position.


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