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:
Apr. 09, 2019

Filed:

Jul. 02, 2015
Applicants:

Shenzhen Cimc-tianda Airport Support Ltd., Guangdong, CN;

China International Marine Containers (Group) Ltd., Guangdong, CN;

Inventors:

Lan Deng, Shenzhen, CN;

Shaomin Chang, Shenzhen, CN;

Wei Xiang, Shenzhen, CN;

Yuefeng Yang, Shenzhen, CN;

Haibin Wang, Shenzhen, CN;

Haiqiu Liu, Shenzhen, CN;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06K 9/62 (2006.01); G01S 17/06 (2006.01); G01S 17/88 (2006.01); G08G 5/06 (2006.01); B64F 1/00 (2006.01); G06K 9/00 (2006.01); G06K 9/20 (2006.01); G06K 9/36 (2006.01); G06K 9/60 (2006.01); H04N 7/00 (2011.01);
U.S. Cl.
CPC ...
G06K 9/6202 (2013.01); B64F 1/002 (2013.01); G01S 17/06 (2013.01); G01S 17/88 (2013.01); G06K 9/00791 (2013.01); G08G 5/06 (2013.01); G08G 5/065 (2013.01); B64F 1/00 (2013.01); G06K 9/20 (2013.01); G06K 9/36 (2013.01); G06K 9/60 (2013.01); H04N 7/00 (2013.01);
Abstract

A system and method for aircraft docking guidance and aircraft type identification. The method is executed in the system for aircraft docking guidance and aircraft type identification comprising a machine vision sub-system, a laser scanning sub-system and a fusion module. The method includes: in step, obtaining, by the machine vision sub-system, an image via image capturing means, and calculating a first aircraft front wheel position therefrom; in step, obtaining, by the laser scanning sub-system, the position of the nose of an aircraft via laser scanning means, and calculating a second aircraft front wheel position; in step, fusing the first aircraft front wheel position and the second aircraft front wheel position according to a fusion rule, to obtain deviation of an aircraft front wheel.


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