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. 28, 2020

Filed:

Jun. 29, 2016
Applicant:

Yuneec Technology Co., Limited, Kowloon, Hong Kong, CN;

Inventors:

Yu Tian, Jiangsu, CN;

Wenyan Jiang, Jiangsu, CN;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01C 21/00 (2006.01); G01S 7/481 (2006.01); G01S 17/933 (2020.01); G01S 17/86 (2020.01); B64C 39/02 (2006.01); B64D 47/08 (2006.01); G03B 15/00 (2006.01); G03B 17/12 (2006.01); G06K 9/20 (2006.01); G06K 9/46 (2006.01); G06T 7/60 (2017.01); H04N 5/232 (2006.01); G06K 9/62 (2006.01); G05D 1/00 (2006.01); G05D 1/02 (2020.01); G06K 9/00 (2006.01); G05D 1/10 (2006.01); G08G 5/04 (2006.01); H04N 5/247 (2006.01);
U.S. Cl.
CPC ...
G01C 21/005 (2013.01); B64C 39/024 (2013.01); B64D 47/08 (2013.01); G01S 7/481 (2013.01); G01S 17/86 (2020.01); G01S 17/933 (2013.01); G03B 15/006 (2013.01); G03B 17/12 (2013.01); G05D 1/0038 (2013.01); G05D 1/0094 (2013.01); G05D 1/0202 (2013.01); G05D 1/101 (2013.01); G06K 9/0063 (2013.01); G06K 9/209 (2013.01); G06K 9/46 (2013.01); G06K 9/4604 (2013.01); G06K 9/6202 (2013.01); G06T 7/60 (2013.01); G08G 5/045 (2013.01); H04N 5/2328 (2013.01); H04N 5/23296 (2013.01); B64C 2201/027 (2013.01); B64C 2201/108 (2013.01); B64C 2201/141 (2013.01); B64C 2201/146 (2013.01); G06K 2209/21 (2013.01); G06T 2207/10032 (2013.01); H04N 5/23238 (2013.01); H04N 5/247 (2013.01);
Abstract

An aircraft and an obstacle avoidance method and system thereof. The obstacle avoidance system comprises an image capturing apparatus (), a gimbal stability-enhancement system, and a second controller (). The gimbal stability-enhancement system comprises a gimbal body () and a gimbal control system (). The image capturing apparatus () is arranged on the gimbal body (), and is used for capturing an image in a flying direction when the aircraft is flying. The gimbal control system () is connected to the gimbal body (). The second controller () is used for determining whether an obstacle exists in the image captured by the image capturing apparatus (), and if yes, changing the flying direction of the aircraft according to a position of the obstacle, and if not, controlling the aircraft to fly in the current flying direction.


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