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. 26, 2021

Filed:

Feb. 01, 2019
Applicant:

Hangzhou Zero Zero Technology Co., Ltd., Zhejiang, CN;

Inventors:

Tong Zhang, Zhejiang, CN;

Lei Zhang, Zhejiang, CN;

Zhaozhe Wang, Zhejiang, CN;

Xi Zhang, Zhejiang, CN;

Mengwen Tan, Zhejiang, CN;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/10 (2006.01); B64D 47/08 (2006.01); B64C 39/02 (2006.01); H04N 5/225 (2006.01); H04N 13/204 (2018.01); G06K 9/00 (2006.01); G06T 7/50 (2017.01); H04N 5/247 (2006.01);
U.S. Cl.
CPC ...
G05D 1/101 (2013.01); B64C 39/024 (2013.01); B64D 47/08 (2013.01); G06K 9/00624 (2013.01); G06T 7/50 (2017.01); H04N 5/2253 (2013.01); H04N 5/247 (2013.01); H04N 13/204 (2018.05); B64C 2201/141 (2013.01); G06T 2207/10028 (2013.01); G06T 2207/30252 (2013.01);
Abstract

An unmanned aerial vehicle is described herein. The unmanned aerial vehicle includes a fuselage body, a lift mechanism coupled to the fuselage body, and a depth sensing and obstacle avoidance system coupled to the fuselage body. The depth sensing and obstacle avoidance system includes a platform assembly, a pair of stereovision cameras coupled to a platform assembly, and a motor assembly coupled to the fuselage body and to the platform assembly. The platform assembly includes a support member extending between a first end and an opposite second end along a longitudinal axis. The pair of stereovision cameras includes each stereovision camera positioned at an opposite end of the support member. The motor assembly is configured to rotate the platform assembly with respect to the fuselage body about a rotational axis perpendicular to the longitudinal axis of the platform assembly.


Find Patent Forward Citations

Loading…