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:
Dec. 22, 2020

Filed:

Aug. 18, 2018
Applicant:

Haoxiang Electric Energy (Kunshan) Co., Ltd., Jiangsu, CN;

Inventors:

Yu Tian, Jiangsu, CN;

Wenyan Jiang, Jiangsu, CN;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/08 (2006.01); B64C 39/02 (2006.01); G05D 1/06 (2006.01); G08G 5/00 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0816 (2013.01); B64C 39/024 (2013.01); G05D 1/0669 (2013.01); B64C 2201/146 (2013.01); G08G 5/0069 (2013.01);
Abstract

A method for controlling an attitude of a rotor UAV (unmanned aerial vehicle) includes judging whether the rotor UAV is in a first attitude on a support base; and starting a first thrust generating device which is offset from a first side of a center of gravity of the rotor UAV, the first thrust generating device generating a thrust that faces away from the support base while working, the first side moving away from the support base, flipping the rotor UAV and switching the rotor UAV from the first attitude to a second attitude. Also, a system for controlling the attitude of the rotor UAV is provided. According to the method and the system, the rotor UAV can be switched between different attitudes without artificially assisting in adjusting a current attitude of the rotor UAV, so that the convenience in use and the satisfaction of experience are improved.


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