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. 25, 2017

Filed:

Nov. 30, 2015
Applicant:

Metal Industries Research & Development Centre, Kaohsiung, TW;

Inventors:

Chih-Ming Chang, Kaohsiung, TW;

Kuang-Shine Yang, Tainan, TW;

Ho-Chung Fu, Kaohsiung, TW;

Ying-Cherng Lu, Kaohsiung, TW;

Chih-Ming Chiou, Pingtung County, TW;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/08 (2006.01); B64C 27/08 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0825 (2013.01); B64C 27/08 (2013.01); B64C 39/024 (2013.01); B64C 2201/108 (2013.01);
Abstract

A multiple rotors aircraft and a control method thereof are provided. The control method comprises the following steps. First, current motion information of the multiple rotors aircraft is obtained. Then, at least one control gain is adjusted through a gain adjustment function according to the current motion information. The gain adjustment function conforms to a non-Lipschitzian characteristic, and at least one rotor of the multiple rotors aircraft is controlled according to the control gain. Therefore, the multiple rotors aircraft would be ensured that its flight attitude is toward a target position, and the expected result would be conformed rapidly.


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