Jianq Chyun IP Office
Multiple rotors aircraft and control method
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.
Metal Industries Research & Development Centre
B G B B G B
B64C G05D B64C B64C G05D B64C
additional inventional inventional additional inventional additional
Ying-Cherng Chih-Ming Kuang-Shine Chih-Ming Ho-Chung
Lu Chang Yang Chiou Fu