Title:
METHOD FOR CONTROLLING DEFORMABLE ROLLING AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2023/124124
Kind Code:
A1
Abstract:
A method for controlling a deformable rolling aircraft. The method comprises the following steps: after a control system receives a starting signal, a driving device (5) driving a rotor wing to rotate, and the rotor wing generating a lifting force, so that a first wing (21) and a second wing (22) are unfolded towards two sides away from a substrate (1), and the deformable rolling aircraft being in a flight state; after the control system receives a landing signal, the driving device (5) driving the rotor wing to decelerate, and after the deformable rolling aircraft descends and lands, the first wing (21) and the second wing (22) being unfolded in the direction of the substrate (1) to form a spherical shape; and when the deformable rolling aircraft is of the spherical shape, after the control system receives a rolling signal, the driving device (5) driving at least part of the rotor wing to rotate, and the rotor wing generating a tangential force, so that the spherical deformable rolling aircraft is in a rolling state. By means of the control method, another playing mode can be achieved after landing, and the playing methods of the aircraft are enriched, thereby improving the playability and fun thereof.
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Inventors:
CHEN ZEFENG (CN)
CHEN BAOCAI (CN)
CHEN BAOCAI (CN)
Application Number:
PCT/CN2022/113480
Publication Date:
July 06, 2023
Filing Date:
August 19, 2022
Export Citation:
Assignee:
ALPHA GROUP CO LTD (CN)
GUANGZHOU ALPHA CULTURE COMMUNICATIONS CO LTD (CN)
GUANGZHOU ALPHA CULTURE COMMUNICATIONS CO LTD (CN)
International Classes:
B64C1/30; B64C27/08; B64D45/06
Foreign References:
CN114313210A | 2022-04-12 | |||
CN114194389A | 2022-03-18 | |||
CN216375004U | 2022-04-26 | |||
CN216375003U | 2022-04-26 | |||
CN110844069A | 2020-02-28 | |||
CN113148129A | 2021-07-23 | |||
US20140084114A1 | 2014-03-27 | |||
CN106586006A | 2017-04-26 |
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