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Title:
FLIGHT CONTROL METHOD, UNMANNED AERIAL VEHICLE, AND FLIGHT CONTROL SYSTEM
Document Type and Number:
WIPO Patent Application WO/2021/062817
Kind Code:
A1
Abstract:
A flight control method, an unmanned aerial vehicle (100), and a flight control system. The flight control method comprises: step S201. receiving a hit signal, the hit signal being used for triggering flight of a virtual unmanned aerial vehicle (201) after being hit in a simulated game interface of an unmanned aerial vehicle (100), and the hit signal further comprising hit parameters about the virtual unmanned aerial vehicle (201) being hit; step 202. obtaining a flight mode and flight parameters according to the hit parameters, the flight mode comprising at least one of a roll mode, a shake mode, a spin mode, or a drift mode; step 203. controlling the unmanned aerial vehicle (100) to fly according to the flight mode and the flight parameters, to simulate that the virtual unmanned aerial vehicle (201) is hit. The unmanned aerial vehicle (100) determines the flight mode and the flight parameters according to the hit signal, and executes at least one of rolling, shaking, spinning, or drifting, thereby implementing interaction between the real unmanned aerial vehicle (100) and the virtual unmanned aerial vehicle (201).

Inventors:
LV, Ximin (No. 9 Yuexing 1st Rd., Hi-Tech Park , Nanshan District, Shenzhen Guangdong 7, CN)
GAO, Xiang (No. 9 Yuexing 1st Rd., Hi-Tech Park , Nanshan District, Shenzhen Guangdong 7, CN)
Application Number:
CN2019/109743
Publication Date:
April 08, 2021
Filing Date:
September 30, 2019
Export Citation:
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Assignee:
SZ DJI TECHNOLOGY CO., LTD. (No. 9 Yuexing 1st Rd., Hi-Tech Park , Nanshan District, Shenzhen Guangdong 7, CN)
International Classes:
B64C27/08; A63F13/213; G05D1/10
Attorney, Agent or Firm:
LEADER PATENT & TRADEMARK FIRM (Bldg. A Winland International Center, No. 32 Xizhimen North Street. Haidian District, Beijing 2, CN)
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