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Patent Searching and Data


Title:
UNMANNED AERIAL VEHICLE TAKE-OFF AND LANDING CONTROL SYSTEM AND CONTROL METHOD
Document Type and Number:
WIPO Patent Application WO/2017/114295
Kind Code:
A1
Abstract:
Disclosed is an unmanned aerial vehicle take-off and landing control system and a control method. The control system comprises a magnet assembly arranged on a side of an unmanned aerial vehicle (1) and a magnetic field assembly arranged on a side of a parking apron. An electrification coil (2) is arranged in the magnetic field assembly. Current is introduced into the electrification coil (2). A supporting magnetic field is generated by the magnetic field assembly on the side of the parking apron, so that thrust acting on the unmanned aerial vehicle (1) is formed. Resultant force is formed by the thrust and a lift force or resistance in the unmanned aerial vehicle (1) take-off or landing processes to supplement the lift force or the resistance. In the unmanned aerial vehicle (1) take-off and landing processes, the current of the electrification coil (2) is changed to form a uniform magnetic field, the thrust acting on the unmanned aerial vehicle (1) is generated to supplement the lift force or the resistance in the take-off and landing processes, the safety performance of the unmanned aerial vehicle (1) is improved, the usage energy consumption of the unmanned aerial vehicle (1) is reduced, and the service life of the unmanned aerial vehicle (1) is prolonged.

Inventors:
HU TENGFEI (CN)
Application Number:
PCT/CN2016/111573
Publication Date:
July 06, 2017
Filing Date:
December 22, 2016
Export Citation:
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Assignee:
GOERTEK TECH CO LTD (CN)
International Classes:
B64C19/00; B64F1/00
Foreign References:
US20150251561A12015-09-10
CN101671988A2010-03-17
CN105667768A2016-06-15
CN205366055U2016-07-06
CN204297122U2015-04-29
CN103879563A2014-06-25
CN202193207U2012-04-18
CN204297116U2015-04-29
Other References:
See also references of EP 3372492A4
Attorney, Agent or Firm:
BEIJING LONGAN LAW FIRM (CN)
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