Title:
UNMANNED AERIAL VEHICLE, FLIGHT CONTROL MECHANISM FOR UNMANNED AERIAL VEHICLE, AND METHOD FOR USING UNMANNED AERIAL VEHICLE AND MECHANISM FOR UNMANNED AERIAL VEHICLE
Document Type and Number:
WIPO Patent Application WO/2019/198155
Kind Code:
A1
Abstract:
The purpose of the present invention is to provide a flight control mechanism for controlling flight of an unmanned aerial vehicle by controlling collision between the vehicle and a boundary surface, an unmanned aerial vehicle equipped with the mechanism, and a method for using the mechanism and the vehicle. Provided is a flight control mechanism for an unmanned aerial vehicle including: a first initial collision member; a second initial collision member; and a holding member that holds the first and second initial collision members with a space therebetween above the body of the unmanned aerial vehicle, is tiltable with respect to the vehicle body by rotating about a predetermined position inside or above the vehicle body toward the side of the vehicle body, and rotates in response to collision between the first or second initial collision member and a boundary surface.
Inventors:
KUROIWA KENJI (JP)
INOUE SHOSUKE (JP)
INAGAKI YUSUKE (JP)
INOUE SHOSUKE (JP)
INAGAKI YUSUKE (JP)
Application Number:
PCT/JP2018/015100
Publication Date:
October 17, 2019
Filing Date:
April 10, 2018
Export Citation:
Assignee:
AUTONOMOUS CONTROL SYSTEMS LABORATORY LTD (JP)
NJS CO LTD (JP)
NJS CO LTD (JP)
International Classes:
B64C39/02; B64C13/18; B64C13/20; B64C27/04; B64D25/00; B64D43/00; B64D47/08
Domestic Patent References:
| WO2017183219A1 | 2017-10-26 |
Foreign References:
| JP2017136914A | 2017-08-10 | |||
| JP2016211878A | 2016-12-15 | |||
| JP2018505094A | 2018-02-22 | |||
| JP2005193727A | 2005-07-21 | |||
| JP2006051841A | 2006-02-23 |
Attorney, Agent or Firm:
TANAKA Shinichiro et al. (JP)
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