Title:
AIRCRAFT AND CONTROL METHOD FOR SAME
Document Type and Number:
WIPO Patent Application WO/2019/244893
Kind Code:
A1
Abstract:
An aircraft (10) and a control method therefor. The aircraft (10) has: a velocity acquisition unit (80a) that acquires the velocity (v) of the aircraft (10); a roll angle calculation unit (80c) that calculates the roll angle (φ) of the aircraft (10); a turning radius calculation unit (80d) that calculates the turning radius (r) of the aircraft (10) on the basis of the velocity (v) and the roll angle (φ); and a yaw rate calculation unit (80e) that calculates the yaw rate (yr) of the aircraft (10) on the basis of the velocity (v) and the turning radius (r). A control unit (80f) controls flight of the aircraft (10) on the basis of the roll angle (φ) and the yaw rate (yr).
Inventors:
FURUKAWA JUN (JP)
KATO MASASHI (JP)
KATO MASASHI (JP)
Application Number:
PCT/JP2019/024118
Publication Date:
December 26, 2019
Filing Date:
June 18, 2019
Export Citation:
Assignee:
HONDA MOTOR CO LTD (JP)
International Classes:
B64C13/04; B64C27/08; B64C29/00; B64C39/02
Domestic Patent References:
| WO2017174944A1 | 2017-10-12 | |||
| WO2014195660A1 | 2014-12-11 |
Foreign References:
| JP2015205646A | 2015-11-19 | |||
| JP2007062451A | 2007-03-15 | |||
| US5738302A | 1998-04-14 |
Attorney, Agent or Firm:
CHIBA Yoshihiro et al. (JP)
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