Title:
飛翔機及び飛翔機の制御方法
Document Type and Number:
Japanese Patent JP7180450
Kind Code:
B2
Abstract:
To provide a flight machine which can suppress that an airframe moves away from a wall surface while suppressing power consumption.SOLUTION: A flight machine 10 comprises an airframe 11, a first wind direction anemometer 91, a second wind direction anemometer 92, and a control part 86. The airframe 11 has plural rotary wings 40A to 40D, and plural motors 41A to 41D. The first wind direction anemometer 91 is located on a front side of the airframe 11, and performs output according to a wind direction and a wind speed of first cross wind W1. The second wind direction anemometer 92 is located on a rear side of the airframe 11, and performs output according to a wind direction and a wind speed of second cross wind W2. The control part 86 performs the following control when a rotation moment acts around a yaw axis of the airframe 11 by first cross wind W1 and second cross wind W2 in the case that the front side of the airframe 11 contacts a wall surface. That is, the control part 86 controls the airframe 11 on the basis of output of the first wind direction anemometer 91 and output of the second wind direction anemometer 92 so that a rotation moment M is reduced.SELECTED DRAWING: Figure 8
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Inventors:
Yoshiro Haneda
Taku Kudo
Taku Kudo
Application Number:
JP2019036867A
Publication Date:
November 30, 2022
Filing Date:
February 28, 2019
Export Citation:
Assignee:
富士通株式会社
International Classes:
B64C25/36; B64C13/16; B64C27/08; B64C39/02; B64D27/24; G01P13/00; G05D1/10
Domestic Patent References:
| JP2017083318A | ||||
| JP2016145734A | ||||
| JP2017501405A | ||||
| JP2017039334A | ||||
| JP2013107626A | ||||
| JP2012228944A | ||||
| JP2017171014A | ||||
| JP2016215958A |
Attorney, Agent or Firm:
Atsushi Nakajima
Kato Kazuho
Hiroshi Fukuda
Kato Kazuho
Hiroshi Fukuda