Title:
観測装置
Document Type and Number:
Japanese Patent JP6409503
Kind Code:
B2
Abstract:
A observation device includes an aircraft and an observation unit attached to the aircraft that observes a target within a predetermined view angle. The aircraft includes a base, at least two thrusters that generate a propulsion force including lift, actuators that change a direction of the propulsion force generated by the thrusters with respect to the base, an inertial measurement unit (IMU) that detects an orientation of the base with respect to a ground surface, and a controller that controls the thrusters and the actuators based on the orientation of the base detected by the IMU. The observation unit is fixedly attached to the base and the aircraft is configured to fly in any arbitrary orientation with respect to the ground surface through a combination of a magnitude of the propulsion force and the direction of the propulsion force of each of the thrusters.
Inventors:
Takenori Matsue
Koji Kawasaki
Michihiro Matsuura
Masami Kurosaka
Masayuki Inaba
Koji Kawasaki
Michihiro Matsuura
Masami Kurosaka
Masayuki Inaba
Application Number:
JP2014220637A
Publication Date:
October 24, 2018
Filing Date:
October 29, 2014
Export Citation:
Assignee:
株式会社ＳＯＫＥＮ
株式会社デンソー
国立大学法人 東京大学
株式会社デンソー
国立大学法人 東京大学
International Classes:
B64C27/28; B64C39/02; B64D27/24; B64D47/08
Domestic Patent References:
| JP1101297A | ||||
| JP2011162173A | ||||
| JP2010195293A | ||||
| JP2005206015A |
Foreign References:
| US20110001001 | ||||
| US20120083945 | ||||
| US20100044499 | ||||
| US20090283629 | ||||
| US5080304 | ||||
| US20110226892 | ||||
| US20020125367 | ||||
| CN102991672A | ||||
| US20040129827 | ||||
| CN203486139U |
Attorney, Agent or Firm:
Kazuyuki Yahagi
Taihei Nonobe
Takanori Kubo
Taihei Nonobe
Takanori Kubo