The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 02, 2018

Filed:

Oct. 28, 2015
Applicants:

Denso Corporation, Kariya, Aichi-pref., JP;

Nippon Soken, Inc., Nishio, Aichi-pref., JP;

The University of Tokyo, Tokyo, JP;

Inventors:

Takenori Matsue, Nishio, JP;

Koji Kawasaki, Nichio, JP;

Michihiro Matsuura, Nishio, JP;

Masami Kurosaka, Nishio, JP;

Masayuki Inaba, Tokyo, JP;

Assignees:

DENSO CORPORATION, Kariya, Aichi-pref., JP;

SOKEN, INC., Nisshin, Aichi-pref., JP;

THE UNIVERSITY OF TOKYO, Tokyo, Bunkyo-Ku, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/00 (2006.01); B64C 39/02 (2006.01); H04N 7/18 (2006.01); G05D 1/00 (2006.01); G05D 1/08 (2006.01);
U.S. Cl.
CPC ...
B64C 39/024 (2013.01); G05D 1/0094 (2013.01); G05D 1/0858 (2013.01); H04N 7/185 (2013.01); B64C 2201/027 (2013.01); B64C 2201/042 (2013.01); B64C 2201/127 (2013.01); B64C 2201/141 (2013.01);
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.


Find Patent Forward Citations

Loading…