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:
Jul. 21, 2020

Filed:

Mar. 15, 2018
Applicant:

Ricoh Company, Ltd., Tokyo, JP;

Inventor:

Hideomi Sakuma, Kanagawa, JP;

Assignee:

RICOH COMPANY, LTD., Tokyo, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/02 (2006.01); B64C 11/46 (2006.01); B64C 39/02 (2006.01); G05D 1/08 (2006.01);
U.S. Cl.
CPC ...
B64C 29/02 (2013.01); B64C 11/46 (2013.01); B64C 39/024 (2013.01); G05D 1/0808 (2013.01); B64C 2201/021 (2013.01); B64C 2201/027 (2013.01); B64C 2201/042 (2013.01); B64C 2201/044 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01); B64C 2201/146 (2013.01); B64C 2201/165 (2013.01);
Abstract

An aircraft includes propellers at a center of the airframe; a first power source; a pitch adjuster to change pitch angles of the propellers; a plurality of attitude control propellers; a second power source lower in output than the first power source; and a control circuit to control attitude of the airframe. The control circuit includes a first yaw rotation generation control unit to control first yaw rotation generated by torques of the propellers with the pitch adjuster; and a second yaw rotation generation control unit to control a second yaw rotation generated by torques generated by a difference in rotation speed between the attitude control propellers. The control circuit is configured to control the first yaw rotation generation control unit and the second yaw rotation generation control unit in accordance with a magnitude of a command value of yaw rotation.


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