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:
May. 02, 2023

Filed:

Dec. 13, 2017
Applicant:

Acsl Ltd., Tokyo, JP;

Inventors:

Kenzo Nonami, Chiba, JP;

Yi Yang, Chiba, JP;

Assignee:

ACSL Ltd., Tokyo, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05D 1/08 (2006.01); B64C 39/02 (2023.01); G05D 1/00 (2006.01); G06F 17/16 (2006.01); B64U 10/10 (2023.01); B64U 30/20 (2023.01); B64U 101/00 (2023.01);
U.S. Cl.
CPC ...
G05D 1/0808 (2013.01); B64C 39/024 (2013.01); G05D 1/0022 (2013.01); G06F 17/16 (2013.01); B64U 10/10 (2023.01); B64U 30/20 (2023.01); B64U 2101/00 (2023.01); B64U 2201/20 (2023.01);
Abstract

[Problem to be Solved] The object is to provide a device, a method and the like which, when a fault occurs, particularly when a fault occurs in an operation of some of rotary wings, can control a flight depending on the fault, or which can be at least used for control when a fault occurs, or which can detect the fault. [Solution] A control device for unmanned aircraft comprising: a rotary-wing control signal generation circuit for generating a rotary wing control signal for causing a driving device to drive a plurality of rotary wings for flying the unmanned aircraft; a measuring device for measuring a physical amount relating to an operation of at least one of the plurality of rotary wings; and a fault detection circuit for detecting a fault in the operation of at least one of the plurality of rotary wings by using the physical amount measured by the measuring device, wherein the rotary-wing control signal generation circuit is configured to generate a rotary wing control signal depending on the fault detected by the fault detection circuit in the operation of at least one of the plurality of rotary wings, is provided.


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