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:
Mar. 05, 2019

Filed:

Dec. 02, 2016
Applicants:

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

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

Inventors:

Hiroki Ishii, Nishio, JP;

Koji Kawasaki, Nishio, JP;

Takenori Matsue, Nishio, JP;

Shinji Andou, Nishio, JP;

Hiroyasu Baba, Nishio, JP;

Assignees:

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

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05D 1/08 (2006.01); B64D 31/10 (2006.01); G07C 5/08 (2006.01); G05D 1/04 (2006.01); B64C 27/08 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
B64D 31/10 (2013.01); B64C 27/08 (2013.01); B64C 39/024 (2013.01); G05D 1/042 (2013.01); G05D 1/0816 (2013.01); G07C 5/0808 (2013.01); B64C 2201/024 (2013.01); B64C 2201/027 (2013.01); B64C 2201/108 (2013.01); B64C 2201/141 (2013.01);
Abstract

In an aerial vehicle, a malfunction determiner determines whether there is a malfunction in one of thrusters of the aerial vehicle. A flight controller activates the thrusters, and controls the output of each of the thrusters. The flight controller deactivates, when it is determined that there is a malfunction in one of the thrusters as a malfunctioned thruster, the malfunctioned thruster. The flight controller deactivates a selected thruster in the thrusters; the selected thruster being paired to the malfunctioned thruster, and controls the active thrusters except for the deactivated thrusters in all the thrusters to make the flight attitude of the aerial vehicle stable. The flight controller controls the active thrusters to cause the aerial vehicle to land while maintaining the flight attitude of the aerial vehicle being stable.


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