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:
Jun. 18, 2024

Filed:

Mar. 04, 2020
Applicants:

Mitsubishi Electric Corporation, Tokyo, JP;

Japan Aerospace Exploration Agency, Tokyo, JP;

Inventors:

Kenji Fujiwara, Tokyo, JP;

Hisatoshi Fukumoto, Tokyo, JP;

Tomoki Takegami, Tokyo, JP;

Tetsuya Kojima, Tokyo, JP;

Akihiko Iwata, Tokyo, JP;

Masahiro Sugahara, Tokyo, JP;

Hiroshi Kobayashi, Tokyo, JP;

Mari Nishiyama, Tokyo, JP;

Akira Nishizawa, Tokyo, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02P 27/06 (2006.01); B60L 50/52 (2019.01); H02K 11/33 (2016.01); H02M 3/158 (2006.01); H02M 7/537 (2006.01);
U.S. Cl.
CPC ...
H02P 27/06 (2013.01); B60L 50/52 (2019.02); H02K 11/33 (2016.01); H02M 3/158 (2013.01); H02M 7/537 (2013.01); B60L 2200/10 (2013.01);
Abstract

A motor control device includes: a step-down device including a DC-output power conversion device having a first mode for outputting first voltage and a second mode for outputting second voltage lower than the first voltage; a power supply device; and a control device, and controls a motor. When a flying object takes off, the control device controls the power conversion device in the first mode. When the control device judges that flight information which is one or both of information of a motor parameter obtained along with control for the motor and information of an environmental factor relevant to the flight altitude of satisfies a predetermined condition, or when the control device has received an mode signal for which the second mode is selected on the basis of the flight information during control for the motor, the control device controls the power conversion device in the second mode.


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