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:
Feb. 28, 2023

Filed:

Nov. 22, 2019
Applicant:

Futaba Corporation, Mobara, JP;

Inventor:

Masahiro Tanaka, Mobara, JP;

Assignee:

FUTABA CORPORATION, Mobara, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/08 (2006.01); B64C 39/02 (2023.01); B64C 27/12 (2006.01); G05D 1/00 (2006.01); B64C 27/57 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0816 (2013.01); B64C 27/12 (2013.01); B64C 27/57 (2013.01); B64C 39/024 (2013.01); G05D 1/0011 (2013.01); G05D 1/0858 (2013.01); B64C 2201/14 (2013.01);
Abstract

A driving control device for a remote controlled helicopter includes an rpm detection unit that detects an rpm of a main rotor, a gyro sensor that detects angular velocities of control axes including roll, pitch and yaw axes, and a control unit that generates a control signal of a control actuator for controlling movements of the control axes based on the angular velocities detected by the gyro sensor and a steering signal sent from a transmitter. The control unit has information on the gyro sensitivities of the control axes and information on a set rpm of the main rotor which are preset for each of the flight states of the remote controlled helicopter, and corrects the gyro sensitivities based on a difference between the set rpm corresponding to a selected flight state among the flight states and an rpm of the main rotor detected by the rpm detection unit.


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