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. 31, 2020

Filed:

Sep. 29, 2017
Applicant:

Disney Enterprises, Inc., Burbank, CA (US);

Inventors:

Gunter D. Niemeyer, Pasadena, CA (US);

Morgan T. Pope, Burbank, CA (US);

Assignee:

DISNEY ENTERPRISES, INC., Burbank, CA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/08 (2006.01); B25J 13/08 (2006.01); B64C 17/02 (2006.01); B25J 9/16 (2006.01); B25J 11/00 (2006.01); B25J 19/00 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0808 (2013.01); B25J 9/1607 (2013.01); B25J 9/1615 (2013.01); B25J 11/003 (2013.01); B25J 11/0035 (2013.01); B25J 13/08 (2013.01); B25J 13/089 (2013.01); B25J 19/0008 (2013.01); B64C 17/02 (2013.01); B25J 13/086 (2013.01);
Abstract

A robot configured to provide accurate control over the rate of spin or rotation of the robot. To control the rate of spin, the robot includes an inertia shifting (or moving) assembly positioned within the robot's body so that the robot can land on a surface with a target orientation and 'stick the landing' of a gymnastic maneuver. The inertia shifting assembly includes sensors that allow the distance from the landing surface (or height) to be determined and that allow other parameters useful in controlling the robot to be calculated such as present orientation. In one embodiment, the sensors include an inertial measurement unit (IMU) and a laser range finder, and a controller processes their outputs to estimate orientation and angular velocity. The controller selects the right point of the flight to operate a drive mechanism in the inertia shifting assembly to achieve a targeted orientation.


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