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:
Jan. 05, 2021

Filed:

Jan. 26, 2018
Applicant:

Amazon Technologies, Inc., Seattle, WA (US);

Inventors:

Ben Thompson Ludington, Sammamish, WA (US);

Carlos Guillermo Parodi, Issaquah, WA (US);

Assignee:

Amazon Technologies, Inc., Seattle, WA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 25/00 (2006.01); G01C 19/5783 (2012.01); G01C 23/00 (2006.01); B64F 5/60 (2017.01); G01P 15/08 (2006.01); G01P 21/00 (2006.01); G01P 15/18 (2013.01);
U.S. Cl.
CPC ...
G01C 25/00 (2013.01); B64F 5/60 (2017.01); G01C 19/5783 (2013.01); G01C 23/00 (2013.01); G01P 15/0802 (2013.01); G01P 15/18 (2013.01); G01P 21/00 (2013.01);
Abstract

Where a body includes one or more inertial motion sensors, such as gyroscopes or accelerometers, the body's response to inertial motion may be simulated by actually imparting inertial motion to the sensors, and interpreting signals received from such sensors in response to the inertial motion. Gyroscopes or accelerometers of an aerial vehicle may be physically removed therefrom and remain in communication with an inertial navigation system, and rotated by one or more motors or motorized components to simulate angular velocities on the gyroscopes or accelerations on the accelerometers. Signals received by the inertial navigation system from the gyroscopes or the accelerometers may be evaluated to confirm the operability of the gyroscopes and accelerometers, the responsiveness of the inertial navigation system to sensed inertial motion or events associated with such inertial motion, or any other aspect of the aerial vehicle.


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