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:
Oct. 05, 2021

Filed:

Aug. 30, 2018
Applicant:

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

Inventors:

Sebastian Robin Fischer, Seattle, WA (US);

David Friedman, Seattle, WA (US);

Marco Antonio De Barros Ceze, Seattle, WA (US);

Louis Leroi LeGrand, III, Seattle, WA (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/46 (2006.01); B64C 39/02 (2006.01); B64C 27/20 (2006.01); B64C 27/26 (2006.01); B64C 29/02 (2006.01); B64C 39/06 (2006.01); G05D 1/00 (2006.01); G05D 1/08 (2006.01); G05D 1/10 (2006.01);
U.S. Cl.
CPC ...
B64C 39/024 (2013.01); B64C 11/46 (2013.01); B64C 27/20 (2013.01); B64C 27/26 (2013.01); B64C 29/02 (2013.01); B64C 39/062 (2013.01); G05D 1/0055 (2013.01); G05D 1/0816 (2013.01); G05D 1/101 (2013.01); B64C 2201/028 (2013.01); B64C 2201/042 (2013.01); B64C 2201/104 (2013.01); B64C 2201/128 (2013.01); B64C 2201/165 (2013.01);
Abstract

Systems and methods to control aerial vehicles in degraded operational states are described. For example, for an aerial vehicle having six propulsion mechanisms arranged around a fuselage, one or more modified control schemes may be implemented to maintain control and navigation of the aerial vehicle responsive to a motor out situation, such as a failure of one propulsion mechanism. The modified control schemes may seek to emulate normal operation of a quadcopter, and/or may seek to utilize all remaining propulsion mechanisms to maintain controllability of the aerial vehicle in all six degrees of freedom of movement.


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