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:
Aug. 30, 2016

Filed:

Dec. 20, 2013
Applicant:

Google Inc., Mountain View, CA (US);

Inventors:

Erik Christopher Chubb, San Francisco, CA (US);

Damon Vander Lind, Alameda, CA (US);

Brian Hachtmann, San Martin, CA (US);

Assignee:

Google Inc., Mountain View, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05D 1/08 (2006.01); B64C 17/00 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0816 (2013.01); B64C 17/00 (2013.01); B64C 39/022 (2013.01); B64C 39/024 (2013.01); G05D 1/0866 (2013.01); B64C 2201/021 (2013.01); B64C 2201/042 (2013.01);
Abstract

An example method may include receiving data representing an initial position and an initial attitude of an aircraft. The method further includes determining a change to a first attribute and a second attribute of the position or the attitude of the aircraft to achieve a subsequent position and a subsequent attitude. The method also includes determining a priority sequence for changing the first attribute and the second attribute of the position or the attitude of the aircraft based on a first thrust of the actuator to achieve the change to the first attribute and a second thrust of the actuator to achieve the change to the second attribute. The priority sequence is configured to cause changes to the first attribute before causing changes to the second attribute where the actuator is unable to concurrently provide the first thrust and the second thrust.


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