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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.

Patent No.:

US 10845824 B1

PDFFull Text
Date of Patent:
Nov. 24, 2020

Filed:

Aug. 21, 2018

Supplemental attitude with engaged and disengaged input device modes

Applicant:

Kitty Hawk Corporation, Mountain View, CA (US);

Inventors:

Alexander David Selwa, Mountain View, CA (US);

Mark Johnson Cutler, Sunnyvale, CA (US);

Assignee:

Kitty Hawk Corporation, Palo Alto, CA (US);

Attorney:

Van Pelt, Yi & James LLP

Primary Examiner:

Nga X Nguyen

Int. Cl.
CPC ...
G05D 1/08 (2006.01); B64C 17/00 (2006.01); B64C 19/00 (2006.01); B64C 29/00 (2006.01); B64C 15/02 (2006.01); B64C 13/18 (2006.01); B64C 27/20 (2006.01); B64C 27/57 (2006.01); G05D 1/00 (2006.01); B64C 13/04 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0816 (2013.01); B64C 13/0421 (2018.01); B64C 13/18 (2013.01); B64C 15/02 (2013.01); B64C 17/00 (2013.01); B64C 19/00 (2013.01); B64C 27/20 (2013.01); B64C 27/57 (2013.01); B64C 29/0091 (2013.01); G05D 1/0011 (2013.01); G05D 1/0858 (2013.01); B64C 2201/146 (2013.01);
Abstract

An input attitude associated with an input device of an aircraft is received. A supplemental attitude is generated, including by selecting a position-based supplemental attitude to be the supplemental attitude in the event the input device is in a disengaged state and selecting a velocity-based supplemental attitude to be the supplemental attitude in the event the input device is in an engaged state. The input attitude and the supplemental attitude are combined in order to obtain a combined attitude. The aircraft is controlled using the combined attitude.

Find Patent Forward Citations

Selwa, Alexander. (2020). Supplemental attitude with engaged and disengaged input device modes (U.S. Patent No. 10845824). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10845824

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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