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:
Jul. 05, 2022

Filed:

Dec. 02, 2019
Applicant:

Aurora Flight Sciences Corporation, Manassas, VA (US);

Inventors:

William Bosworth, Somerville, MA (US);

Devin Richard Jensen, Cambridge, MA (US);

Margaret Reagan, Cambridge, MA (US);

Assignee:
Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G01L 5/22 (2006.01); G01L 5/00 (2006.01); G05D 1/10 (2006.01); G05D 1/08 (2006.01); B64D 43/00 (2006.01); B64C 13/08 (2006.01); G01C 21/00 (2006.01); G05D 1/00 (2006.01); B25J 11/00 (2006.01); G06V 10/10 (2022.01); G06V 10/147 (2022.01); G06V 10/75 (2022.01); G06V 20/59 (2022.01); G06F 3/0488 (2022.01); G06F 3/02 (2006.01); G06F 3/0483 (2013.01); G06F 3/04817 (2022.01);
U.S. Cl.
CPC ...
G05D 1/106 (2019.05); B25J 11/00 (2013.01); B64C 13/08 (2013.01); B64D 43/00 (2013.01); G01C 21/00 (2013.01); G01L 5/0028 (2013.01); G01L 5/0061 (2013.01); G05D 1/0088 (2013.01); G05D 1/0808 (2013.01); G05D 1/101 (2013.01); G06V 10/10 (2022.01); G06V 10/147 (2022.01); G06V 10/751 (2022.01); G06V 20/59 (2022.01); G01L 5/00 (2013.01); G06F 3/02 (2013.01); G06F 3/0483 (2013.01); G06F 3/0488 (2013.01); G06F 3/04817 (2013.01);
Abstract

An aircrew automation system may comprise an actuation system and a computer system having a processor and one or more interfaces. The computer system can be communicatively coupled with a flight control system of an aircraft and configured to generate control commands based at least in part on flight situation data. The actuation system is operatively coupled with the computer system and comprises a robotic arm, a force sensor, and a controller. The robotic arm can be configured to engage a cockpit instrument among a plurality of cockpit instruments. The force sensor is operably coupled to the robotic arm and configured to measure a force when the robotic arm makes contact with the cockpit instrument. The controller is operably coupled with the robotic arm and the force sensor.


Find Patent Forward Citations

Loading…