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:
Jun. 27, 2023

Filed:

Dec. 12, 2018
Applicant:

Insitu, Inc., a Subsidiary of the Boeing Company, Bingen, WA (US);

Inventors:

David Harty, Husum, WA (US);

Douglas Allyn Miller, Sisters, OR (US);

Kenneth Hillen, Aloha, OR (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 11/07 (2006.01); G06F 9/455 (2018.01); H04L 9/40 (2022.01); B64C 39/02 (2023.01); B64U 101/00 (2023.01);
U.S. Cl.
CPC ...
G06F 11/0796 (2013.01); B64C 39/024 (2013.01); G06F 9/45558 (2013.01); G06F 11/0712 (2013.01); G06F 11/0739 (2013.01); H04L 63/02 (2013.01); B64U 2101/00 (2023.01); G06F 2009/45575 (2013.01); G06F 2009/45587 (2013.01);
Abstract

Apparatus and methods for controlling unmanned systems (UMSs), such as unmanned aircraft, are provided. A UMS can be provided that includes a physical computer, one or more auxiliary systems for the UMS, and a payload. The physical computer can execute software to cause the physical computer at least to instantiate a plurality of virtual computers that include a mission virtual computer and a payload virtual computer for: controlling the one or more auxiliary systems for the UMS using the mission virtual computer, communicating with the payload using the payload virtual computer, determining whether a software fault has occurred on one virtual computer of the plurality of virtual computers, and after determining that a software fault has occurred on one virtual computer of the plurality of virtual computers, preventing the software fault from causing a fault on a different virtual computer of the plurality of virtual computers.


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