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:
Feb. 01, 2022

Filed:

Jul. 09, 2019
Applicant:

Wing Aviation Llc, Mountain View, CA (US);

Inventors:

Parsa Dormiani, Mountain View, CA (US);

Brian Viele, Mountain View, CA (US);

Assignee:

Wing Aviation LLC, Mountain View, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); B64C 13/50 (2006.01); H04L 12/40 (2006.01); B64C 39/04 (2006.01); B64C 29/02 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
H04L 12/40195 (2013.01); B64C 13/503 (2013.01); B64C 13/505 (2018.01); B64C 29/02 (2013.01); B64C 39/024 (2013.01); B64C 39/04 (2013.01); G05D 1/0077 (2013.01); B64C 2201/027 (2013.01); B64C 2201/088 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01); B64C 2201/141 (2013.01); H04L 12/40176 (2013.01); H04L 2012/4028 (2013.01); H04L 2012/40215 (2013.01); H04L 2012/40267 (2013.01);
Abstract

An example embodiment includes a plurality of flight modules including a primary flight module and a secondary flight module. The embodiment includes a CAN controller, a second CAN controller, a first CAN bus configured to transmit primary control signals from the first CAN controller to the primary flight module and to the secondary flight module, and a second CAN bus configured to transmit secondary control signals from the second CAN controller to the primary flight module and the secondary flight module. The primary flight module is configured to perform functions responsive to receiving the primary control signals, and not in response to receiving the secondary control signals and the secondary flight module is configured to perform functions responsive to receiving the secondary control signals, and not in response to receiving the primary control signals.


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