Invention Grant
- Patent Title: Asymmetric CAN-based communication for aerial vehicles
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Application No.: US15661974Application Date: 2017-07-27
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Publication No.: US10382225B2Publication Date: 2019-08-13
- Inventor: Parsa Dormiani , Brian Viele
- Applicant: Wing Aviation LLC
- Applicant Address: US CA Mountain View
- Assignee: Wing Aviation LLC
- Current Assignee: Wing Aviation LLC
- Current Assignee Address: US CA Mountain View
- Agency: McDonnell Boehnen Hulbert & Berghoff LLP
- Main IPC: H04L12/40
- IPC: H04L12/40 ; B64C39/02 ; B64C13/50 ; G05D1/00

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.
Public/Granted literature
- US20190036732A1 Asymmetric CAN-based Communication for Aerial Vehicles Public/Granted day:2019-01-31
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