Invention Grant
US08744650B1 Aircraft control system 有权
飞机控制系统

Aircraft control system
Abstract:
A method and apparatus comprising a bus system and a plurality of control units connected to the bus system. The plurality of control units are each configured to control a same number of hardware systems in a vehicle, store a number of parameters used to control the number of hardware systems, and synchronize the number of parameter stored using the bus system in response to a change in the number of parameters at a selected control unit in the plurality of control units.
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