A flight control system for an aircraft includes a flight control computer system connected to a plurality of bus nodes via an electronic or optoelectronic bus system, the plurality of bus nodes are each configured to perform at least one of controlling an associated aircraft device based on a command message received from the flight control computer system via the bus system and sending an information message to the flight control computer system via the bus system. According to one aspect of the invention, the electronic or optoelectronic bus system is a redundant electronic or optoelectronic bus system comprising a plurality of independent bus subsystems, each bus node being configured to communicate with a flight control computer system via two different subsystems of the plurality of independent bus subsystems, each bus node is further configured to communicate with the flight control computer system via a first of the respective two different bus subsystems based on the associated predetermined bus communication protocol and via a second of the respective two different bus subsystems based on the associated predetermined bus communication protocol.

    用于飞行器的飞行控制系统包括经电子或光电总线系统与多个总线节点连接的飞行控制计算机系统,多个总线节点各自配置为执行基于经总线系统从飞行控制计算机系统接收的命令消息控制相关联飞行器装置以及经总线系统将信息消息发送至飞行控制计算机系统中的至少一个。根据本发明一个方面,电子或光电总线系统是包括多个独立总线子系统的冗余电子或光电总线系统,每个总线节点配置为经多个独立总线子系统中的两个不同子系统与飞行控制计算机系统通信,每个总线节点还配置为基于相关联预定总线通信协议经相应两个不同总线子系统中的第一总线子系统并基于相关联预定总线通信协议经相应两个不同总线子系统中的第二总线子系统与飞行控制计算机系统通信。


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    Titel :

    Fault-tolerant aircraft flight control system and aircraft preferably having such aircraft flight control system


    Weitere Titelangaben:

    容错飞行器飞行控制系统和优选具有此类飞行器飞行控制系统的飞行器


    Beteiligte:

    Erscheinungsdatum :

    2022-08-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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