The invention discloses a dual-redundancy aircraft flight safety console and a control method. The dual-redundancy aircraft flight safety console comprises a safety control station module, a communication module, a safety console upper computer, a safety console lower computer and a power supply module, the safety control console upper computer and the safety control console lower computer are connected through a serial port RS422; the safety control console upper computer and the safety control console lower computer are respectively in communication connection with the communication module; the safety control station module is connected with the communication module; the power supply module is used for supplying power; according to the safety control console upper computer, the safety control console lower computer carries out heartbeat detection through an RS422 interface, and if the upper computer detects that the lower computer fails, instructions can be sent through an internet access of the upper computer.
本发明公开了一种双冗余飞行器飞行安全控制台及控制方法,包括安控站模块、通信模块、安控台上位机、安控台下位机、电源模块;所述的安控台上位机与安控台下位机之间通过串口RS422连接;所述的安控台上位机与安控台下位机分别与所述的通信模块通信连接;所述的安控站模块与所述的通信模块连接;所述的电源模块用于进行供电;所述的安控台上位机、安控台下位机通过RS422接口进行心跳检测,若上位机检测到下位机失效,则可以通过上位机的网口进行指令的发送。
Dual-redundancy aircraft flight safety console and control method
一种双冗余飞行器飞行安全控制台及控制方法
02.05.2023
Patent
Elektronische Ressource
Chinesisch
IPC: | G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Computer redundancy for aircraft flight control
Tema Archiv | 1977
|Computer redundancy for aircraft flight control
AIAA | 1977
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