The invention discloses an avionics function test system. The avionics function test system comprises a control module, a simulator, a simulator interface control module, a signal acquisition and simulation data structure management module and a redundant cloud data synchronous display control module. The output end of the control module is connected with the input end of the simulator, the output end of the simulator is connected with the input end of the simulator interface control module, and the output end of the simulator interface control module is connected with the input end of the signal acquisition and simulation data structure management module. And the output end of the signal acquisition and simulation data structure management module is connected with the input end of the redundant cloud data synchronous display control module and the receiving end of the control module. According to the avionics function test system provided by the invention, the development of a function test program and the experimental verification of the actual application situation of a simulator are realized, the automatic application situation is reproduced, and the reliability and the production efficiency of the function test automation test are improved.
本发明公开了一种航电功能试验测试系统,该航电功能试验测试系统包括:控制模块、模拟器、模拟器接口控制模块、信号采集和仿真数据结构管理模块和冗余云数据同步显控模块;控制模块的输出端与模拟器的输入端连接,模拟器的输出端与模拟器接口控制模块的输入端连接,模拟器接口控制模块的输出端与信号采集和仿真数据结构管理模块的输入端连接,信号采集和仿真数据结构管理模块的输出端与冗余云数据同步显控模块的输入端以及控制模块的接收端连接。本发明提供的航电功能试验测试系统,以实现对功能试验测试程序的开发以及模拟器的实际应用情况进行实验验证,复现自动化应用情景,提高功能试验自动化测试的可靠性和生产效率的效果。
Avionics function test system
一种航电功能试验测试系统
2021-05-21
Patent
Elektronische Ressource
Chinesisch
IPC: | 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 |
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