In this paper,a design scheme of FC Interface Module in Avionic Environment is presented including CamLink interface video information transmission,the CAN interface state data information and FC interface state data information respectively based on the system frame.Test results and real-world applications show that the performance of the FC Interface Module meets the system requirements.%介绍了一种机载FC接口模块的设计与测试方案,结合该模块的系统框架,分别阐述了CamLink接口图像视频信息传输、CAN接口和FC接口状态数据信息传输等方面控制流程的设计.测试结果和工程应用表明,接口模块各项指标均满足系统要求.
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