采用现场可编程门列阵设计arinc 429,MIL-STD - 1553B航空总线接口通信系统,实现总线设备之间的互联。
The ARINC429, MIL-STD-1553B and CAN avionics bus interface communication system based on Field Programmable Gate Array (FPGA) are designed, which links different bus instruments.
分析了网络协议测试仪的串行通信接口功能,设计了一种可编程多协议串行接口电路。
The function of serial communication port in protocol tester was analyzed and a programmable multi-protocol serial communication interface circuit was designed.
利用CPLD芯片的大容量、可编程特性,设计了具有缓存功能的高速异步串行通信接口芯片,以满足日益提高的快速串行通信要求。
Making use of large inner capacity and programmable resource of a CPLD chip, a high speed UART with buffer bas been designed to meet communication requirement.
介绍了新型通信控制器的硬件设计,着重描述了通信接口部分,用复杂可编程逻辑器件CPLD解决了CAN 控制器芯片SJA 1000与AT 91RM 9200之间的时序逻辑问题。
The hardware structure is introduced, emphatically the communication interface circuit. The time sequence logic problem between CAN controller chip SJA1000 and AT91RM9200 is solved using the CPLD.
介绍了新型通信控制器的硬件设计,着重描述了通信接口部分,用复杂可编程逻辑器件CPLD解决了CAN 控制器芯片SJA 1000与AT 91RM 9200之间的时序逻辑问题。
The hardware structure is introduced, emphatically the communication interface circuit. The time sequence logic problem between CAN controller chip SJA1000 and AT91RM9200 is solved using the CPLD.
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