摘要
以自行研制的PCI-A429芯片为例,讨论了内核设计以及系统集成中内核互连的问题。主要介绍了程控配置和自适应方式的两种ARINC429接收模块内核和PCI内核的设计。还分析了内核之间互连的多种控制接口和数据接口。
The approach of the IP-Core design and IP-Core interconnection in the integrated system are discussed with the example of the Chip PCI-A429 developed by CARERI in this paper. The design method of PCI IP-Core and the ARINC429 IP-Core nowadays widely used in the avionics system are proposed. Based on the interconnection between the ARINC429 IP-Core and PCI IP-Core, several control interfaces and data communication interfaces between IP-Cores are analyzed.
出处
《航空电子技术》
2006年第4期38-44,共7页
Avionics Technology
