系统总线

将有一个持久的系统总线（systembus），它在引导时就会启动。

There will be a persistent system bus , which is started at boot time .

有色Petri网在车辆综电系统总线建模中的应用

Application of Colored Petri Nets to Modeling of Vehicle of Vetronics Integration System Bus

MARKⅣ控制系统总线介绍

Introduction to MARK ⅳ Control System Buses

基于FPGA的多功能信号源系统总线设计与实现

Design and Realization of the Bus in Multifunctional Signal Source System Based on FPGA

本文详细研究了这种分离事务流水执行技术并应用该技术实现了X处理器系统总线部件。

We study the split transaction pipelining technology in detail , and apply it to the implementation of system bus component in X processor .

各采集通道把采集数据存入各自缓存，由CPU通过系统总线处理。

Collecting channels stored the collected data into their respective caches , which were disposed by CPU through system bus .

SCA系统总线由SCA运行时用于与SCA组件和SCA模块之间的异步通信。

The SCA System Bus is used by the SCA runtime for asynchronous communication between SCA components and SCA modules .

基于MIPS核的片上系统总线控制器设计

A Bus Controller of the System on Chip Based on MIPS Core

系统总线将CPU与主存连接在一起并且和连接CPU与系统硬件外设的总线隔离开。

The system bus connects the CPU with the main memory and is separate from the buses connecting the CPU with the system 's hardware peripherals .

执行异步消息中间件可以称为软件系统总线系统（SSB）。

Perform asynchronous messaging middleware can be called Soft System Bus ( SSB ) .

此卡采用ISA系统总线作为PC机接口电路。功能完善，使用方便。

The intelligent card adopts ISA bus to interface with the industrial PC and is easy in use with complete functions .

以1553B总线控制器为例，采用SOC设计方法，研究了航天器系统总线的设计和实现。

The SOC design and implementation of the spacecraft system bus was studied , for example of the 1553B bus controller .

CLB总线是一种片上系统总线，一般用来连接高速度、高数据宽度的IP。

The CLB bus is a kind of on-chip system bus which is usually used to connect IPs with high speed and high data width .

当WebSphereJDBCAdapter向SCA系统总线中的队列交付事件时，由于意外因素而可能无法将事件交付给事件接收者。

When WebSphere JDBC Adapter delivers events to the queue in the SCA system bus , it is possible that events fail to be delivered to the recipient of events due to unexpected factors .

在方案描述中，首先给出了验证平台的总体框架，然后逐一介绍了平台的CPU&SEP3203微处理器、核心板硬件设计、FPGA板硬件设计、系统总线设计和电源系统设计，最后给出了平台的实物图。

In the description of the scheme , the general framework of the scheme is shown first , then CPU & SEP3203 , the core board hardware design , FPGA board hardware design , the system bus design and the system of power is specified one by one .

将该模式更改为正确的模式（在本例中，它是MESCASYS，因为该模式是您为SCA系统总线创建的模式）。

Change the schema to the correct schema ( in this case , it is MESCASYS , because that 's the schema you created for the SCA system bus ) .

该方案采用PowerPCG4处理器进行运算，采用VME作为系统总线，RACE++作为高速数据通道，具有稳定、计算能力强、可灵活配置等优点。

By the adoption of PowerPC G4 as DSP , VME as system bus and RACE + + as high speed data exchange path , this stable system has great performance and flexible expansibility .

通过对两种不同方案的实验结果数据进行对比，进一步得出锁读写是造成MPSOC系统总线繁忙率增加的主要原因的结论。

Through the comparison and analysis of the result data which is generated by the above experiments , the further conclusion that lock reading is the main cause of bus busy increasing is got .

几种常用测试系统总线的特点及应用

Compared with several data acquisition system bus peculiarity and its applications

GB/T14241-1993信息处理处理机系统总线接口（欧洲总线A）

Information processing & Processor system bus interface ( Eurobus A )

内部系统总线采用并行单总线结构；

Parallel single-bus architecture is adopted in internal system bus design .

比较分析了当前主要几种测控系统总线技术。

This paper analyzes several kinds technology of measure-control system bus .

航电综合化系统总线接口板研究设计

Design of Bus Interface Board to the Integrated Avionics System

火箭控制系统总线传输技术研究

Research on the Data Bus Transmit Technology for the Rocket Control System

测控系统总线综述

The Summary of the Measurement and Control System Buses

新一代火箭控制系统总线应用技术研究

Research on Bus Application Technique in Control System of New Generation Launch Vehicle

实时嵌入式系统总线的容错技术

Bus Fault Tolerant Technology for Real Time Embedded Systems

测控系统总线技术的现状与分析

The Analysis and Actuality of Measure-control System Bus Technology

小卫星星务计算机系统总线的研究与实现

Development and Implementation of communication bus on small satellites ' house keeping computer

飞机分布式配电系统总线监控器的设计

Design of Bus Monitor in Aircraft Distributed Power System