本文对于利用FPGA芯片进行系统设计的研究人员具有一定的参考价值，也可以作为LONWORKS现场总线智能节点开发的参考资料。
The paper maybe value to those who ready to use FPGA chips in their designs or be reference for development of neuron node based on LONWORKS field-bus technology.
并对PCI总线在氡室检测系统中的具体硬件系统结构、控制芯片与驱动软件设计，与PCI总线对核谱转换的传输性能作了阐述。
And the specific hardware system structure, control slug and the design of drive software and the transmission performance of PCI bus for nuclear spectrometry were also set forth.
本论文的主要工作即着重于系统芯片中片上总线结构的性能评价研究，包括总线结构的建模、系统仿真环境的建立以及性能评价的方法。
This paper focuses on performance estimation of the embedded microprocessor based on the on-chip bus, including on-chip bus modeling, high-level simulation environment building and their combination.
基于USB总线接口芯片CH375，设计了机车信号记录仪数据记录系统，并详细阐述了CH375与TMS320F 2812之间的接口设计。
Based on the USB bus interface chip CH375, we design the locomotive signals data recording system, and detail the design of communication interface of CH375 and TMS320F2812.
文中介绍了一种具有通用性的基于CAN总线的智能测控单元的设计方法，阐述了系统各部分的硬件结构及相应的芯片功能。
This paper presents an all-purpose design for an intelligent measurement and control unit based on a CAN bus, and describes its hardware structure and chip functions.
介绍了基于CAN总线的卷绕式镀膜机蒸镀系统的设计方法，阐述了系统设计的硬件及其芯片选用并介绍了软件设计方法。
This article presents the design of an evaporator system for use with winding plating equipment based on CAN bus, including its hardware structure chip choice and the design of software.
提出了一种实时图像信息处理系统模块化可扩展的多总线结构，详细论述了其系统总线结构、DSP芯片选型及系统复位流程等系统实现中的关键问题。
Some Key points in system realization, such as the system bus structure, the selection of DSP chips and the process of system reset, were discussed in detail.
介绍了一种基于新型USB接口芯片CH372的CAN总线网络适配器系统的设计，提出了一种使用USB接口实现CAN总线网络与计算机连接的方案。
This paper introduces a design of a CAN bus adapter system based on a new type of USB chip CH372 for the communication of the CAN bus and the computer.
继而从芯片选型到电路设计详细论述了系统CPU模块、音视频、总线网络等主要功能部分的硬件设计。
Following the hardware design the main function of the system including CPU module, audio and video, the bus network, was discussed in detail from the chip selection to the circuit design.
分析了总线接口芯片选择原则和总线冲突解决方案，给出了系统实现的硬件接口电路和软件实现详细框图。
The selection principle of bus interface chip and solution of bus conflict are introduced, together with its concrete hardware circuits and software block chart are given.
介绍了基于RS-485总线的单片机多机通信系统，重点介绍了MAX-487芯片和通信系统的组成，并给出了流程图。
The essay introduces multi-chip calculator communication system based on RS-485 bus, especially MAX-487 chip and the components of the communication system and gives the flow diagram.
介绍了采用CPLD实现DSP芯片TMS320C6713和背板VME总线之间高速数据传输的系统设计方法。
The method of using CPLD to realize high speed datatrasmission between DSP chip TMS320C6713 and VMEbus onthe backboard is described.
利用CPLD芯片实现单片机与ISA总线接口之间的高速并行通信，给出系统的总体设计方法及程序框图。
The solution of high speed communication between MCU and ISA bus is designed based on Altera CPLD.
介绍了几种新型的视频转换芯片在机载计算机系统上的应用，主要包括PAL制视频和低电压差分信号(LVDS)视频总线设计。
This paper lays particular stress on new video chips for airborne application, mainly on PAL video and LVDS bus design.
电源优化的处理器系统总线始终处于断电状态，直到感知来自芯片组的数据才通电，从而减少处理器的耗电量。
The power-optimized processor system bus remains powered down until it senses incoming data form the chipset, allowing to the processor to consume less power.
该方案基于USB主/从控制芯片CH375A，在单片机的控制下，实现了CAN总线数据采集系统中嵌入USB主机，从而完成把各节点采集的数据存入U盘，取代了现场数据采集系统必须有一台计算机的模式。
The proposal based on USB Host/Slave controller chip CH375A, realized a USB-Host embedded in CAN bus data acquisition system and stored acquisition data of each node in U flash disk under MCU control.
实践表明，采用I2C总线技术，不仅使系统的芯片大大减少，系统的灵活性增强，而且提高了系统的抗干扰能力。
Practice shows not only the reduction in CMOS chips but also the improvement in agility and anti-interference ability of the system.
针对小型无人机控制系统对功耗、成本、可集成性等的较高要求，设计了一种基于DSP芯片TMS320F2812的总线式飞行控制系统。
A bus-structure flight control system using DSP as processor is designed, which aims at the demands of power, cost and integration from small Unmanned Aerial Vehicle(UAV).
针对小型无人机控制系统对功耗、成本、可集成性等的较高要求，设计了一种基于DSP芯片TMS320F2812的总线式飞行控制系统。
A bus-structure flight control system using DSP as processor is designed, which aims at the demands of power, cost and integration from small Unmanned Aerial Vehicle(UAV).
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