• Figure 3 Typical SOA implementation with a data bus.

    图3有数据总线的典型SOA实现。

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  • As a result data bus is typically implemented using integration layer (Figure 1).

    结果是,数据总线一般由集成层(图1)实现。

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  • Which the data bus SDA is a bidirectional pin used for input or output data.

    其中数据总线sda是一个双向引脚,用于输入或输出数据。

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  • Another alternative is to directly connect the converter to the processor's data bus.

    另一种选择是直接将转换器与处理器的数据总线相连。

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  • High speed data bus is the key technology in avionics integration for advanced fighters.

    高速数据总线是先进军机航空电子综合化的关键支撑技术。

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  • This paper introduces an intelligent data bus fire alarm system by microcomputer control.

    介绍了由微型计算机控制的应用智能型数据总线的智能防火系统。

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  • The test architecture reusing data bus as TAM can reduce the silicon area cost for DFT greatly.

    复用数据总线作为测试传输机构的测试结构可以大大减小可测性设计的面积开销。

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  • We complete the design of crossbar switch with 6 ports and 32 bits data bus on one chip of FPGA.

    我们在单片FPGA中完成了6个端口、32位数据总线宽度交叉开关的设计。

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  • The main functions of the platform are enterprise information portal, enterprise data bus and CRM.

    主要功能包括:企业信息门户、企业数据总线和客户关系管理平台。

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  • MAI, which manages all the control status registers, exchange data with MCU through 8-bit data bus.

    MAI管理设备控制器内的所有状态寄存器,并且通过8位并行数据线与设备端mcu进行数据交换。

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  • The data bus must go into a high-impedance state at least one cycle before output of the latest data.

    在这种切换中,读出的数据有效前,数据总线至少需要有一个时钟的高阻状态。

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  • In this paper, the HJ-90 data bus protocol for shipboard distributed control system will be introduced.

    本文介绍舰载实时分布式系统的总线控制协议,即HJ- 90总线协议。

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  • Now there are some data bus standards, among them the most widely used are the CAN bus and the J1850 bus.

    目前,现行的汽车总线标准很多,其中使用也比较广泛的有CAN总线、J1850等。

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  • To get data and instructions moving among the various components of system, the computer needs a data bus.

    为了让数据和指令放到系统的各个部分里面,计算机需要一个数据总线。

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  • Port 0 is also the multiplexed low-order address and data bus during access to external program and data memory.

    端口0也是复低位地址和在利用外部程序和数据存储器的数据总线。

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  • Other avionics include the 1553b MILSTD data bus, XPS-2 head-up display (HUD), and multifunctional displays (MFD).

    其它的航空电子设备包括1553BMILSTD数据链,XPS - 2平显(HUD)和多功能显示器(MFD)。

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  • The bus is the computer parts connected by a bunch of public signal, address bus, data bus and control bus composition.

    总线是连接计算机各部件的一簇公共信号线,由地址总线、数据总线和控制总线组成。

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  • Besides, the paper also improves a serial communication protocol based on RS-485 data bus, and realizes the application.

    此外,本文还改善了基于RS- 485总线的串口通信协议,并实现了这种协议的应用程序。

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  • To a micro-controller, the PDIUSBD12 appears as a memory device 8-bit data bus and 1 address bit (occupying 2 locations).

    对微控制器而言,PDIUSBD12看起来就像一个带8位数据总线和一个地址位(占用两个位置)的存储器件。

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  • Advanced aircraft power system and its control system was introduced and fault tolerant design of data bus was discussed.

    介绍了先进飞机供电系统及其控制系统的组成,并对数据通信总线的容错设计进行论述。

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  • The increased data bus width enables support for addressable memory space above the 4gb generally available on 32bit architectures.

    增加的数据总线带宽实现了对32位架构上通常可用的4gb以上可寻址内存空间的支持。

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  • The purpose is optimizing bus transmission system by the analysis of integrated avionics system data bus capability parameter.

    通过对综合航电系统数据总线的性能指标分析,以达到优化总线传输系统的目的。

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  • The hardware and software interface between 4-bit data bus dot matrix LCD and 80c31 microprocessor is described in this paper.

    文中论述4位数据总线点阵式液晶显示器LCD与低功耗单片微处理器80c31的硬件、软件接口方法和应用实例。

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  • The composition, function, use , software design and key technology of MIL-STD-1553B data bus integration test system are described.

    阐述了MIL-STD-1553B总线综合测试系统的组成、功能、用途、软件设计和关键技术问题。

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  • Input data appearing on the data bus, is written to the memory array subject to the DM input logic level appearing coincident with the data.

    数据总线上的输入数据是否写入存储器,取决于此时的DM的输入逻辑。

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  • In this paper, a new kind of data bus ARINC 629 is presented, and an ARINC629 bus communicating system is developed for avionics system test.

    本文研究了一种新型航空数据通信总线arinc 629以及应用于该总线机载电子设备测试的总线数据收发装置。

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  • Architecture of data bus is the "nerve center" for the avionics system, which has direct influence on the performance of avionics integration.

    航空电子总线系统结构是航空电子系统的神经中枢,直接决定着航空电子综合化程度的高低和性能的优劣。

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  • Function requirement of existing mobile robot control system is analyzed. Framework and realization mechanism of data bus pattern is described.

    分析了已有移动机器人平台控制系统的功能需求,阐述了总线模式的结构及实现机制。

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  • Function requirement of existing mobile robot control system is analyzed. Framework and realization mechanism of data bus pattern is described.

    分析了已有移动机器人平台控制系统的功能需求,阐述了总线模式的结构及实现机制。

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