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  1. 60-113

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  2. TI网站上的各种电机控制策略的集合,英文的文档-Various collections of motor control strategies on the TI website
  3. 所属分类:Project Design

    • 发布日期:2017-05-11
    • 文件大小:2.24mb
    • 提供者:张新
  1. system-clock

    0下载:
  2. 一本关于系统时钟的书籍,windows基础知识,初学者可参考-A book on the system clock, windows basics, beginners can refer
  3. 所属分类:software engineering

    • 发布日期:2017-05-19
    • 文件大小:5.3mb
    • 提供者:杜先生
  1. PBOC2.0

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  2. PBOC2.0全套技术资料,目前最新版为3.0,但差别不大,是掌握PBOC的必备资料-PBOC2.0 full technical information, the latest version is 3.0, but the difference is not big, is to master the PBOC essential information
  3. 所属分类:software engineering

    • 发布日期:2017-05-25
    • 文件大小:7.5mb
    • 提供者:dinny
  1. CBuilder-K3BOS

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  2. 用C++Builder写K3BOS单据插件-Written with C++ Builder plugin K3BOS documents
  3. 所属分类:software engineering

    • 发布日期:2017-05-01
    • 文件大小:618.13kb
    • 提供者:yetendi
  1. TRAFFIC-LIGHT-CONTROL

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  2. 交通灯控制器 output R1,R2 //--红灯输出 output Y1,Y2 //--黄灯输出 output G1,G2 //--绿灯输出-traffic light control
  3. 所属分类:software engineering

    • 发布日期:2017-04-10
    • 文件大小:1.08kb
    • 提供者:mechael
  1. TaxBilling

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  2. 出租车计费器,七段码管显示输出,里程小于1Km是显示基价-tax billing
  3. 所属分类:software engineering

    • 发布日期:2017-04-10
    • 文件大小:1.05kb
    • 提供者:mechael
  1. Blind-Sources-Separation-code

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  2. Blind Sources Separation code
  3. 所属分类:software engineering

    • 发布日期:2017-04-09
    • 文件大小:8.87kb
    • 提供者:err
  1. danpianji

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  2. 关于自己单片机学习的总结程序,希望对大家有用-MCU learning about their summary procedures, we hope to be useful
  3. 所属分类:software engineering

    • 发布日期:2017-04-17
    • 文件大小:453.71kb
    • 提供者:赵文栋
  1. missile

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  2. In this paper, formation control ideas for multiple spacecraft using the virtual structure approach are presented. If there is no formation feedback from the spacecraft to the virtual structure, the spacecraft will get out of formation when the v
  3. 所属分类:Project Design

    • 发布日期:2017-04-04
    • 文件大小:307.44kb
    • 提供者:alkatel
  1. spascraft

    0下载:
  2. In this paper, formation control ideas for multiple spacecraft using the virtual structure approach are presented. If there is no formation feedback from the spacecraft to the virtual structure, the spacecraft will get out of formation when the v
  3. 所属分类:Project Design

    • 发布日期:2017-05-06
    • 文件大小:1.19mb
    • 提供者:alkatel
  1. coorsinat

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  2. The success of a guided missile is dependent on certain factors. The most significant error sources affecting the success of a guided missile are the initial heading error of the missile and the target maneuvers. Apart from these, the dynamic
  3. 所属分类:Project Design

    • 发布日期:2017-04-03
    • 文件大小:914.42kb
    • 提供者:alkatel
  1. ballis

    0下载:
  2. A method for the determination of the trajectory of a ballistic missile over a rotating, spherical Earth given only the launch position and impact point has been developed. The iterative solution presented uses a state transition matrix to correc
  3. 所属分类:Project Design

    • 发布日期:2017-04-10
    • 文件大小:1.87mb
    • 提供者:alkatel
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