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简易控制系统
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  simple control system
     Study and Analysis of the Simple Control System of a Rocket
     火箭弹简易控制系统分析
短句来源
     Analysis of the Simple Control System of a Multiple-launching Rocket
     多管火箭弹简易控制系统分析
短句来源
     Simple Control System Application with Inverter for Constant Pressure Water Supply
     变频恒压供水简易控制系统的应用
短句来源
     A simple control system with inverter for constant pressure water supply was introduced, this system without PLC controller was able to keep constant water pressure automatically to satisty requirements for water supply.
     介绍一种变频恒压供水简易控制系统,该系统可省去PLC控制器,简便易用,能自动保持水压恒定以满足供水要求。
短句来源
     The features of the simple control system adopted by some rocket weapon system are simply summarized. First the design idea and basis of system concept of a simple control rocket is analyzed.
     简单概述了目前火箭弹武器所采用的简易控制系统的特点 ,分析了火箭弹简易控制系统总体方案的设计思想及设计依据。
短句来源
  相似匹配句对
     Study and Analysis of the Simple Control System of a Rocket
     火箭弹简易控制系统分析
短句来源
     The Application of Simplicity-type DEH Control System
     简易式DEH控制系统的应用
短句来源
     Water Temperature Control System
     水温控制系统
短句来源
     The control system of stepping motor
     步进电机控制系统
短句来源
     The method is simple and easy.
     方法简易.
短句来源
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  simple control system
We report on the development of a simple control system which can handle multiple devices through an optical fibre data link.
      
We illustrate the benefit of our approach with a simple control system of two canal locks.
      
The non-emissive visual sensors and the simple control system developed here are suitable for use on MAVs with a permissible avionic payload of only a few grams.
      
The sufficiency theorem embodying these conditions generalizes those of Boltyanskii and Leitmann and is applied to a simple control system to which their sufficiency theorems are not applicable.
      
However, the system is inherently simple to control and will work well with a very simple control system.
      
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The features of the simple control system adopted by some rocket weapon system are simply summarized. First the design idea and basis of system concept of a simple control rocket is analyzed. Then the system plan, the features of attitude control system, the select principle of measurement element and actuating mechanism are detailed analyzed. Finally the design principle of the range correction system is simply analyzed.

简单概述了目前火箭弹武器所采用的简易控制系统的特点 ,分析了火箭弹简易控制系统总体方案的设计思想及设计依据。对姿态控制系统方案、系统特点以及姿态控制系统敏感元件及执行机构的选择依据进行了详细分析 ,最后对距离修正系统的设计依据进行了简要分析

Existing design methods for the stable loop of missile are, to our best knowledge, rather complicated. Our aim is to present a simplified design method. Section 2 summarizes Eqs. (2) and (3), Table 1 and Fig. 2 of the well-known standard coefficient metnod, which is simple and can serve as the starting point of our simplified design method. The key feature of our simplified design method is the introduction of a proper amplification coefficient ky=5 + 0. 0002 H, where H is the flight height. By means of ky we...

Existing design methods for the stable loop of missile are, to our best knowledge, rather complicated. Our aim is to present a simplified design method. Section 2 summarizes Eqs. (2) and (3), Table 1 and Fig. 2 of the well-known standard coefficient metnod, which is simple and can serve as the starting point of our simplified design method. The key feature of our simplified design method is the introduction of a proper amplification coefficient ky=5 + 0. 0002 H, where H is the flight height. By means of ky we can improve the performance of the acceleration stable loop adaptively. Simulation results, shown in Figs. 3 through 6, show preliminarily that our simplified adaptive design method is indeed simple and practical.

给出一种简易的控制系统设计方法——标准系数法,它能够根据特征多项式方便地确定校正环节的设计参数。通过在加速度回路引入与高度成比例的放大系数,可以自适应地调节导弹稳定回路性能。研究和仿真结果表明这种方法是简单和实用的。

Existed design methods for the roll stablized loop of missile are, to our best knowledge, rather complicated. Our aim is to present a simplified design method. A mathematic model for the roll stablized loop of missile is established. The main concepts of the well known standard coefficient method is summarized, which is simple and can serve as the starting point of our simplified design method. The key feature of our simplified design method is the introduction of a proper amplification coefficient inversely...

Existed design methods for the roll stablized loop of missile are, to our best knowledge, rather complicated. Our aim is to present a simplified design method. A mathematic model for the roll stablized loop of missile is established. The main concepts of the well known standard coefficient method is summarized, which is simple and can serve as the starting point of our simplified design method. The key feature of our simplified design method is the introduction of a proper amplification coefficient inversely proportional to the dynamic pressure, which can improve the performance of the roll stablized loop adaptively. Simulation results show that our simplified adaptive design method is indeed simple and practical.

由于导弹在不同高度变速飞行 ,导弹控制系统是一个时变的非最小相位系统 ,因此导弹控制系统设计是比较复杂的。经典的设计方法一般应用频率响应法、根轨迹法或时域法 ,在初步设计时这些方法还是比较复杂的。采用现代的自适应控制方法也比较复杂。这里给出一种简易的控制系统设计方法——标准系数法 ,这种方法能够根据闭环系统的特征多项式迅速确定校正环节的设计参数 ,通过在反馈回路中引入与动压成反比的放大系数来自适应调节导弹滚动稳定回路性能。研究结果表明这种方法是简单和实用的。

 
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