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missile
相关语句
  导弹
    Analysis of Missile Control System Stability with Monte Carlo Method
    用蒙特卡罗法分析导弹控制系统稳定性
短句来源
    A PRELIMINARY INVESTIGATION OF THE BASIC VERSION OF MISSILE GROUND TEST SYSTEM
    导弹地面测试系统基本型的初探
短句来源
    Design of the Robust Optimal Control System for a BTT Missile
    BTT导弹鲁棒最优控制系统的设计
短句来源
    Software System of Computerized Parameter Measuring Instrument of Missile Control Cabin
    导弹控制舱参数微机化测试仪软件系统
短句来源
    GENERALIZED PREDICTIVE ADAPTIVE CONTROLLER APPLIED TO A MISSILE CONTROL SYSTEM
    广义预测自适应控制器在导弹控制系统设计中应用
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  “missile”译为未确定词的双语例句
    A Research for Homing Missile Variable structure Autopilots
    战术导弹变结构自适变自动驾驶仪研究
短句来源
    In accordance with the characteristics of image sequence obtained by the imaging seeker of air-to-air missile,a passive ranging algorithm based on infrared image sequence is proposed.
    根据红外成像导引头截取时序红外图像的特点,提出了一种跟踪红外运动图像序列中目标的稳定特征点,利用成像所得特征部分尺寸得到距离信息的被动测距方法。
短句来源
    A Fault Diagnosis Expert System for Air-to-Air Missile Tester
    某型空空导弹测试仪故障诊断专家系统
短句来源
    Design of Some New Type Land-air Missile Launch Servo Control System
    某型地空导弹发射伺服控制系统设计
短句来源
    Electromagnetic Leakage from Image Monitor System for Missile Position and Its Protection
    阵地图像监视系统的电磁泄漏及防护
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  missile
On the development of future missile complexes for strategic nuclear forces
      
Possibilities of defense from a missile attacking from the back hemisphere by a vertical maneuver
      
The possibilities to defend an aircraft attacked from the back hemisphere by an air-air missile are investigated.
      
A model problem of determining an optimal vertical maneuver of the aircraft evading a missile that moves in the exponential atmosphere according to a given law of approach subject to aerodynamic drag forces and the Earth's gravitation is studied.
      
With a delay caused by the fact that the missile-flight time is finite, these distributions contain passive zones (i.e., time intervals where shooting makes no sense).
      
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The position system which uses an inductosyn as a transducer can measure the angle and the length very accurately. Combining it with the computer constitutes the digital servo system with high precision. This instrument has been broadly used in astronomical navigation, missile controlling, satellite tracking, radar, disk storage, and almost all kinds of precision machine tools. If the position system works in static mode, the position error of the transducer will affect the positioning precision. However,...

The position system which uses an inductosyn as a transducer can measure the angle and the length very accurately. Combining it with the computer constitutes the digital servo system with high precision. This instrument has been broadly used in astronomical navigation, missile controlling, satellite tracking, radar, disk storage, and almost all kinds of precision machine tools. If the position system works in static mode, the position error of the transducer will affect the positioning precision. However, once the inductosyn has been made, its position error is fixed, hence we can test its characteristic. In this paper, the inductosyn's positional error is analysed, and from which the mathematical model describing the positional error is formed. The computer can automatically correct the positional error through its error characteristic, so that the system's precision of the static positioning will be improved. This is performed by software. "The program for correcting the positional error" written in ALGOL-60 is presented. Because the method is applicable, in principle, to the multipolar rotary transformer, it will be able to make higher precision position system by use of lower precision transducer.When the position system works in dynamic mode (e. g. to measure the antenna's azimuth), as soon as the system has received the return from an object, the computer must immediately read the antenna's azimuth for computing the coordinate of the object at the moment. Because of the delay in the course of tracking, a dynamic error is introduced to the system, and it affects the' dynamic positioning precision of the radar. In this paper, a mathematical model describing the dynamic error is given. Based on this model, a method for testing the dynamic error is developed, which is easy to adopt from the engineering point of view. Also developed here is a new technique to improve the dynamic positioning precision by using a computer to correct the dynamic error. In conclusion, this paper gives the source program for correcting the dynamic error written in ALGOL-60, and the results of running the program on a NOVA machine.

本文通过对位置测量系统工作原理和误差的分析,得到描述传感器位置误差和编码器动态误差的数学模型,并给出一种对工程有实用价值的动态误差测试方法,从而提出了用计算机对位置测量系统的误差进行校正的新技术,还用ALGOL-60算法语言编写了误差校正过程的源程序。采用这种方法可以提高定位精度,并提供了用较低精度传感器组成高精度定位系统的可能性。

In modern industry,especialy in aviation and astronavigation,curves ofhigh degree give form to the surfaces of many parts,such as those of aircraftwings,missile stabilizing fins and ribbed profiles.Machining these Parts byusing interpolation comparing dot by dot would cause complicated programmingand bring about less accuracy as well.In this paper the mathematical model of direct interpolating curves of highdegree is established on the basis of the pulse interpolation at intervals.Inter-polation is illustrated...

In modern industry,especialy in aviation and astronavigation,curves ofhigh degree give form to the surfaces of many parts,such as those of aircraftwings,missile stabilizing fins and ribbed profiles.Machining these Parts byusing interpolation comparing dot by dot would cause complicated programmingand bring about less accuracy as well.In this paper the mathematical model of direct interpolating curves of highdegree is established on the basis of the pulse interpolation at intervals.Inter-polation is illustrated and its flowcharts are given also presented in the paper isan experimental report on interpolation on numerical-control linear cutting mach-ines controlled by TP801 Z80 microcomputer with a single plate of integratedcircuit.

在现代工业中,特别是在航空、宇航工业中,有很多零件的表面是由高次曲线组成的。如飞机的机翼、导弹的尾翼、肋骨线等。如果在数控机床上用逐点比较插补法加工这类零件,不仅编程烦杂而且插补精度也不高。本文根据脉冲间隔插补法建立了直接插补高次曲线的数学模型、列举出插补实例、拟定出插补流程图。并采用TP801 Z80单板微计算机控制数控线切割机进行了插补实验.

TYSY-5 Piezoelectric gyro is a novel miniaturized solid transducer with the physical size of 36×64x16mm3, weight of~100g, power supply of 0.5W (for the type of non-constant temperature),output gradient of~ 18mV/°/s,preparation time of 10 minutes,and atmospheric temperature of -40℃ to +50℃. Other routine tests are demonstrated to meet the needs of aeronautics. Particularly, this transducer is available for solid-state angular rate sensors used in telemeterring of air-to-air missiles.

本文介绍一种空-空弹遥测用固态角速率传感器。外形尺寸为36×64×16mm~3。重量约为100g。分有恒温的与不加恒温的二类。不加恒温的功耗约为0.5W,加恒温的约9W。输出梯度为18mV/°/s,非线性误差不大于2%,准备时间为10分钟,工作环境温度-40—+50℃,其他例行试验也符合航空要求。由于采取了新的设计方法,与过去同类型产品相比,准备时间缩短了二倍,体积减小、重量减轻,高温和低温下的稳定性按角速率计算,提高一倍,线性度及阻尼比均有改善。

 
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