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   certain missile 的翻译结果: 查询用时:0.171秒
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certain missile
相关语句
  某型导弹
     Design of Virtual Operation Environment of a Certain Missile Based On DI-GUY
     基于DI-GUY的某型导弹虚拟操作训练环境设计
短句来源
     The Design of Measurement and Control System for a Certain Missile Based on CAN
     基于CAN的某型导弹测控系统的设计
短句来源
     Application of SpaceBall in a Certain Missile's Virtual Hanging System
     SpaceBall在某型导弹虚拟挂弹系统中的应用
     Application of DSP in Test Training Device for Certain Missile
     DSP在某型导弹地面测试训练产品中的应用
短句来源
     Research on Detection Simulation Model for Radar Net of Certain Missile
     某型导弹雷达网检测仿真模型研究
短句来源
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  某导弹
     Research on the Application of RTSI Bus to the Launch and Control System Based on PXI-Bus in Certain Missile
     RTSI总线在某导弹PXI-Bus发控系统中的应用研究
短句来源
     Stress Analysis Calculations for Certain Missile Sample Code
     某导弹采编器的应力分析计算
短句来源
     Design of the Dynamic Parameters` Sampling Unit of Certain Missile Mockup
     某导弹模型动态参数的采集单元设计
短句来源
     The application of RTSI bus to the launch and control system based on PXI-Bus in certain missile is studied.
     对RTSI总线在某导弹PX I-Bus发控系统中的应用作了较深入的研究.
短句来源
     Take certain missile launcher as the main object, the reliability evaluation methods of the canister's inner ballistic functional parameters were introduced(namely: Bayes method and Monte Carlo digital simulation method).
     以某导弹发射装置为主要研究对象 ,介绍了可对其筒内弹道性能参数进行可靠性评估的方法 ,即 :Bayes方法和Monte -Carlo数字仿真法。 在Bayes方法中针对试验数据为来自不同母体的特点 ,给出了内弹道性能参数服从正态分布下的环境因子 ;
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  “certain missile”译为未确定词的双语例句
     Finite Element Analysis of Static-Dynamic for Certain Missile Erecting Arm
     导弹起竖臂的静动态有限元分析
短句来源
     The analysis and design of the guidance and control loop for a certain missile on the basis of radome compensation
     考虑天线罩瞄准线误差补偿的制导控制回路分析与设计
短句来源
     The paper describes production background of the on-board electronic section of a certain missile and its development status at home and abroad. It focus on the design process of the on-board electronic section and operation principle of the circuit composed by 16 bit microprocessor and FPGA, as well as carry out integration and miniaturization research by taking the certain antitank missile and its derivative as background.
     本论文论述了某小型导弹弹上电子舱的产生背景及国内外发展状况,重点介绍了弹上电子舱的设计过程和由16位的微处理器及FPGA组成电路工作原理,并以某反坦克导弹及其改型为背景开展弹上电子舱综合化、小型化的研究。
短句来源
     A method of constructing certain missile virtual maintenance training system was proposed based on virtual reality technology,virtual prototype technology and process simulation technology.
     提出基于虚拟现实技术、虚拟样机技术和过程仿真技术的大型复杂装备虚拟维修训练系统设计方法。
短句来源
     Research on Fault Diagnosis of Docking and Debugging of Weapon System Certain Missile
     导弹武器系统对接联调故障诊断系统研究
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The augmentation-analytical reconstruction proportional navigation law is given. Using" the method of analytical reconstruction the acceleration information of target is added into-the missile guidance law. The performance of the homing missile are improved. Using this-guidance law for a certain missile, the good numerical simulation results are obtained.

本文提出“解析重构比例导引规律”,这是一种扩展的比例导引规律。在导弹上用解析重构的方法形成目标加速度信息并引入导引规律,提高了自动导引导弹的性能。将此导引规律应用于某导弹,通过数学仿真得到较好的结果。

It is a very complex and time-consuming work to evaluate the performance of the air-to-air missiles. For overcoming this difficulty, an expert simulation system for target practice of air-to-air missiles was designed recently. With the inital attack conditions and the target avoidance strategy being selected with the expert knowledge, the simulation times necessary for evaluating the performance of missiles is reduced in a great deal. The use of general mathematical models and the separation...

It is a very complex and time-consuming work to evaluate the performance of the air-to-air missiles. For overcoming this difficulty, an expert simulation system for target practice of air-to-air missiles was designed recently. With the inital attack conditions and the target avoidance strategy being selected with the expert knowledge, the simulation times necessary for evaluating the performance of missiles is reduced in a great deal. The use of general mathematical models and the separation between the general knowledge and the knowledge related to certain missiles and targets make the system be able to be applied to various kinds of air-to-air missiles. This paper introduces this simulation system, including system structure, avoidance strategy analysis,knowledge representation and the building of general mathematical models. The application example of this system to a certain kind of missile is also given with the intention to demonstrate the effectiveness of the system.

本文介绍一个为检验空空导弹性能而研制的空空导弹打靶专家仿真系统。该系统采用专家经验选择导弹初始攻击条件和目标的逃逸策略,因而可以大大减少检验导弹性能所必需的仿真次数。该系统采用通用型数学模型,并把与具体导弹及目标有关的知识与一般性知识分开,因而具有较强的通用性。

Major technique problems and its technical measures used in sturctural optimization design of missile wing are discussed. Optimization software for microcomputer is designed based on the technical measures and its principle The principle, characteristics and operational environment of SODS software package are presented Structural optimization design of missile wing for a certain missile is given as an example The results show that the optimizing algorithm is effective, the software is short and pithy,...

Major technique problems and its technical measures used in sturctural optimization design of missile wing are discussed. Optimization software for microcomputer is designed based on the technical measures and its principle The principle, characteristics and operational environment of SODS software package are presented Structural optimization design of missile wing for a certain missile is given as an example The results show that the optimizing algorithm is effective, the software is short and pithy, flexible and convenient in use.

介绍了弹翼结构优化设计中的一些重要技术问题:利用设计变量链化减少设计变量数目;采用区域化方法和抛弃法删除约束;利用函数的二价台劳展开构成高质量的显函数,以减少分析次数,利用满应力概念形成动态几何下限,依据圣维南原理,将约束Hessian矩阵简化成对角阵;灵敏度分析采用虚载荷法和状态空间法两种方法。基于上述原理和技术措施,编制了优化设计软件包,经典型算例和某型导弹弹翼优化设计应用表明,本文提出的优化算法是有效的,软件短小精练、使用灵活简便。

 
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