antiaircraft missile

英 [ˌæntɪˈeəkrɑːft ˈmɪsaɪl] 美 [ˌæntaɪˈɛrˌkræft ˈmɪsl]

网络  防空导弹

电力



双语例句

  1. Study on Leading Error and Angle Acquisition Problems of Composite Guidance Antiaircraft Missile
    防空导弹复合导引引导误差与角度截获问题研究
  2. The targets type recognition is an important content of antiaircraft missile command and control model.
    目标识别模型是防空导弹指控模型的重要组成部分。
  3. Terminal Sliding Mode Control for Attitude Control of Antiaircraft Missile
    防空导弹姿态控制系统终态滑模变结构设计
  4. Abstract: the paper introduces the function, composition, characteristics and the process of operation for the Russian antiaircraft missile system top-m1.from the point of the system requirements, the main technologies adopted is introduced in the two radar systems of top-m1.
    文摘:介绍了俄罗斯“道尔-m1”防空导弹武器系统的功能、组成、特点和作战过程,并从武器系统的总体需求出发,介绍了其两部雷达所应用的主要技术。
  5. Research on autopilot of control system for portable antiaircraft missile
    便携式防空导弹自动驾驶仪控制系统研究
  6. Research on the Whole Flying Trajectory Simulation System of Command Guided Antiaircraft Missile
    指令制导防空导弹全弹道飞行仿真系统研究
  7. A Modified proportional guidance Law is studied and designed base on a certain antiaircraft missile here.
    以某型防空导弹为背景,在给定的初始条件下,为使弹道需用过载分布合理,研究设计了一种适合工程应用的修正比例导引规律。
  8. Application of Integral Separated PID Control in Antiaircraft Missile
    积分分离PID控制在某防空导弹中的应用
  9. Reliability is the important determinative factor of antiaircraft missile system, also is the important connotation of materiel facility.
    可靠性是防空导弹武器系统效能的重要决定因素,亦是武器装备质量的重要内涵。
  10. In view of the contents and features of the overall design of antiaircraft missile, especially dynamic uncertainty of the design process, a new concept named self-adapting concurrent design ( SACD) is proposed based upon the fundamental principle of concurrent design and adaptive control.
    针对防空导弹总体设计的内容和特征,特别是其设计过程的动态不确定性,应用并行设计和自适应控制基本原理,提出了自适应并行设计的概念。
  11. The delay modeling of information processing and communication of an antiaircraft missile weapon system
    防空导弹武器系统的信息处理与通信延迟建模
  12. A New Method of the General Device Interconnection in the Antiaircraft Missile
    防空导弹弹上设备互联网设计新方法和新技术
  13. Research on the overall concurrent design concept and method for antiaircraft missile
    防空导弹并行总体设计概念与方法探讨
  14. Modeling and analysis of command and control system based on Petri net in antiaircraft missile
    基于PETRI网的防空指控系统的建模及分析
  15. The architecture is valuable in network centric warfare of the antiaircraft missile system.
    该结构对实现防空导弹网络中心战有指导意义。
  16. Study of Control Mechanism Based on One Antiaircraft Missile Flying Simulation
    基于某型防空导弹飞行仿真的控制机制研究
  17. The Application of Computer to Display Control Systems of Antiaircraft Missile
    计算机在防空导弹武器显示控制系统中的应用
  18. Simulation and Judgment of Casualty Lethality Criteria for Antiaircraft Missile
    某型防空导弹杀伤标准的判定与仿真研究
  19. Its basic content is explained in detail. The whole dynamic flying simulation of the guided, control system of one antiaircraft missile is analyzed and designed by this method.
    介绍了一种,详细说明了它的基本内容,并以此方法对防空导弹制导控制系统的全弹道动态飞行仿真进行了分析、设计。
  20. Study on the Plume Simulation of One Antiaircraft Missile
    基于某型防空导弹的尾焰仿真研究
  21. Simulation Model for Battle Damage of Antiaircraft Missile Based on Object-Oriented
    基于面向对象的防空导弹战斗损伤仿真模型
  22. Research of Flight Simulation Space Visualization in the Antiaircraft Missile System
    防空导弹系统飞行仿真空间可视化研究
  23. The paper first describes the hierarchical reasoning structure of the data fusion in military applications and various methods of data fusion. Then some applications are further introduced in the C 4 I system of antiaircraft missile weapons.
    首先叙述数据融合在军事应用中的递阶推理体系结构和各种数据融合方法,然后对防空导弹武器C4I(CommandControlCommunicationComputerIntelligence,简称C4I)系统中应用它的某些方面作了进一步的表述。
  24. The Parameter Model about the Combat Resilience of Antiaircraft Missile Weapon System
    防空导弹武器系统抢修性时间参数模型
  25. Research of Simulation Techniques Apply in Development of Antiaircraft Missile
    仿真技术在防空导弹研制中的应用研究
  26. A Method of Trajectory Optimization for Homing Antiaircraft Missile
    寻的防空导弹的一种弹道优化方法
  27. Simulation technique is the essential measure of guidance optimization design and performance research for portable antiaircraft missile.
    仿真技术是便携式防空导弹系统优化设计和性能研究的必要手段。
  28. Vertical launching technology of Antiaircraft Missile
    防空导弹的垂直发射技术
  29. TOP-M1 Antiaircraft Missile Weapon System
    道尔-M1防空导弹武器系统
  30. The thesis also introduces the DSS system of cost control management of antiaircraft missile armament system.
    并且,对航天二院防空导弹武器系统成本控制管理DSS系统进行了简要的分析和介绍。