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winged missile
相关语句
  飞航导弹
     THE APPLICATION OF LORAN-C/INS COMBINED NAVIGATION SYSTEM TO THE WINGED MISSILE
     Loran-C/INS组合导航系统在飞航导弹上的应用
短句来源
     The Application of H_∞ Control Theory to a Winged Missile's Attitude Control System
     H_∞控制理论在飞航导弹姿态控制中的应用
短句来源
     DEVELOPMENT OF FLIGHT SIMULATION TECHNIQUE FOR WINGED MISSILE
     飞航导弹飞行仿真技术的发展
短句来源
     Technology Application Research on Accuracy Evaluation and Verification of Winged Missile Weapon System
     飞航导弹武器系统精度评估与鉴定技术应用研究
短句来源
     Overload Control System Design for Winged Missile Using Fuzzy Dynamic Backsteping
     模糊反演飞航导弹过载控制系统设计
短句来源
更多       
  有翼导弹
     INTEGRATION DESIGN OF AIRFRAME/SOLID ROCKET MOTOR FOR WINGED MISSILE
     有翼导弹/固体火箭发动机一体化设计
短句来源
     The Analysis on Dynamical Stability of Winged Missile
     有翼导弹的动态稳定性分析
短句来源
     Same problems of integration design of airframe solid rocket motor for winged missile are studied.
     以某空空导弹为算例,研究了有翼导弹/发动机一体化设计问题。
短句来源
     Process and approaches of identifying key characteristics in the early stage of product development were proposed including three steps: design requirement acquisition,design requirement and characteristics mapping,and key characteristics decision. Finally,the wing design for winged missile was used to verify the proposed process and approaches.
     在此基础上,提出了产品开发早期的关键特性识别过程及其方法,包括设计要求获取、设计要求与特性映射和关键特性判定3个步骤,并以有翼导弹的弹翼为例予以验证。
短句来源
  “winged missile”译为未确定词的双语例句
     In this paper, high frequency scattering theories, including physical optics (PO), geometrical optics (GO) and magnetic equivalent currents (MEC), were used for calculating the radar cross section of winged missile with ellipsoidal and olive warhead considering the relative phase contributions of scattering centers.
     通过综合运用物理光学法 (PO)、等效电磁流法 (MEC)和几何光学法 (GO)等 ,并考虑目标各部分散射场间的相对相位关系 ,分析了椭球体和橄榄体两种不同形状弹头导弹的电磁特性 ,计算出了它们的雷达散射截面积 (RCS)。
短句来源
     On the base of those results,stealth measures of the winged missile are discussed in the end.
     最后,依据仿真结果对如何实现导弹目标隐身的措施进行了讨论。
短句来源
     Then, a simple effective overload control method for winged missile using intelligent resistance is presented.
     然后给出了一种简单有效的基于规则的智能阻尼过载控制方法。
短句来源
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The vibration design of the sensitive equipments on board of a certain multi-purpose sea defense missile was described and the result of ground vibration test was analysed. A concept of two-mass vibration reduced system model proposed in this paper is suitable to investigation into response of special missile-borne equipment to vibration. On basis of theoretically analysing the vibration transfer curve of single-degree-of-freedom vibration reduced system, several vibration design methods suitable...

The vibration design of the sensitive equipments on board of a certain multi-purpose sea defense missile was described and the result of ground vibration test was analysed. A concept of two-mass vibration reduced system model proposed in this paper is suitable to investigation into response of special missile-borne equipment to vibration. On basis of theoretically analysing the vibration transfer curve of single-degree-of-freedom vibration reduced system, several vibration design methods suitable for winged-missile-borne equipment have been outlined with particular attention given to the high damping function principle and the actual effect of application to this type missile.

本文介绍并分析了某型多用途海防导弹弹上灵敏设备的振动设计及地面振动试验结果。文中提出的二质量减振系统模型概念,很适用于弹上特设安装振动响应的研究;结合对单自由度有阻尼减振系统的振动传递曲线的理论分析,归纳出几种适用于飞航导弹设备振动设计的方法,其中重点介绍了高阻尼减振的作用原理及在该型号导弹上的实际应用效果。

The simulation engineering is coming into the procedure of winged missile development step by step and starts playing an important role owing to its effectiveness. The simulation test of a strapped-down inertial guidance system for winged missile is described. The results show that the simulatiom are important in research, development, experiment and trial flight for the missile system.

飞航导弹仿真工程正以其自身有成效的工作逐步进入型号研制序列中它应担当的角色。本文所介绍的飞航导弹方位捷联惯导仿真试验,充分表明了仿真在导弹系统论证、研制、原理实验及靶场试验准备中的重要作用。

The development prospect, features and main problems of simulation technologies for winged missile are described in accordance with the needs of the missile and the simulation experiences at home and abroad. Some views and suggestions are proposed.

本文结合飞航导弹的特点以及国内外飞航导弹的仿真经验,对于今后飞航导弹仿真技术的发展方向、特点和主要的技术问题进行了探讨,提出了作者个人的一些看法和建议。

 
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