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空空导弹
相关语句
  air to air missile
     The Test Method of Fuze Initiation Property in the Air to Air Missile System Test
     空空导弹总体试验中引信启动特性测试方法
短句来源
     Adaptive Flight Control System of Air to Air Missile with Quantitative Feedback Theory
     空空导弹自适应飞控系统的定量反馈理论设计
短句来源
     Introduces the calibration technique of fuze shielding transmit-receive isolation,forward transmission and the test method of fuze initiation property in the air to air missile system test.
     介绍了空空导弹总体试验中引信屏蔽罩收发隔离度、正向传输插损的标定技术和引信启动特性测试方法。
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     Present Status of Development and Applications of IR Air to Air Missile Equipment
     红外技术在空空导弹中的应用现状及发展趋势
短句来源
     According to polynomial fitting and interpolation method resolving existence problem of air to air missile impact area,presents two methods of pure BP neural network and the interpolation of BP neural network.
     针对多项式拟合和插值法解算空空导弹攻击区所存在的问题,提出了采用纯BP神经网络和BP网络-插值方法计算空空导弹攻击区。
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  aam
     Research and Application of on Quick Simulation for the AAM with Complex Guidance
     复合制导空空导弹快速仿真研究与应用
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     Analysis and evaluation of new approach of AIM-9X AAM seeker
     AIM-9X空空导弹位标器新技术分析和评价
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     Analysis of AAM Acquisition Probability in Multi-target Attacking
     多目标攻击空空导弹的目标截获概率分析
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     Modularization and Software Technology of AAM Fuze
     空空导弹引信模块化、软件化技术
短句来源
     Main kinds and characteristic parameters of active jamming for AAM with active radar are discussed,and the realization methods of active jamming in HWIL simulation are also studied.
     文中讨论了主动雷达型空空导弹所面临有源干扰的主要种类和特征参数,并对在半实物仿真试验中典型有源干扰信号的实现方法进行了研究。
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  “空空导弹”译为未确定词的双语例句
     Design of AIM Model Reference Variable Structure Flight Control System
     空空导弹模型参考变结构飞控系统设计
短句来源
     Analysis and Simulation of Design of a Missile Tracking Controller
     空空导弹跟踪控制器设计的理论分析与仿真
短句来源
     Design and Simulation of Guidance and Control System for Air-to-Air Missile
     空空导弹制导控制系统设计与仿真研究
短句来源
     Test and Analysis of Information Transmit Delay in Air-to-Air Missile System
     空空导弹系统信息延迟时间的测试及分析
短句来源
     Investigation of Target Recognition and Tracking Algorithm for Infrared Imaging Air-to-Air Missile
     红外成象型空空导弹目标识别与跟踪算法研究
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  aam
The outer diameter of Cu nanotubes can be controlled by adjusting the aperture of anodic alumina membranes (AAM) template, and the thickness of the tube wall can be controlled by deposition time.
      
The kinetics of free-radical copolymerization and terpolymerization of acrylamide (AAm), N, N'-methylenebis(acrylamide) (MBA) and methacrylic acid (MA) in the inverse water/monomer/cyclohexane/Tween 85 miniemulsion was investigated.
      
Active Appearance Model (AAM) enables accurate tracking of facial features in real-time, but lacks occlusions and self-occlusions.
      
The idea is to include occluded images into AAM training data.
      
We demonstrate the results by running experiments using gradient descent algorithm for fitting the AAM.
      
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This article describes the Norwegian Advanced Surface-to-Air Missile Systems (NASAMS), Which is a ground-launched version of the advanced medium-range air-to-air missile. The new weapon eventually will replace aging Hawk missile batteries that Currently guard air bases throughout Norway .

本文主要介绍挪威先进面空导弹系统(NASAMS),这种系统是先进中程空空导弹的陆基型。该新型武器最终将要替换目前用来保卫挪威空军基地的老式的霍克导弹连。

This article describes development of US' Advanced Air-to-Air Missile and concepts proposed by two industrial teams. The General Dynamics/ Westinghouse's AAAM concept uses folded long-chord cruciform wings and narrow-chord cruciform tailfins, a tandem-rocket booster plus a sustainer rocket with thrust-vector control, inertial midcourse guidance system plus semi-active radar / infrared seekers. The Hughes / Raytheon's missile uses a single pair of wings, a integral rocket / ramjet propulsion systems, and active...

This article describes development of US' Advanced Air-to-Air Missile and concepts proposed by two industrial teams. The General Dynamics/ Westinghouse's AAAM concept uses folded long-chord cruciform wings and narrow-chord cruciform tailfins, a tandem-rocket booster plus a sustainer rocket with thrust-vector control, inertial midcourse guidance system plus semi-active radar / infrared seekers. The Hughes / Raytheon's missile uses a single pair of wings, a integral rocket / ramjet propulsion systems, and active radar / imaging-infrared guidance. The two concepts are in the competition.

本文介绍了美国先进空空导弹(AAAM)研制情况及两个工业小组提出的AAAM导弹方案。通用动力-西屋公司的方案采用可折叠的长弦十字形弹翼和窄弦十字形尾翼,串列式助推器加上火箭主发动机,惯导加半主动雷达/红外末制导,并采用了推力向量控制系统。休斯-雷锡恩公司的方案采用单对弹翼,整体式火箭-冲压发动机,主功雷达和光电结合的制导方式。这两种方案正在竞争之中。

This report summarized and set up a more general model which can be used in arbitrary plane and fit to pursuit,intercept,down-shot,up-shot,and off-boresight launch on all aspects.Moreover it presents a new quick method determining attack area by program design and one with it can display or copy the results by graphic technology.Other studies concern the effects of the many factors on the attack area.It is true that this model is useful for Air-to-Air missile performances analysis.

本文建立了空空导弹任意平面的全向攻击区计算模型,在程序设计上实现了快速求解攻击区边界的方法,并利用图形显示技术,将攻击区从终端或打印机输出。最后以某型号实例进行了计算。

 
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