再入段的英文

• re-entry portion
• reentry stage

• "再入"英文翻译    reentry
• "段"英文翻译    section; segment; part; para ...
• "再入段截击" 英文翻译 :    reentry interception; satellite interception
• "再入段遥控" 英文翻译 :    reentry phase remote control
• "再入段假目标" 英文翻译 :    re-entry decoy
• "再入" 英文翻译 :    [航空] reentry◇再入大气层导弹 reentry missile; 再入弹[轨]道 reentry trajectory; 再入遥测 reentry telemetry; 再入制导 reentry guidance
• "加入段" 英文翻译 :    building-out section
• "进入段" 英文翻译 :    approach section; entry leg
• "输入段" 英文翻译 :    input section; load segment
• "装入段" 英文翻译 :    load segment
• "双线插入段" 英文翻译 :    double track interpolation
• "冰川舌嵌入段" 英文翻译 :    entrenched part of the glacier tongue
• "复格式插入段" 英文翻译 :    divertimento
• "输入段综合症" 英文翻译 :    afferent loop syndrome
• "再入, 再进" 英文翻译 :    reentry
• "再入舱" 英文翻译 :    reentry capsule; re-entry package
• "再入的" 英文翻译 :    reentrant
• "再入点" 英文翻译 :    reentry point
• "再入杆" 英文翻译 :    reentry post
• "再入级" 英文翻译 :    reclassification; return stage
• "再入角" 英文翻译 :    reentrance angle; reentry angle
• "再入院" 英文翻译 :    readmission
• "垂直再入" 英文翻译 :    vertical reentry
• "大过载再入" 英文翻译 :    high-g reentry
• "大阻力再入" 英文翻译 :    high drag reentry

• In this paper , the principles and methods of target recognition are discussed mainly , using infrared optical technical equipment through the measurement of the target s temperature , radiant intensity and infrared thermal image
  反导系统对于来袭弹道导弹弹道中段及再入段的识别可以用微波雷达技术，也可用光学技术。
• The guidance scheme includes a trajectory planner that generates a feasible flight trajectory and a control law that achieves bounded tracking of the downrange and crossrange distances as functions of energy
  其中，轨迹规划器可产生一个可行的飞行轨迹。控制律作为能量的函数可实现再入段对纵向和横向航程的有界跟踪。
• The characteristics of the method is that it can modify the guidance coefficients automatically according to the errors between the actual trajectory and the standard trajectory , this is the essential of the standard trajectory guidance . it don " t need any pre - knowledge of the coefficients , this simplifies the problem greatly . following that , the method of predicting the falling site of the instant retuning trajectory is studied
  这一方法的特点是从反馈增益系数对再入段纵程偏差修正的本质出发，利用实际弹道和标准弹道的偏差，通过调节升阻比增量，不断修正再入段纵程偏差，最终确定反馈增益系数；这一方法的优点是在求解反馈增益系数时，不必依赖先验知识选取初值，使反馈增益系数的确定更为简便。
• The approach of obtaining the guidance coefficients can be utilized in the situations in which more than four coefficients are hired for guidance to enhance the guidance performance . in addition , more precise earth model , which is non - spherical and will circle around its body axis , can be considered , and this will lead to more true results
  最后，本文对进一步的工作提出了建议，认为可以考虑用四维以上的制导参数确定反馈增益系数以改善其制导性能，另外，可以进一步考虑地球旋转时影响飞船再入段纵程的因素，使得拟合结果更接近实际情况。
• Abstract : in order to achieve effective breaking through the enemy s anti - missile defense theatre and avoid intercepted by anti - missile defense system , many breakthrough methods have been implemented in middle course and re - entry phase of ballistic missile to protect the missile from acquisition , tracking and recognition by anti - missile system
  文摘:弹道导弹为实现有效的突破反导防区而不被防御系统拦截，在其弹道中段和再入段采用了多种突防措施，以免受反导系统的搜索、跟踪和识别。