控制导弹的英文

• direct a missile

• "控制"英文翻译    control; dominate; regulate; ...
• "导弹"英文翻译    guided missile
• "雷达控制导弹" 英文翻译 :    radar-controlled missile; rader homing missile
• "自主控制导弹" 英文翻译 :    internally-guided missile; self-dependent missile
• "燃气舵控制导弹" 英文翻译 :    jet-vane-controlled missile
• "无线电控制导弹" 英文翻译 :    radio-controlled missile
• "导弹的制导" 英文翻译 :    missile guidance
• "导弹制导" 英文翻译 :    guided-missile control; missile guidance
• "导弹制导仪" 英文翻译 :    mi ile director; missile director
• "炮射制导弹" 英文翻译 :    clgp
• "试制导弹" 英文翻译 :    pre-production missile
• "研制导弹" 英文翻译 :    research and development missile
• "制导导弹" 英文翻译 :    aim a missile; navigate missile; seeker
• "导弹指令制导系统控制手柄" 英文翻译 :    command-guidance joy-stick
• "反导弹导弹制导站" 英文翻译 :    antimissile missile guidance station
• "被动制导导弹" 英文翻译 :    passive-guided missile
• "波束制导导弹" 英文翻译 :    beam follower; beam rider; riding missile; beam-launched missile; rider
• "导弹制导波束" 英文翻译 :    missile-bearing beam; missile-guidance beam
• "导弹制导军官" 英文翻译 :    missile guidance officer
• "导弹制导雷达" 英文翻译 :    missile guidance radar; missile-guidance radar
• "导弹制导设备" 英文翻译 :    missile guidance gear; missile guidance set
• "导弹制导系统" 英文翻译 :    missile brain; missile guidance system
• "地面制导导弹" 英文翻译 :    ground-guided missile
• "电视制导导弹" 英文翻译 :    television controlled missile; television-controlled missile
• "光电制导导弹" 英文翻译 :    electro-optically guided missile

• In order to design the autopilot for a rear controlled missile we must make a first estimate of the required aerodynamic derivatives .
  为了设计尾部控制导弹的自动驾驶仪，我们必须首先估算一下所需要的气动力导数。
• Design of missile vertlcal lanch system based on sing - chip control
  基于单片机控制导弹垂直发射系统设计
• The task of the missile control system is to guide the missile to the object , then smash it
  导弹控制系统的设计任务就是实现对导弹的控制，控制导弹飞向目标，最后击毁目标。
• And the traditional designed autopilot has poor robustness , so it should shift the autopilot ' s gain for the btt missile flying stably along the whole trajectory
  又由于用传统方法设计的自动驾驶仪鲁棒性不高，为控制导弹沿全弹道飞行，需逐段切换自动驾驶仪的增益。
• This thesis uses fuzzy changing the gain proportion guidance to control the yaw angle v and the pitching angle , and to realize following track , with the predetermined track , which had been designed by hierarchical track planning with voronoi diagram
  本文在利用voronoi图的分层航迹规划,规划出预定航迹,并利用模糊变增益比例制导律控制导弹的偏角v和弹道的倾角,实现航迹跟踪。
• This design method overcomes the traditional autopilot ' s disadvantage that should shift the autopilot ' s gain according to flight phase ; it also can make the btt missile fly stably along the whole trajectory , and can intercept a maneuvering target accurately
  该设计方法克服了传统自动驾驶仪在控制导弹飞行中需逐段切换增益的不足，能控制btt导弹在大空域内沿全弹道稳定飞行，并能精确拦截机动目标。