制导站的英文

• guidance site; guidance station
  ◇制导站设备 [工业] guidance station equipment

• 制导:    guidance; guide; control and ...
• 站:    stand; be on one's feet
• 制导站设备:    guidance-position equipment
• 反导弹导弹制导站:    antimissile missile guidance station
• 前方观测制导站:    forward observation guidance station

例句与用法

1. Ground guidance station display symbology
   地面制导站显示器字符
2. General specification of tv tracker for ground to air missile guidance station
   地空导弹制导站电视跟踪仪通用规范
3. ( 4 ) applying measurement noise automatic weighting kalman filter to the guidance of line - guidance torpedo , we compromised target information and torpedo information , which in turn come from sonar of guidance station and inertial measurement units of torpedo
   ( 4 )将多传感器量测噪声自动加权卡尔曼滤波应用在线导鱼雷制导中，融合来自制导站声纳测量到的目标信息和来自鱼雷惯性测量组件的鱼雷位置和姿态等信息进行了仿真研究。
4. The tactical missile seeker handover accuracy from midcourse to terminal guidance is researched . the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources . firstly , the terminal guidance seeker presetting parameters are computed , based on the equations of a surface - to - air missile movement and a target movement . then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed . it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target , which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided
   研究复合制导的战术导弹中末制导交班的导引头预定精度问题.提出用小扰动法分析导引头预定参数对误差源的误差敏感性关系.以中远程防空导弹为例，结合导弹运动方程组和目标运动模型，计算了中末制导交班的导引头预定参数，并计算了在制导站雷达测量误差下的末制导导引头预定参数的计算精度.可知，导引头定位参数的计算误差随着弹目距离的接近而显著增大，得到中末制导交班不能太晚的重要结论
5. Abstract : the tactical missile seeker handover accuracy from midcourse to terminal guidance is researched . the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources . firstly , the terminal guidance seeker presetting parameters are computed , based on the equations of a surface - to - air missile movement and a target movement . then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed . it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target , which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided
   文摘:研究复合制导的战术导弹中末制导交班的导引头预定精度问题.提出用小扰动法分析导引头预定参数对误差源的误差敏感性关系.以中远程防空导弹为例，结合导弹运动方程组和目标运动模型，计算了中末制导交班的导引头预定参数，并计算了在制导站雷达测量误差下的末制导导引头预定参数的计算精度.可知，导引头定位参数的计算误差随着弹目距离的接近而显著增大，得到中末制导交班不能太晚的重要结论