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1)  Guidance image
制导图
2)  image guidance
图像制导
1.
This system was tested in the half practical emulational system of image guidance.
以 DSP和 CPL D为核心 ,构造了一种针对细长目标的准实时识别跟踪系统 ,并在图像制导半实物闭环仿真系统内进行了仿真试验。
3)  conductivity mapping
电导制图
4)  guidance reference image
制导基准图
1.
To solve the problem of guidance reference image resources support of cruise missile,requirement and general steps of route planning,preparation and preprocessing of mat ching zone reference images is studied.
立足于巡航导弹作战保障 ,研究了制导基准图制备过程中巡航导弹航迹规划的要求及一般步骤 ,匹配区基准图的筛选与预处理 。
5)  image-aided terminal guidance
图像末制导
1.
In anti-runway image-aided terminal guidance system,the images of missile-borne camera maybe not include the whole runway.
反跑道图像末制导系统中,针对弹载图像中可能不存在完整跑道,而跑道内部比较均匀很难由灰度或结构特征锁定目标点的问题,提出一种攻击目标点的选取方法。
6)  image guided missile
图像制导导弹
1.
To remove dissymmetry of the movement of monitor image under some conditions when image guided missile adopting guided search,two factors causing this dissymmetry are found,viz,the angular velocity of line of sight and the lead speed of the missile.
为了消除图像制导导弹在采用导引搜索时某些情况下监视器画面移动速度的不对称现象,找到了形成不对称现象的两个原因——视线角速度和导弹的前置速度,在此基础上对常规一字型搜索规律进行了改进,形成一种非对称一字型搜索规律。
2.
To study the target catching probability of image guided missile,a model of various maneuverability flight of helicoptcr is founded and left-to-right guided searching program and several measuring errors are introduced.
为了研究图像制导导弹采用导引搜索时目标的进场概率,建立了目标作不同机动的模型,并将测量误差引入到模型中。
3.
For an image guided missile,adopting guided search can increase the probability of target entering the instantaneous field of view of the seeker,but it may cause dissymmetry of the monitor image under some conditions.
对于图像制导导弹,采用导引搜索可提高目标的进场概率,但在某些情况下会引起监视器画面移动的不对称现象。
补充资料:波束制导(见遥控制导)


波束制导(见遥控制导)
beam-rider guidance

  boshu zhidao波束制导(beam一rider guidanee)见遥控制导。
  
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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