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公开(公告)号：KR1020140052301A
公开(公告)日：2014-05-07
申请号：KR1020120118267
申请日：2012-10-24
Applicant: 국방과학연구소
Abstract: The present invention relates to a strapdown seeker, and more specifically, to a system and a method for estimating a line of sight rate by taking into account, the delay time of the strapdown seeker. According to the present invention, in the case of the strapdown seeker, the implementation of a loop acting as a stabilization loop is possible by taking into account, the delay time of the strapdown seeker.
Abstract translation: 本发明涉及一种捷联寻求者，更具体地说，涉及一种通过考虑到连接引导器的延迟时间来估计视线速率的系统和方法。 根据本发明，在连接引导器的情况下，通过考虑连接引导件的延迟时间，可以实现作为稳定环路的回路。
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公开(公告)号：KR101751647B1
公开(公告)日：2017-06-28
申请号：KR1020160126411
申请日：2016-09-30
Applicant: 국방과학연구소
CPC classification number: G01S13/883 , G01S13/006
Abstract: 본발명은표적을요격하기위한비행체의공간안정화루프를가지는탐색기유도신호에포함된상기비행체의동체운동성분을제거한시선변화율을산출하여유도명령을생성하는공간안정화루프를가지는탐색기유도신호의동체운동성분제거방법으로서, 본발명에의하면, 공간안정화루프를가지는 2축김블형탐색기에서유도신호로부터유도루프의안정성을증가시킬수 있다.
Abstract translation: 本发明是在资源管理器的感应信号的具有用于产生感应命令来计算视线率的线，去除具有车顶的空间稳定性拦截目标包括在资源管理器的感应信号中的车辆的身体运动分量的空间稳定回路的身体运动 作为成分去除方法中，本发明可从在第二chukgim beulhyeong具有空间稳定回路Explorer中的感应圈增加的感应信号的稳定性。
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公开(公告)号：KR101432736B1
公开(公告)日：2014-09-23
申请号：KR1020120118267
申请日：2012-10-24
Applicant: 국방과학연구소
Abstract: 본 발명은 동체 부착형 탐색기에 관한 것으로서, 더 상세하게는 동체 부착형 탐색기 지연 시간을 고려한 시선각 변화율 추정 시스템 및 방법에 대한 것이다.
본 발명에 따르면, 동체 부착형 탐색기의 경우 동체 부착형 탐색기 지연 시간을 고려하여 안정화 루프의 역할을 수행하는 루프의 구현이 가능하다.-
公开(公告)号：KR101385451B1
公开(公告)日：2014-04-15
申请号：KR1020120144623
申请日：2012-12-12
Applicant: 국방과학연구소
Abstract: The present invention relates to an apparatus and method for controlling impact velocity of a flying object. The method for control impact velocity of a flying object according to an embodiment includes the steps of: when the combustion speed of the flying object is higher than a reference combustion speed at the time of the combustion termination of the flying object, decreasing the flying speed by lowering the flight altitude, thereby decreasing the impact velocity; and when the combustion speed of the flying object is lower than the reference combustion speed at the time of the combustion termination of the flying object, increasing the flying speed by raising the flight altitude, thereby increasing the impact velocity. [Reference numerals] (100) Combustion speed detecting unit; (200) Control unit
Abstract translation: 本发明涉及一种用于控制飞行物体的撞击速度的装置和方法。 根据实施例的用于控制飞行物体的撞击速度的方法包括以下步骤：当飞行物体的燃烧速度高于飞行物体燃烧终止时的参考燃烧速度时，降低飞行速度 降低飞行高度，从而降低冲击速度; 并且当飞行物体的燃烧速度低于飞行物体的燃烧终止时的基准燃烧速度时，通过提高飞行高度来提高飞行速度，从而提高冲击速度。 （附图标记）（100）燃烧速度检测单元; （200）控制单元
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