-
公开(公告)号:KR101330213B1
公开(公告)日:2013-11-18
申请号:KR1020130105472
申请日:2013-09-03
Applicant: 국방과학연구소
Abstract: The present invention provides a device for assembling and testing a portable guided missile which includes a platform with a rail extended in the first direction; a portable guide missile which fixes module which fixes the portable guide missile by covering and is driven to be rotated in the second direction parallel to the ground surface and in the third direction perpendicular to the ground surface; a launching tube fixing module which fixes a portable guide missile launching tube and is moved along the rail by being mounted on the platform; a front table which is arranged by being separated from the platform in the first direction; an image tracking unit which collects data by tracking a target on the front table which is acquired by a seeker mounted on the portable guide missile; and a driving unit which drives the portable guide missile fixing module based on the data. [Reference numerals] (AA) Operate a mock target;(BB) Spot the mock target in move and lock on the target;(CC) Track the target and check the eye line information;(DD) Track the target;(EE) Check the performance of a guided missile;(FF) Gimbal;(GG) Give an operation command;(HH) Check the gimbal to be controlled;(II) Target tracking information;(JJ) Additional data
Abstract translation: 本发明提供了一种用于组装和测试便携式导弹的装置,其包括具有沿第一方向延伸的轨道的平台; 便携式导弹,其固定通过覆盖固定便携式导弹的模块,并被驱动沿平行于地面的第二方向和垂直于地面的第三方向旋转; 发射管固定模块,其固定便携式导弹发射管,并通过安装在平台上沿着轨道移动; 前台,其沿第一方向与平台分离; 图像跟踪单元,其通过跟踪由安装在便携式导弹上的探测器获取的前台上的目标来收集数据; 以及基于该数据驱动便携式引导导弹固定模块的驱动单元。 (参考号)(AA)操作模拟目标;(BB)瞄准移动中的模拟目标并锁定目标;(CC)跟踪目标并检查眼线信息;(DD)跟踪目标;(EE) 检查导弹的性能;(FF)Gimbal;(GG)给出操作命令;(HH)检查待控制的万向节;(II)目标跟踪信息;(JJ)附加数据
-
公开(公告)号:KR1020170009465A
公开(公告)日:2017-01-25
申请号:KR1020150101579
申请日:2015-07-17
Applicant: 국방과학연구소
Abstract: 본발명은유도무기체계에서의표적추적방법에관한것으로, 보다상세하게는, 시야각이고정된카메라를이용하여표적을추적하는경우표적과의거리가가까워짐에따라표적의크기가커지는것을인지하고상기크기가커진표적의중점을다시감지하여상기표적의중점을중심으로새로운표적영상을설정함으로써, 표적을놓치지않고타격할수 있는유도무기체계에서의표적추적방법에관한것이다. 본발명에의한유도무기체계에서의표적추적방법의일 실시예는, 표적영상으로부터추출되는표적의특징값을이용하여표적을추적하는표적추적단계; 상기표적영상에서상기표적의크기를추정하는표적크기추정단계; 상기추정된표적의크기가상기표적영상을벗어나는지판단하여상기표적영상을교체할지판단하는표적영상교체판단단계; 및상기표적영상을교체하는것으로판단하는경우표적영상을교체하고교체된표적영상으로부터표적의특징값을추출하는표적영상교체단계; 를포함할수 있다.
-
公开(公告)号:KR101408093B1
公开(公告)日:2014-06-17
申请号:KR1020140007831
申请日:2014-01-22
Applicant: 국방과학연구소
Abstract: The present invention relates to a mounting device for a portable guided missile and, more specifically, a mounting device for a portable guided missile, capable of simultaneously perform a function providing management convenience and firing stability while performing roles of a fixing unit and a support unit. The mounting device for a portable guided missile includes a Picatinny rail adaptor mounted on a portable weapon; a ball head connected to the lower end of the Picatinny rail adaptor; and a holder supporting the lower end of the ball head.
Abstract translation: 本发明涉及一种用于便携式导弹的安装装置,更具体地说,涉及一种用于便携式导弹的安装装置,能够同时执行提供管理便利性和起火稳定性的功能,同时执行定影单元和支撑单元的作用 。 用于便携式导弹的安装装置包括安装在便携式武器上的Picatinny轨道适配器; 连接到Picatinny轨道适配器下端的球头; 以及支撑球头下端的支架。
-
公开(公告)号:KR101750162B1
公开(公告)日:2017-06-23
申请号:KR1020150101579
申请日:2015-07-17
Applicant: 국방과학연구소
Abstract: 본발명은유도무기체계에서의표적추적방법에관한것으로, 보다상세하게는, 시야각이고정된카메라를이용하여표적을추적하는경우표적과의거리가가까워짐에따라표적의크기가커지는것을인지하고상기크기가커진표적의중점을다시감지하여상기표적의중점을중심으로새로운표적영상을설정함으로써, 표적을놓치지않고타격할수 있는유도무기체계에서의표적추적방법에관한것이다. 본발명에의한유도무기체계에서의표적추적방법의일 실시예는, 표적영상으로부터추출되는표적의특징값을이용하여표적을추적하는표적추적단계; 상기표적영상에서상기표적의크기를추정하는표적크기추정단계; 상기추정된표적의크기가상기표적영상을벗어나는지판단하여상기표적영상을교체할지판단하는표적영상교체판단단계; 및상기표적영상을교체하는것으로판단하는경우표적영상을교체하고교체된표적영상으로부터표적의특징값을추출하는표적영상교체단계; 를포함할수 있다.
Abstract translation: 另外,本发明衍生的涉及一种武器系统eseoui目标跟踪方法,更具体地,在通过使用所述固定摄像机的视场角的目标的跟踪的情况下,注意到,随着距离的目标增加,并且目标的方法和尺寸大小 本发明涉及一种冲击可导致武器系统eseoui目标跟踪方法,通过其而无需再检测放大的目标的聚焦设置关于目标的中点,目标未命中一个新的目标图像。 根据本发明的制导武器系统中的目标跟踪方法的一个实施例包括:目标跟踪步骤,使用从目标图像提取的目标的特征值来跟踪目标; 估计目标图像中目标的大小; 确定估计的目标的大小是否在目标图像之外并且确定是否替换目标图像; 以及目标图像替换步骤,在确定替换目标图像时,替换目标图像并且从替换的目标图像提取目标的特征值; 该可包含。
-
公开(公告)号:KR101356554B1
公开(公告)日:2014-01-29
申请号:KR1020130095894
申请日:2013-08-13
Applicant: 국방과학연구소
Abstract: The present invention relates to a deploying and folding structure of a wing used for controlling a position and a posture of a guided missile during a flight. The guided missile includes a plurality of wings used for controlling the posture and the position of the guided missile during the flight. The deploying and folding structure of the wing of the guided missile includes a hinge which is a rotary axis of the wing by being included on one end of the wing; a spring providing a rotatory force to the wing while the wing is rotated; and a hinge body in which the wing, the spring, and the hinge are assembled. The deploying and folding structure of the wing of the guided missile is characterized by deploying and folding the wing by rotating the same around the hinge once.
Abstract translation: 本发明涉及一种用于在飞行中控制导弹的位置和姿势的机翼的展开和折叠结构。 导弹包括用于控制飞行中导弹的姿势和位置的多个翼。 导弹翼的展开和折叠结构包括一个铰链,它是翼的旋转轴线,它包括在机翼的一端; 弹簧在机翼旋转时向机翼提供旋转力; 以及铰接体,其中机翼,弹簧和铰链组装在其中。 导弹翼的展开和折叠结构的特点是通过围绕铰链旋转一次来展开和折叠机翼。
-
公开(公告)号:KR101338156B1
公开(公告)日:2013-12-06
申请号:KR1020130105471
申请日:2013-09-03
Applicant: 국방과학연구소
Abstract: The present invention provides a portable ejection deice for a guided missile. The present invention includes a first cylindrical surface; a housing including an extended surface extended from one end of the first surface by being curved towards the outside of a cylinder; and a connection ring assembly connecting the portable guided missile and the housing. The connection ring assembly unit includes a body in which a groove in which the extended surface inserted is formed on one end, wherein the one end forms a free end and the other end forms a fixed end by being connected to the housing; a spring applying elasticity to the body by being arranged between a first surface and the connection ring body; and a fixing pin of which one end faces the first surface by passing through the body.
Abstract translation: 本发明提供一种用于导弹的便携式喷射罩。 本发明包括第一圆筒形表面; 壳体,其包括从所述第一表面的一端朝向圆柱体的外侧弯曲的延伸表面; 以及连接便携式导弹和壳体的连接环组件。 连接环组件单元包括其中在一端形成有延伸表面插入的槽的主体,其中一端形成自由端,另一端通过连接到壳体形成固定端; 弹簧通过布置在第一表面和连接环体之间而对身体施加弹性; 以及通过穿过本体而使其一端面向第一表面的固定销。
-
-
-
-
-