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1. 发明授权

CN106461361B 目标标记装置以及包括该目标标记装置的目标处理系统失效
公开(公告)号：CN106461361B
公开(公告)日：2018-07-17
申请号：CN201580008749.3
申请日：2015-01-07
申请人： MBDA法国公司
发明人：亚历山大·科特恩科夫 , 大卫·维古鲁 , 安东尼·维瓦瑞斯 , 奥利维尔·赫伯特 , 阿诺·杜兰廷
IPC分类号： F41G7/22 , B64C39/02 , F42B12/38 , F42B12/40 , G05D1/00 , F41G3/18
CPC分类号： F42B12/365 , B64C39/024 , B64C39/028 , B64C2201/12 , B64C2201/146 , F41G3/18 , F41G7/226 , F41G7/2286 , F41G7/2293 , F41H7/005 , F42B12/40 , G05D1/12
摘要：目标标记装置(1)包括：小型飞行单元(2)，所述飞行单元(2)被配置成在较低的高度处飞行并且借助于制导命令被制导，所述飞行单元(2)设置有至少一个能够测量环境的至少一个参数的传感器(4)；数据传输单元(6)，所述数据传输单元被配置成至少发射与所述传感器(4)所实现的测量结果有关的数据并且接收所述飞行单元(2)处的制导指令；以及，至少一个能够发射位置信息的发射器(9)。

2. 发明公开

CN106461361A 目标标记装置以及包括该目标标记装置的目标处理系统失效
公开(公告)号：CN106461361A
公开(公告)日：2017-02-22
申请号：CN201580008749.3
申请日：2015-01-07
申请人： MBDA法国公司
发明人：亚历山大·科特恩科夫 , 大卫·维古鲁 , 安东尼·维瓦瑞斯 , 奥利维尔·赫伯特 , 阿诺·杜兰廷
IPC分类号： F41G7/22 , B64C39/02 , F42B12/38 , F42B12/40 , G05D1/00 , F41G3/18
CPC分类号： F42B12/365 , B64C39/024 , B64C39/028 , B64C2201/12 , B64C2201/146 , F41G3/18 , F41G7/226 , F41G7/2286 , F41G7/2293 , F41H7/005 , F42B12/40 , G05D1/12
摘要：目标标记装置(1)包括：小型飞行单元(2)，所述飞行单元(2)被配置成在较低的高度处飞行并且借助于制导命令被制导，所述飞行单元(2)设置有至少一个能够测量环境的至少一个参数的传感器(4)；数据传输单元(6)，所述数据传输单元被配置成至少发射与所述传感器(4)所实现的测量结果有关的数据并且接收所述飞行单元信息的发射器(9)。(2)处的制导指令；以及，至少一个能够发射位置

4. 发明专利

JP2009144973A Target tracking guidance device and method 有权
标题翻译：目标跟踪指导装置和方法
公开(公告)号：JP2009144973A
公开(公告)日：2009-07-02
申请号：JP2007322143
申请日：2007-12-13
申请人： Ihi Aerospace Co Ltd , 株式会社Ihiエアロスペース
发明人： ISHIZUKA MASAYUKI , TANAKA NAOHIRO , NAKAJIMA TAKURO , MORITA KOJI
IPC分类号： F41G7/22 , G01S1/70 , G01S13/88
CPC分类号： F41G7/2293 , F41G7/226
摘要： PROBLEM TO BE SOLVED: To provide a target tracking guidance device and its method, constituting a system without mounting a laser output adjusting device and the like, since the reflected light of stable intensity is detected by a seeker regardless of angles of a laser irradiator, a target and a flying object, suppressing increase in dimension and mass of the laser irradiator, and eliminating restriction in operations such as transportation and installation. SOLUTION: This target tracking guidance device includes: a laser beam irradiating device 12 for irradiating the laser beam 3 to the target 1; and the flying object 14 loading the infrared ray seeker 16 detecting the reflected light 4 of the laser beam by the target, the laser beam 3 is irradiated to the target, and the reflected light 4 is detected by the infrared ray seeker 16, thus the target is captured, and the flying object is made to fly toward the target direction. A polarized light converting element 18 (1/4 wavelength lagging element) is disposed to convert the polarized light of the laser beam 2 generated by the laser beam irradiating device 12 from the linear polarized light to the circular polarized light, and the polarized light of the laser beam is converted from the linear polarized light to the circular polarized light to irradiate the laser beam 3 of circular polarized light to the target. COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：为了提供一种目标跟踪引导装置及其方法，其构成了不安装激光输出调节装置等的系统，因为不管角度如何，由探测器检测出稳定强度的反射光激光照射器，目标和飞行物体，抑制激光照射器的尺寸和质量的增加，并且消除诸如运输和安装的操作中的限制。该目标跟踪引导装置包括：激光束照射装置12，用于将激光束3照射到目标1; 并且飞行物体14装载由目标检测激光束的反射光4的红外线探测器16，激光束3照射到目标物，并且反射光4被红外线探测器16检测，因此，目标被捕获，飞行物体朝向目标方向飞行。偏振光转换元件18（1/4波长滞后元件）被设置为将由激光束照射装置12产生的激光束2的偏振光从线性偏振光转换为圆偏振光，将激光束从线性偏振光转换成圆偏振光，将圆偏光的激光束3照射到目标物上。版权所有（C）2009，JPO＆INPIT

5. 发明专利

JP2009162632A Laser semiactive guidance method 审中-公开
标题翻译：激光干扰指导方法
公开(公告)号：JP2009162632A
公开(公告)日：2009-07-23
申请号：JP2008000931
申请日：2008-01-08
申请人： Ihi Aerospace Co Ltd , 株式会社Ihiエアロスペース
发明人： ISHIZUKA MASAYUKI , TANAKA NAOHIRO , NAKAJIMA TAKURO , MORITA KOJI
IPC分类号： G01S17/88
CPC分类号： F41G3/145 , F41G7/226 , F41G7/2293
摘要： PROBLEM TO BE SOLVED: To provide a laser semiactive guidance method that is capable of improving the detection accuracy of an object by a seeker, that dispenses with the need for arranging staff to a laser irradiation device, that is capable of mounting a seeker with improved sensitivity on a flying object such as a missile, or the like, and that is capable of reducing the size and weight of the laser irradiation device.
SOLUTION: A laser irradiation device 3 decreases the laser output, stepwise or continuously, after lapse of a first setting time (T1) from the time of launch of a flying object 1 (T0), such that the intensity of a reflected laser light 6 at a seeker 1a falls within the range of light-detecting sensitivity of the seeker 1a.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供一种激光半主动引导方法，其能够通过寻求者提高对象的检测精度，从而不需要将人员安排到激光照射装置，该激光照射装置能够安装具有对诸如导弹等飞行物体的灵敏度提高的探测器，并且能够减小激光照射装置的尺寸和重量。解决方案：激光照射装置3在从飞行物体1（T0）的发射时间经过第一设定时间（T1）之后逐步或连续地减小激光输出，使得反射的引导器1a处的激光6落在探针1a的光检测灵敏度的范围内。版权所有（C）2009，JPO＆INPIT

6. 发明专利

JP3624853B2 Laser semi-active guidance methods and laser semi-active induction system 有权
公开(公告)号：JP3624853B2
公开(公告)日：2005-03-02
申请号：JP2001150022
申请日：2001-05-18
申请人：日本電気株式会社
发明人：和久神田
IPC分类号： F41G7/22 , F41G7/26 , G01S17/66 , G01S17/88 , G01S17/89
CPC分类号： F41G7/2293 , F41G7/226

7. 发明公开

KR1020070120184A 타겟 지정 및/또는 조명 시스템 및 항공 정찰 시스템 有权
标题翻译：目标指定和/或照明和空中重建系统
公开(公告)号：KR1020070120184A
公开(公告)日：2007-12-21
申请号：KR1020077025988
申请日：2006-04-07
申请人： 탈레스
发明人： 라로퀴,서지 , 운테라이너,패트릭 , 베르디,올리비에
IPC分类号： F41G3/22
CPC分类号： F41G7/226 , F41G3/145 , F41G7/2293 , G01C11/02
摘要： The invention concerns a system for target designation and/or illumination in a scene, which is designed to be fixed to an aircraft and comprising at least one optical path (1) equipped with a matrix sensor (2) forming an image of the scene, each image corresponding to an instantaneous field centered about a line of sight LV, and equipped with a device for deflecting the line of sight at a specific speed Vd enabling the target designation and illumination function to be provided through scanning. It comprises an additional device (3) for deflecting the line of sight at a speed Vr enabling an air reconnaissance function to be further provided through counter-scanning.
摘要翻译：本发明涉及一种用于场景中的目标指定和/或照明的系统，其被设计为固定到飞行器并且包括装备有形成场景的图像的矩阵传感器（2）的至少一个光路（1）每个图像对应于以视线LV为中心的瞬时场，并且配备有用于以能够通过扫描提供目标指定和照明功能的特定速度Vd偏转视线的装置。它包括用于以能够通过反扫描进一步提供空中侦察功能的速度Vr偏转视线的附加装置（3）。

8. 发明专利

KR102237510B1 KR102237510B1 - Methods and defense systems for repelling threats 有权
公开(公告)号：KR102237510B1
公开(公告)日：2021-04-07
申请号：KR1020197016403A
申请日：2017-10-27
申请人： 라인메탈 바페 뮤니션 게엠베하
发明人： 마르쿠스 융 , 알렉산더 그라프
IPC分类号： F41H13/00 , F41G3/14 , F41G7/22 , F41H11/02 , G01S7/495
CPC分类号： F41H13/005 , F41G3/145 , F41G7/226 , F41G7/2293 , F41H11/02 , G01S7/495
摘要： 위협물(2)이 방어 수단(3)에 대해 더 잘 보이도록 하는 것이 제안된다. 이러한 맥락에서, 위협물(2)은, 방어 수단(3)을 위해 더욱 강렬하게 이미지화되어야 한다. 더욱 효과적인 이미지화의 목적을 위해, 위협물(2)이, 더 강한 IR 특징을 방출하는 것 그리고 그에 따라 방어 수단(3)을 위해 배경에 대해 충분히 두드러지는 것이, 준비된다. 더 강한 IR 특징은, 위협물(2)의 표면(9)을 가열함에 의해 야기되고, 이는 레이저 무기 시스템(7)에 의해 구현된다. 방어 수단(3)은, 이러한 가열을 더 양호하게 검출할 수 있으며, 그리고 이를 위한 IR 탐지 헤드를 구비한다.

9. 发明专利

JP5209288B2 Target tracking guidance system and method 有权
公开(公告)号：JP5209288B2
公开(公告)日：2013-06-12
申请号：JP2007322143
申请日：2007-12-13
申请人：株式会社Ihiエアロスペース
发明人：正之石塚 , 直浩田中 , 卓郎中島 , 康志森田
IPC分类号： F41G7/22 , G01S1/70 , G01S13/88 , G01S17/66
CPC分类号： F41G7/2293 , F41G7/226

10. 发明专利

JP2011133165A Device and method for controlling flight of passive type missile 审中-公开
标题翻译：用于控制被动型飞行器的装置和方法
公开(公告)号：JP2011133165A
公开(公告)日：2011-07-07
申请号：JP2009292500
申请日：2009-12-24
申请人： Mitsubishi Electric Corp , 三菱電機株式会社
发明人： MORITA SHINICHI , MANIWA HISAKAZU , TAKAHASHI RYUHEI , OKAMURA ATSUSHI
IPC分类号： F41G7/22 , F42B10/60 , F42B15/01 , G01S13/46 , G01S13/88 , G01S13/94
CPC分类号： F41G7/2286 , F41G7/226
摘要： PROBLEM TO BE SOLVED: To improve positioning accuracy in a passive type missile observing TDOA and FDOA and passively positioning a target position. SOLUTION: This passive type missile flight control device observes the TDOA and FDOA by receiving both scattered waves irradiated from a known transmission source, made to hit a target and scattered and direct waves directly coming from the known transmission source, and includes a flight control part (14) positioning the target without irradiating electric waves and controlling its own flight route toward the target. The passive type missile flight control device further includes a GDOP calculating part (18) calculating GDOP based on the geometric arrangement of the missile, the transmission source and the target, estimating the orthogonal degree of ISO-TDOA and ISO-FDOA and generating a quantitative determination index of current measurement errors by the missile. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：提高无源式导弹观测TDOA和FDOA的定位精度，并对目标位置进行被动定位。解决方案：该被动型导弹飞行控制装置通过接收从已知的发射源照射的散射波，被瞄准目标，并且分散和直接来自已知的传输源的直接波，观察到TDOA和FDOA，并且包括飞行控制部分（14）定位目标而不照射电波并且控制其自己的朝向目标的飞行路线。被动型导弹飞行控制装置还包括基于导弹，发射源和目标的几何布置计算GDOP的GDOP计算部分（18），估计ISO-TDOA和ISO-FDOA的正交程度并产生定量导弹当前测量误差的确定指标。版权所有（C）2011，JPO＆INPIT

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