CN104570346A - Long-wave infrared optical imaging system for image stabilization indirectly based on image spaces - Google Patents
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Abstract
一种基于像方间接稳像的长波红外光学成像系统,属于光学制导领域。针对现有用于跟踪及稳像的三轴稳定平台体积较大,无法满足超音速导引头系统对窗口小型化的要求,所述系统沿光路传播方向依次设置有望远光学镜组、摆镜、成像光学镜组和探测器;所述望远光学镜组与成像光学镜组的光轴相交,中间通过摆镜进行光路对接,摆镜在旋转机构的带动下在航向、俯仰两个方向进行摆动,将望远光学镜组视场范围内的光束反射至成像光学镜组,经成像光学镜组汇聚至探测器上生成红外图像。本发明提供的长波红外光学成像系统可以在满足系统小型化的同时,实现系统对目标的大视场搜索与小视场跟踪的功能。
The invention relates to a long-wave infrared optical imaging system based on image-side indirect image stabilization, which belongs to the field of optical guidance. In view of the large size of the existing three-axis stabilization platform used for tracking and image stabilization, which cannot meet the requirements of the supersonic seeker system for the miniaturization of the window, the system is sequentially equipped with a telescopic optical lens group, an oscillating mirror, Imaging optical mirror group and detector; the telescopic optical mirror group intersects with the optical axis of the imaging optical mirror group, and the optical path is connected through the swing mirror in the middle, and the swing mirror is driven by the rotating mechanism to swing in two directions of heading and pitching , reflecting the light beam within the field of view of the telescopic optical mirror group to the imaging optical mirror group, and converging on the detector through the imaging optical mirror group to generate an infrared image. The long-wave infrared optical imaging system provided by the present invention can realize the functions of the system to search for a target in a large field of view and track in a small field of view while satisfying the miniaturization of the system.
Description
技术领域technical field
本发明属于光学制导技术领域,涉及一种长波红外光学成像系统,具体涉及一种基于像方间接稳像的长波红外光学成像系统。The invention belongs to the technical field of optical guidance, and relates to a long-wave infrared optical imaging system, in particular to a long-wave infrared optical imaging system based on image-side indirect image stabilization.
背景技术Background technique
红外成像制导系统是超音速导引头的重要组成部分,具有制导精度高、抗干扰能力强、全天候工作等优点,是当今世界各国军事发展的重点研究对象。小型化的超音速导引头有利于提高制导武器的机动能力,增大弹头的有效载荷,增强武器的杀伤力,对未来军事战争的发展具有重要作用。因此,在保证红外成像制导系统小型化的同时如何实现该系统大视场搜索与小视场跟踪的功能成为当今制导武器发展的重点之一。The infrared imaging guidance system is an important part of the supersonic seeker. It has the advantages of high guidance precision, strong anti-interference ability, and all-weather work. It is the key research object of military development in various countries in the world today. The miniaturized supersonic seeker is conducive to improving the maneuverability of guided weapons, increasing the payload of warheads, and enhancing the lethality of weapons, which will play an important role in the development of future military warfare. Therefore, how to realize the functions of large field of view search and small field of view tracking while ensuring the miniaturization of the infrared imaging guidance system has become one of the key points in the development of guided weapons today.
如图1所示,传统的三轴伺服稳定系统包括横滚框架1、俯仰框架2、方位框架3和红外热像仪4,其中横滚框架1沿Z轴方向安装在基座上,绕Z轴旋转;俯仰框架2沿X轴安装在横滚框架1上,绕X轴旋转;方位框架3沿Y轴安装在俯仰框架2上,绕Y轴旋转,它们分别由一部直流无刷力矩电机驱动旋转。但是三个框架为外延叠加结构,且均为旋转运动装置,这使得三轴稳定平台系统体积较大,在要求窗口小型化的超音速导引头系统中难以安装使用。CN103760670A公开了一种含反射式空间光调制器的大视场扫描红外光学系统,该系统由双二次曲面校正板、消色差旋转雷斯莱棱镜对、分光棱镜、反射式空间光调制器等沿光轴依次排列组成,其中消色差旋转雷斯莱棱镜对可以进行大范围视场扫描,从而实现对目标的大视场搜索;分光棱镜可以对光路进行折转,从而可以减小光学系统体积。但是消色差旋转雷斯莱棱镜对是利用旋转实现大视场扫描搜索的,它无法根据已发现目标的位置调整其航向与俯仰角度,以使目标始终位于成像视场中心,故无法对目标进行小视场范围跟踪。所以,在满足系统小型化的同时如何实现系统大视场搜索和小视场跟踪成为红外成像制导系统研究的难点之一。As shown in Figure 1, a traditional three-axis servo stabilization system includes a roll frame 1, a pitch frame 2, an azimuth frame 3, and an infrared thermal imaging camera 4, wherein the roll frame 1 is installed on the base along the Z-axis direction, around the Z-axis The pitch frame 2 is installed on the roll frame 1 along the X axis and rotates around the X axis; the azimuth frame 3 is mounted on the pitch frame 2 along the Y axis and rotates around the Y axis. They are respectively driven by a DC brushless torque motor Drive rotation. However, the three frames are epitaxial superimposed structures, and they are all rotary motion devices, which makes the three-axis stabilized platform system bulky and difficult to install and use in supersonic seeker systems that require miniaturized windows. CN103760670A discloses a large-field-of-view scanning infrared optical system containing a reflective spatial light modulator. The system consists of a double quadric surface correction plate, an achromatic rotating Resley prism pair, a beam splitting prism, a reflective spatial light modulator, etc. Arranged in sequence along the optical axis, the achromatic rotating Resley prism pair can scan a wide range of field of view, thereby realizing a large field of view search for the target; the beam splitter prism can bend the optical path, thereby reducing the volume of the optical system . However, the achromatic rotating Resley prism pair uses rotation to realize a large field of view scanning search, and it cannot adjust its heading and pitch angles according to the position of the discovered target so that the target is always located in the center of the imaging field of view, so the target cannot be searched. Small field of view range tracking. Therefore, how to realize the system's large field of view search and small field of view tracking while satisfying the miniaturization of the system has become one of the difficulties in the research of infrared imaging guidance systems.
发明内容Contents of the invention
针对现有用于跟踪及稳像的三轴稳定平台体积较大,无法满足超音速导引头系统对窗口小型化的要求,本发明提供了一种基于像方间接稳像的长波红外光学成像系统,可以在满足系统小型化的同时,实现系统对目标的大视场搜索与小视场跟踪的功能。Aiming at the large size of the existing three-axis stabilization platform used for tracking and image stabilization, which cannot meet the miniaturization requirements of the supersonic seeker system, the present invention provides a long-wave infrared optical imaging system based on image-side indirect image stabilization , while satisfying the miniaturization of the system, the system can realize the functions of large field of view search and small field of view tracking for the target.
本发明的目的是通过以下技术方案实现的:The purpose of the present invention is achieved through the following technical solutions:
一种基于像方间接稳像的长波红外光学成像系统,沿光路传播方向依次设置有望远光学镜组、摆镜、成像光学镜组和探测器;所述望远光学镜组与成像光学镜组的光轴相交,中间通过摆镜进行光路对接,摆镜在旋转机构的带动下在航向、俯仰两个方向进行摆动,将望远光学镜组视场范围内的光束反射至成像光学镜组,经成像光学镜组汇聚至探测器上生成红外图像。A long-wave infrared optical imaging system based on image-side indirect image stabilization, in which a telescopic optical mirror group, a swing mirror, an imaging optical mirror group, and a detector are sequentially arranged along the propagation direction of the optical path; the telescopic optical mirror group and the imaging optical mirror group The optical axes of the optical axes intersect, and the optical path is connected through the swing mirror in the middle. The swing mirror swings in the two directions of heading and pitch under the drive of the rotating mechanism, and reflects the beam within the field of view of the telescopic optical mirror group to the imaging optical mirror group. The infrared image is generated by converging on the detector through the imaging optical mirror group.
现有用于跟踪及稳像的三轴稳定平台体积较大,无法满足导引头系统对窗口小型化的要求。相比于现有的用于跟踪及稳像的三轴稳定平台,本发明具有如下有益效果:The existing three-axis stabilization platform used for tracking and image stabilization is too large to meet the requirements of the seeker system for the miniaturization of the window. Compared with the existing three-axis stabilized platform for tracking and image stabilization, the present invention has the following beneficial effects:
(1)远光学镜组与成像光学镜组的光轴相交并有一定夹角,中间通过摆镜进行光路对接,这样能够满足系统小型化的要求;(1) The optical axes of the far optical lens group and the imaging optical lens group intersect and have a certain angle, and the optical path is connected through the swing mirror in the middle, which can meet the requirements of system miniaturization;
(2)摆镜在航向与俯仰方向进行摆动,实现对目标的大视场扫描搜索;发现目标后则在伺服控制系统的控制下根据弹体姿态不断调整其航向与俯仰角度,以使目标始终位于成像光学镜组的视场中心,从而实现对目标的小视场跟踪功能。(2) The oscillating mirror swings in the heading and pitching directions to realize the large field of view scanning search for the target; after the target is found, under the control of the servo control system, the heading and pitching angle are continuously adjusted according to the attitude of the projectile, so that the target is always It is located in the center of the field of view of the imaging optical mirror group, so as to realize the small field of view tracking function of the target.
(3)成像光学镜组采用二次成像光路结构,并在光路中加入反射镜折叠光路,以使系统外形尺寸满足小型化。(3) The imaging optical mirror group adopts a secondary imaging optical path structure, and a mirror is added to the optical path to fold the optical path, so that the system size can be miniaturized.
附图说明Description of drawings
图1是传统的伺服稳定系统结构图;Fig. 1 is a structural diagram of a traditional servo stabilization system;
图2是长波红外光学成像系统的结构图;Fig. 2 is a structural diagram of a long-wave infrared optical imaging system;
图3是长波红外光学成像系统的光路原理图;Fig. 3 is a schematic diagram of the optical path of the long-wave infrared optical imaging system;
图4是望远光学镜组与成像光学镜组的视场比较图。Fig. 4 is a comparison diagram of the field of view between the telescopic optical lens group and the imaging optical lens group.
具体实施方式Detailed ways
下面结合附图对本发明的技术方案作进一步的说明,但并不局限于此,凡是对本发明技术方案进行修改或者等同替换,而不脱离本发明技术方案的精神和范围,均应涵盖在本发明的保护范围中。The technical solution of the present invention will be further described below in conjunction with the accompanying drawings, but it is not limited thereto. Any modification or equivalent replacement of the technical solution of the present invention without departing from the spirit and scope of the technical solution of the present invention should be covered by the present invention. within the scope of protection.
长波红外光学成像系统是超音速导引头的重要组成部分,它的结构如图2所示,由窗口5、望远光学镜组6、摆镜7、成像光学镜组8和探测器9组成。望远光学镜组6与成像光学镜组8相对窗口5位置保持不变,它们的光轴相交且夹角为104°,中间通过摆镜7进行光路对接,从而可以满足系统小型化的要求。The long-wave infrared optical imaging system is an important part of the supersonic seeker. Its structure is shown in Figure 2. It consists of a window 5, a telescopic optical mirror group 6, a swing mirror 7, an imaging optical mirror group 8 and a detector 9. . The positions of the telescopic optical lens group 6 and the imaging optical lens group 8 relative to the window 5 remain unchanged, their optical axes intersect and the angle is 104°, and the optical path is connected through the swing mirror 7 in the middle, so as to meet the requirements of system miniaturization.
望远光学镜组6包括第一曲面反射镜15、第二曲面反射镜16和望远镜组14,其中望远镜组14由第一透镜14-1、第二透镜14-2、第三透镜14-3和第四透镜14-4组成。望远光学镜组6是一个大视场光学系统,其视场为26.25°×28°(航向×俯仰),覆盖了跟踪视场范围。望远光学镜组6为一个望远系统,它能将跟踪视场范围内接收到的光束以平行光形式投射到摆镜7位置。望远光学镜组6的入瞳靠近窗口5,这样不仅可以减小窗口5的尺寸,还不会产生光线遮挡。The telescopic optical mirror group 6 comprises the first curved reflector 15, the second curved reflector 16 and the telescope group 14, wherein the telescope group 14 consists of the first lens 14-1, the second lens 14-2, the third lens 14-3 and the fourth lens 14-4. The telescopic optical lens group 6 is a large field of view optical system, and its field of view is 26.25°×28° (heading×pitch), covering the range of the tracking field of view. The telescopic optical lens group 6 is a telescopic system, which can project the light beam received in the tracking field of view to the position of the swing mirror 7 in the form of parallel light. The entrance pupil of the telescopic optical lens group 6 is close to the window 5, so that not only can the size of the window 5 be reduced, but also light blocking will not occur.
成像光学镜组8包括第一成像镜组10、反射镜11和第二成像镜组12,其中第一成像镜组10由第五透镜10-1和第六透镜10-2组成,第二成像镜组12由第七透镜12-1、第八透镜12-2和第九透镜12-3组成;成像光学镜组8采用二次成像的光路结构,并在光路中加入反射镜以使光路发生偏转,从而使系统外形尺寸满足小型化的要求。成像光学镜组8为小视场光学系统,其视场为6.25°×5°(航向×俯仰)。它通过摆镜7的二维摆动完成对望远光学镜组6大视场的扫描搜索,发现目标后则对目标进行小视场跟踪成像。The imaging optical mirror group 8 includes a first imaging mirror group 10, a mirror 11 and a second imaging mirror group 12, wherein the first imaging mirror group 10 is composed of a fifth lens 10-1 and a sixth lens 10-2, and the second imaging mirror group 10 is composed of a fifth lens 10-1 and a sixth lens 10-2. Mirror group 12 is made up of the 7th lens 12-1, the 8th lens 12-2 and the 9th lens 12-3; Imaging optics mirror group 8 adopts the optical path structure of secondary imaging, and adds mirror in the optical path to make the optical path occur deflection, so that the system dimensions meet the requirements of miniaturization. The imaging optical mirror group 8 is a small field of view optical system, and its field of view is 6.25°×5° (heading×pitch). It scans and searches the 6 large fields of view of the telescopic optical lens group through the two-dimensional swing of the oscillating mirror 7, and performs tracking and imaging of the target in a small field of view after the target is found.
摆镜7位于望远光学镜组6与成像光学镜组8之间,其在方位方向和俯仰方向的旋转角度分别为±5°和±12°。摆镜7的安装方式为摆镜反射面法线与望远光学镜组6光轴在航向方向上夹角为52°,俯仰方向夹角为0°,这样能够满足系统小型化的要求。望远光学镜组6的出瞳与成像光学镜组8的入瞳应耦合在摆镜7位置,这样不仅可以满足摆镜外形尺寸小型化的要求,还可以避免摆镜7摆动带来的成像质量影响。摆镜7在旋转机构的带动下可在航向、俯仰两个方向进行摆动,从而将望远光学镜组6视场范围内的光束反射至成像光学镜组8,实现对目标的大视场搜索与小视场跟踪。The swing mirror 7 is located between the telescopic optical lens group 6 and the imaging optical lens group 8, and its rotation angles in the azimuth direction and the pitch direction are ±5° and ±12° respectively. The installation method of the oscillating mirror 7 is that the included angle between the normal line of the oscillating mirror reflection surface and the optical axis of the telescopic optical mirror group 6 is 52° in the heading direction, and 0° in the pitching direction, which can meet the requirements of system miniaturization. The exit pupil of the telescopic optical mirror group 6 and the entrance pupil of the imaging optical mirror group 8 should be coupled at the position of the oscillating mirror 7, which can not only meet the requirement of miniaturization of the oscillating mirror size, but also avoid the imaging caused by the oscillating mirror 7 quality impact. Driven by the rotating mechanism, the swinging mirror 7 can swing in two directions of heading and pitching, so as to reflect the light beam within the field of view of the telescopic optical mirror group 6 to the imaging optical mirror group 8, so as to realize the large field of view search for the target Tracking with a small field of view.
如图3所示,长波红外光学成像系统的工作过程为:As shown in Figure 3, the working process of the long-wave infrared optical imaging system is:
望远光学镜组6接收物方视场范围内景物发出的光束。在望远光学镜组6内光束先后通过第一曲面反射镜15和第二曲面反射镜16的连续反射后进入望远镜组14,经望远镜组14准直后以平行光形式投射到摆镜7位置。摆镜7将望远光学镜组6视场内的光束反射至成像光学镜组8。在成像光学镜组8内光束通过第一成像镜组10的透射后入射至反射镜11上,该反射镜11能够使进入成像光学镜组8中的光束发生光路偏转,以此满足系统小型化的要求。偏转后的光束再通过第二成像镜组12后最终汇聚至探测器光敏面13上生成红外图像,从而实现对目标的大视场搜索和小视场跟踪功能。The telescopic optical lens group 6 receives the light beam emitted by the scene in the field of view of the object side. In the telescopic optical mirror group 6, the light beam successively passes through the continuous reflection of the first curved reflector 15 and the second curved reflector 16 and then enters the telescope group 14. After being collimated by the telescope group 14, it is projected to the position of the swing mirror 7 in the form of parallel light. The swinging mirror 7 reflects the light beam in the field of view of the telescopic optical lens group 6 to the imaging optical lens group 8 . In the imaging optical mirror group 8, the light beam is transmitted through the first imaging mirror group 10 and then incident on the mirror 11. The mirror 11 can deflect the optical path of the beam entering the imaging optical mirror group 8, so as to meet the miniaturization of the system. requirements. The deflected light beam passes through the second imaging mirror group 12 and finally converges on the photosensitive surface 13 of the detector to generate an infrared image, thereby realizing the functions of searching for a large field of view and tracking a target in a small field of view.
在上述工作过程中,由于望远光学镜组视场17属于大视场(26.25°×28°)光学系统,成像光学镜组视场18属于小视场(6.25°×5°)光学系统,这导致成像光学镜组的视场无法充满望远光学镜组的整个视场,如图4所示。因此,为了实现对目标的大视场搜索,摆镜7应在航向、俯仰两个方向进行摆动,从而将望远光学镜组6不同视场内的光束反射至成像光学镜组8。发现目标后摆镜7则在伺服控制系统的控制下根据弹体姿态不断调整其在航向和俯仰方向上的倾斜角度,以使目标始终位于成像光学镜组的视场中心,从而实现对目标的小视场跟踪。In the above-mentioned working process, since the field of view 17 of the telescopic optical lens group belongs to the large field of view (26.25°×28°) optical system, and the field of view 18 of the imaging optical lens group belongs to the small field of view (6.25°×5°) optical system, this As a result, the field of view of the imaging optical lens group cannot fill the entire field of view of the telescopic optical lens group, as shown in FIG. 4 . Therefore, in order to achieve a large field of view search for the target, the oscillating mirror 7 should swing in the two directions of heading and pitching, so as to reflect the light beams in different fields of view of the telescopic optical mirror group 6 to the imaging optical mirror group 8 . When the target is found, the swing mirror 7 is under the control of the servo control system to continuously adjust its inclination angle in the heading and pitching directions according to the attitude of the projectile, so that the target is always located in the center of the field of view of the imaging optical mirror group, so as to realize the accuracy of the target. Small field of view tracking.
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CN106488149A (en) * | 2016-09-30 | 2017-03-08 | 哈尔滨工业大学 | A kind of image enhaucament optical system integrating steady picture based on image space scanner uni |
CN109254392A (en) * | 2018-08-22 | 2019-01-22 | 哈尔滨新光光电科技有限公司 | A kind of miniaturization rolling-backstroke long wave refrigeration optical system |
CN109406112A (en) * | 2017-08-17 | 2019-03-01 | 北京遥感设备研究所 | A kind of head-shield optics side window light transmission ratio-dependent method |
CN111190282A (en) * | 2019-12-30 | 2020-05-22 | 哈尔滨新光光电科技股份有限公司 | Large-view-field transmission type high-energy laser emission system |
CN111998801A (en) * | 2020-08-19 | 2020-11-27 | 哈尔滨新光光电科技股份有限公司 | Roll pendulum formula two-dimensional imaging mechanism |
CN112068217A (en) * | 2020-09-30 | 2020-12-11 | 西安雷华测控技术有限公司 | Day and night detector for aircraft |
CN112505916A (en) * | 2020-10-30 | 2021-03-16 | 哈尔滨新光光电科技股份有限公司 | Image space scanning optical system based on curved surface prism |
CN112558272A (en) * | 2020-12-07 | 2021-03-26 | 中国电子科技集团公司第十一研究所 | Double-view-field scanning infrared optical system |
CN112596229A (en) * | 2020-12-16 | 2021-04-02 | 航天科工微电子系统研究院有限公司 | Large-caliber off-axis transmitting telescope optical system for directional transmitting equipment |
CN113783626A (en) * | 2021-08-24 | 2021-12-10 | 长春理工大学 | A communication receiving optical system of a UAV laser communication device |
CN118192035A (en) * | 2024-05-13 | 2024-06-14 | 长春通视光电技术股份有限公司 | Airborne dual-band common-aperture photoelectric load and imaging method |
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2015
- 2015-02-10 CN CN201510069394.0A patent/CN104570346A/en active Pending
Cited By (15)
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CN106488149A (en) * | 2016-09-30 | 2017-03-08 | 哈尔滨工业大学 | A kind of image enhaucament optical system integrating steady picture based on image space scanner uni |
CN109406112A (en) * | 2017-08-17 | 2019-03-01 | 北京遥感设备研究所 | A kind of head-shield optics side window light transmission ratio-dependent method |
CN109406112B (en) * | 2017-08-17 | 2020-08-18 | 北京遥感设备研究所 | Method for determining light transmission proportion of optical side window of hood |
CN109254392A (en) * | 2018-08-22 | 2019-01-22 | 哈尔滨新光光电科技有限公司 | A kind of miniaturization rolling-backstroke long wave refrigeration optical system |
CN109254392B (en) * | 2018-08-22 | 2019-06-14 | 哈尔滨新光光电科技有限公司 | A kind of miniaturization rolling-backstroke long wave refrigeration optical system |
CN111190282A (en) * | 2019-12-30 | 2020-05-22 | 哈尔滨新光光电科技股份有限公司 | Large-view-field transmission type high-energy laser emission system |
CN111998801A (en) * | 2020-08-19 | 2020-11-27 | 哈尔滨新光光电科技股份有限公司 | Roll pendulum formula two-dimensional imaging mechanism |
CN111998801B (en) * | 2020-08-19 | 2021-10-19 | 哈尔滨新光光电科技股份有限公司 | Roll pendulum formula two-dimensional imaging mechanism |
CN112068217A (en) * | 2020-09-30 | 2020-12-11 | 西安雷华测控技术有限公司 | Day and night detector for aircraft |
CN112505916A (en) * | 2020-10-30 | 2021-03-16 | 哈尔滨新光光电科技股份有限公司 | Image space scanning optical system based on curved surface prism |
CN112558272A (en) * | 2020-12-07 | 2021-03-26 | 中国电子科技集团公司第十一研究所 | Double-view-field scanning infrared optical system |
CN112596229A (en) * | 2020-12-16 | 2021-04-02 | 航天科工微电子系统研究院有限公司 | Large-caliber off-axis transmitting telescope optical system for directional transmitting equipment |
CN113783626A (en) * | 2021-08-24 | 2021-12-10 | 长春理工大学 | A communication receiving optical system of a UAV laser communication device |
CN118192035A (en) * | 2024-05-13 | 2024-06-14 | 长春通视光电技术股份有限公司 | Airborne dual-band common-aperture photoelectric load and imaging method |
CN118192035B (en) * | 2024-05-13 | 2024-07-09 | 长春通视光电技术股份有限公司 | Airborne dual-band common-aperture photoelectric load and imaging method |
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