CN1329742C - Laser radar control method based on image intensifier - Google Patents
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Abstract
本发明公开了一种基于像增强器的激光雷达控制方法,采用像增强器做为探测器,得到激光回波的图象,用来反演大气信息。通过耦合在像增强器的CCD相机采集视频信号,通过同步分离,处理后触发激光器发光,由光电二极管检测出光时间并触发延时器,延时信号通过脉宽发生器产生脉冲信号,触发像增强器工作。基于像增强器的激光雷达控制方法可以胜任多数采用带有开门时间控制的图象传感器的激光雷达的控制,控制精度较高,具有实用价值。
The invention discloses a laser radar control method based on an image intensifier. The image intensifier is used as a detector to obtain laser echo images for reversing atmospheric information. The video signal is collected by the CCD camera coupled to the image intensifier, and the laser is triggered to emit light after processing through synchronous separation. The photodiode detects the light time and triggers the delayer. The delayed signal generates a pulse signal through the pulse width generator to trigger image enhancement. machine work. The laser radar control method based on the image intensifier can be competent for the control of most laser radars using image sensors with door opening time control, the control accuracy is high, and it has practical value.
Description
技术领域technical field
本发明涉及光学环境监测及电子学领域,具体是一种基于像增强器的激光雷达控制方法。The invention relates to the fields of optical environment monitoring and electronics, in particular to a laser radar control method based on an image intensifier.
背景技术Background technique
激光雷达是测量大气参数的重要手段,为了得到不同高度的大气信息,需要对不同距离的激光回波进行探测,传统激光雷达是基于光电倍增管或光子计数器作为探测器的,因此控制系统只要对出光时间进行检测,再延时适当时间(不要求特别精确),打开倍增管或光子计数器,即可得到所需信息。但这种雷达所能得到的信息不能完全满足需要。Lidar is an important means of measuring atmospheric parameters. In order to obtain atmospheric information at different heights, it is necessary to detect laser echoes at different distances. Traditional Lidar is based on photomultiplier tubes or photon counters as detectors. Therefore, the control system only needs to The light emission time is detected, and then delayed for an appropriate time (no special accuracy is required), and the multiplier tube or photon counter is turned on to obtain the required information. However, the information obtained by this radar cannot fully meet the needs.
发明内容Contents of the invention
为了解决上述方案出现的问题,采取精确延时,利用激光传输的速度与时间的乘积得到所要的距离,采用精确的像增强器开门时间与光速的乘积得到所要的光柱长度,通过一系列精确控制延时时间和开门时间,对大气进行若干分层剖面观测,再通过对数据的分析,得到大气的剖面信息。为了达到上述目的,延时时间和开门时间精度至少要达到10纳秒量级(对应的距离或气柱长度的精度为1.5米)。像增强器必须外加CCD相机,所以存在同步问题,即图像不能出现在CCD相机的消隐时刻,否则得不到图像,所以,整个系统的工作时序必须接受CCD同步信号的控制。In order to solve the problems of the above-mentioned schemes, precise time delay is adopted, the desired distance is obtained by the product of the laser transmission speed and time, and the desired beam length is obtained by the product of the precise opening time of the image intensifier and the speed of light, through a series of precise control Delay time and door opening time, conduct several layered profile observations on the atmosphere, and then obtain atmospheric profile information through data analysis. In order to achieve the above-mentioned purpose, the delay time and door opening time accuracy must reach at least 10 nanoseconds (the corresponding distance or air column length accuracy is 1.5 meters). The image intensifier must be equipped with a CCD camera, so there is a synchronization problem, that is, the image cannot appear at the blanking moment of the CCD camera, otherwise the image cannot be obtained, so the working timing of the entire system must be controlled by the CCD synchronization signal.
本发明的技术方案如下:Technical scheme of the present invention is as follows:
基于像增强器的激光雷达控制方法,其特征在于:Based on the laser radar control method of image intensifier, it is characterized in that:
将像增强器放置在接收望远镜焦点处,通过中继透镜耦合方式将像增强器与CCD相机进行耦合,CCD器件采集并输出的视频信号,分为两路:一路送给计算机采集,一路输入同步分离器进行同步分离,输出奇偶场同步信号,此奇偶场同步信号输入单稳态电路后输出窄脉冲信号,此窄脉冲信号输入缓冲器后输出缓冲信号,缓冲信号送入激光器的外触发器,激光器受触发出光;在激光器出口,由PIN光电二极管检测出光时刻,输出出光信号,出光信号输入射极跟随器进行缓冲,输出标准TTL电平,触发可编程延时器,由可编程延时器输出触发信号触发可编程脉宽发生器,可编程脉宽发生器产生脉冲信号,此脉冲信号输入至功率驱动部分后,输出驱动信号触发像增强器工作。Place the image intensifier at the focal point of the receiving telescope, and couple the image intensifier with the CCD camera through the relay lens coupling method. The video signal collected and output by the CCD device is divided into two channels: one is sent to the computer for collection, and the other is input synchronously The splitter performs synchronous separation and outputs the odd-even field synchronous signal. The odd-even field synchronous signal is input into the monostable circuit and outputs a narrow pulse signal. The narrow pulse signal is input into the buffer and then outputs a buffer signal. The buffer signal is sent to the external trigger of the laser. The laser is triggered to emit light; at the exit of the laser, the PIN photodiode detects the moment of light emission, and outputs the light signal, which is input to the emitter follower for buffering, outputs standard TTL level, triggers the programmable delayer, and the programmable delayer The output trigger signal triggers the programmable pulse width generator, and the programmable pulse width generator generates a pulse signal. After the pulse signal is input to the power drive part, the output drive signal triggers the image intensifier to work.
同步分离器所用芯片是LM1881;激光器是可外触发的YAG脉冲激光器,重复频率25Hz;单稳态电路所用芯片是74ls123;PIN光电二极管为高速硅PIN光电二极管。The chip used in the synchronous separator is LM1881; the laser is an externally triggered YAG pulse laser with a repetition rate of 25 Hz; the chip used in the monostable circuit is 74ls123; the PIN photodiode is a high-speed silicon PIN photodiode.
单稳态电路后输出窄脉冲信号脉宽为9-11微秒。After the monostable circuit outputs a narrow pulse signal, the pulse width is 9-11 microseconds.
本发明的效果Effect of the present invention
基于像增强器的激光雷达控制方法可以胜任多数采用带有开门时间控制的图象传感器的激光雷达的控制,控制精度较高,具有实用价值。The laser radar control method based on the image intensifier can be competent for the control of most laser radars using image sensors with door opening time control, the control accuracy is high, and it has practical value.
附图说明Description of drawings
图1是本发明的控制方法原理方框图。Fig. 1 is a schematic block diagram of the control method of the present invention.
图2是本发明的控制系统方框图。Fig. 2 is a block diagram of the control system of the present invention.
图3是本发明的时序发生器模块方框图。Fig. 3 is a block diagram of the timing generator module of the present invention.
图4是本发明的单片机部分电路原理图。Fig. 4 is a schematic diagram of a part of the circuit of the single-chip microcomputer of the present invention.
图5是本发明的延时部分电路原理图。Fig. 5 is a circuit schematic diagram of the delay part of the present invention.
具体实施方式Detailed ways
参见图1-5,将像增强器放置在接收望远镜焦点处,通过中继透镜耦合方式将像增强器与CCD相机进行耦合,CCD器件采集并输出的视频信号,分为两路:一路送给计算机采集,一路输入同步分离器LM1881进行同步分离,输出奇偶场同步信号,此奇偶场同步信号输入单稳态电路74ls123后输出脉宽为9-11微秒窄脉冲信号,此窄脉冲信号输入缓冲器后输出缓冲信号,缓冲信号送入激光器的外触发器,激光器受触发出光;激光器是可外触发的YAG脉冲激光器,重复频率25Hz;在激光器出口,由高速硅PIN光电二极管检测出光时刻,输出出光信号,出光信号输入射极跟随器进行缓冲,输出标准TTL电平,触发可编程延时器,由可编程延时器输出触发信号触发可编程脉宽发生器,可编程脉宽发生器产生脉冲信号,此脉冲信号输入至功率驱动部分后,输出驱动信号触发像增强器工作。Refer to Figure 1-5, place the image intensifier at the focal point of the receiving telescope, couple the image intensifier with the CCD camera through the relay lens coupling method, the video signal collected and output by the CCD device is divided into two channels: one is sent to Computer acquisition, one input synchronous separator LM1881 for synchronous separation, output odd and even field synchronous signal, this odd and even field synchronous signal is input into the monostable circuit 74ls123 and then output a narrow pulse signal with a pulse width of 9-11 microseconds, this narrow pulse signal is input into the buffer The buffered signal is output after the laser, and the buffered signal is sent to the external trigger of the laser, and the laser is triggered to emit light; the laser is a YAG pulse laser that can be triggered externally, and the repetition frequency is 25Hz; at the exit of the laser, the high-speed silicon PIN photodiode detects the moment of light output, and outputs The optical signal, the optical signal is input to the emitter follower for buffering, the output standard TTL level, triggers the programmable delayer, the programmable delayer outputs the trigger signal to trigger the programmable pulse width generator, and the programmable pulse width generator generates Pulse signal, after the pulse signal is input to the power drive part, the output drive signal triggers the work of the image intensifier.
像增强器通过圆筒直接与接收望远镜连接,使像增强器的光敏面处于像增强器焦平面即可。中继光路包括两个调整光束方向的反射镜和一个发散系统。激光光束经过一个发散系统直接入射到望远镜次镜。发散系统可以是负透镜也可以是正透镜。The image intensifier is directly connected to the receiving telescope through the cylinder, so that the photosensitive surface of the image intensifier is in the focal plane of the image intensifier. The relay optical path includes two mirrors to adjust the beam direction and a diverging system. The laser beam is directly incident on the secondary mirror of the telescope through a diverging system. Diverging systems can be either negative or positive lenses.
计算机与单片机通过并口进行数据通讯,单片机将计算机传输的指令转化为各执行机构的驱动信号,锁存器将数据锁存于可预置计数器的预置端。在系统焦距由远到近或由近到远的扫描过程中,计算机按预先射定的数据发出数据到单片机,经单片机处理后形成步进电机的脉冲信号,提供给步进电机驱动器,控制调焦电机工作。The computer and the single-chip microcomputer carry out data communication through the parallel port. The single-chip microcomputer converts the instructions transmitted by the computer into the driving signals of each actuator, and the latch stores the data in the preset end of the preset counter. During the scanning process of the focal length of the system from far to near or from near to far, the computer sends data to the single-chip microcomputer according to the pre-set data, and the pulse signal of the stepping motor is formed after processing by the single-chip microcomputer, which is provided to the stepping motor driver to control the adjustment. The coke motor works.
发射和接收望远镜均为口径350mm的卡式天文望远镜。像增强器是日本滨松公司的高速闸门像增强器,型号为C7609。CCD相机选用普通高分辨率黑白CCD。单片机采用microchip公司的PIC16C74,锁存器采用3片74LS373,组成延时器和脉冲发生器的基本计数单元共采用2片74F163和5片74ls191高速可预置计数器,计数时钟100MHz,时间精度达到5nS。延时范围为0.5μS-200μS,脉宽调节范围为100nS-10μS延时和脉宽发生器(时序发生器)。Both the transmitting and receiving telescopes are card-type astronomical telescopes with an aperture of 350mm. The image intensifier is a high-speed gate image intensifier produced by Japan Hamamatsu Company, the model is C7609. The CCD camera uses a common high-resolution black and white CCD. The single-chip microcomputer adopts PIC16C74 of microchip company, the latch adopts three pieces of 74LS373, and the basic counting unit of the delayer and pulse generator adopts two pieces of 74F163 and five pieces of 74ls191 high-speed preset counters, the counting clock is 100MHz, and the time accuracy reaches 5nS . The delay range is 0.5μS-200μS, the pulse width adjustment range is 100nS-10μS delay and pulse width generator (timing generator).
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|---|---|---|---|---|
| CN100462737C (en) * | 2006-06-29 | 2009-02-18 | 哈尔滨工业大学 | Range-gated laser 3D imaging radar system |
| CN100443920C (en) * | 2006-06-29 | 2008-12-17 | 哈尔滨工业大学 | Gain Modulated Pulsed Imaging LiDAR System |
| CN103135102A (en) * | 2013-02-02 | 2013-06-05 | 中国科学院安徽光学精密机械研究所 | Laser radar system with function of inhibiting low-altitude strong echo signals |
| CN104931974A (en) * | 2015-06-15 | 2015-09-23 | 中国科学院上海光学精密机械研究所 | Light source modulation and demodulation-based ICMOS high-speed 3D imaging laser radar |
| CN106527262A (en) * | 2016-11-04 | 2017-03-22 | 合肥天讯亿达光电技术有限公司 | Single wavelength laser radar monitoring system |
| CN109932729A (en) * | 2019-04-19 | 2019-06-25 | 北京瑞特森传感科技有限公司 | Face battle array laser radar |
| CN113702005A (en) * | 2021-08-31 | 2021-11-26 | 中国科学院合肥物质科学研究院 | Synchronous signal measuring device of Q-switched laser |
| CN114895288B (en) * | 2022-05-10 | 2022-11-15 | 哈尔滨方聚科技发展有限公司 | Laser echo generation system for three-dimensional scene |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1233759A (en) * | 1998-04-24 | 1999-11-03 | 中国科学院上海光学精密机械研究所 | Incoherent laser radar system for detecting atmosphere |
| WO2000077540A1 (en) * | 1999-06-11 | 2000-12-21 | Raytheon Company | Method and device for identifying an object and determining its location |
| CN1340698A (en) * | 2000-08-24 | 2002-03-20 | 中国科学院大气物理研究所 | Overall structure system for multi-wavelength laser radar with discrete units |
| CN1340721A (en) * | 2000-08-24 | 2002-03-20 | 中国科学院大气物理研究所 | Programmable laser trigger controller for multi-wavelength laser radar |
| CN1340700A (en) * | 2000-08-24 | 2002-03-20 | 中国科学院大气物理研究所 | Measuring and control system using network technique for multi-wavelength laser radar |
| CN1340702A (en) * | 2000-08-24 | 2002-03-20 | 中国科学院大气物理研究所 | Program controllable optical gate for multi-wavelength laser radar and its control method |
| EP1441236A1 (en) * | 2003-01-21 | 2004-07-28 | Rosemount Aerospace Inc. | System for profiling objects on terrain forward and below an aircraft utilizing a cross-track scanning laser altimeter |
-
2004
- 2004-09-30 CN CNB2004100648237A patent/CN1329742C/en not_active Expired - Fee Related
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1233759A (en) * | 1998-04-24 | 1999-11-03 | 中国科学院上海光学精密机械研究所 | Incoherent laser radar system for detecting atmosphere |
| WO2000077540A1 (en) * | 1999-06-11 | 2000-12-21 | Raytheon Company | Method and device for identifying an object and determining its location |
| CN1340698A (en) * | 2000-08-24 | 2002-03-20 | 中国科学院大气物理研究所 | Overall structure system for multi-wavelength laser radar with discrete units |
| CN1340721A (en) * | 2000-08-24 | 2002-03-20 | 中国科学院大气物理研究所 | Programmable laser trigger controller for multi-wavelength laser radar |
| CN1340700A (en) * | 2000-08-24 | 2002-03-20 | 中国科学院大气物理研究所 | Measuring and control system using network technique for multi-wavelength laser radar |
| CN1340702A (en) * | 2000-08-24 | 2002-03-20 | 中国科学院大气物理研究所 | Program controllable optical gate for multi-wavelength laser radar and its control method |
| EP1441236A1 (en) * | 2003-01-21 | 2004-07-28 | Rosemount Aerospace Inc. | System for profiling objects on terrain forward and below an aircraft utilizing a cross-track scanning laser altimeter |
Non-Patent Citations (4)
| Title |
|---|
| ICCD相机建模与仿真分析 王晓峰,刘扬,徐德坤,谭吉春,红外与激光工程,第32卷第6期 2003 * |
| ICCD相机建模与仿真分析 王晓峰,刘扬,徐德坤,谭吉春,红外与激光工程,第32卷第6期 2003;基于射线像增强器和视频相机的数字成像检测系统研制 称耀瑜,韩焱,王明泉,潘德恒,华北工学院测试技术学报,第15卷第4期 2001;无扫描三维激光雷达的研究 严惠民,倪旭翔,陈奇霖,陆祖康,中国激光,第27卷第9期 2000 * |
| 基于射线像增强器和视频相机的数字成像检测系统研制 称耀瑜,韩焱,王明泉,潘德恒,华北工学院测试技术学报,第15卷第4期 2001 * |
| 无扫描三维激光雷达的研究 严惠民,倪旭翔,陈奇霖,陆祖康,中国激光,第27卷第9期 2000 * |
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