CN101551457A - A construction method of forward looking linear array three-dimensional synthetic aperture radar system - Google Patents

A construction method of forward looking linear array three-dimensional synthetic aperture radar system Download PDF

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CN101551457A
CN101551457A CNA2009100591265A CN200910059126A CN101551457A CN 101551457 A CN101551457 A CN 101551457A CN A2009100591265 A CNA2009100591265 A CN A2009100591265A CN 200910059126 A CN200910059126 A CN 200910059126A CN 101551457 A CN101551457 A CN 101551457A
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linear array
synthetic aperture
aperture radar
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CN101551457B (en
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张晓玲
王银波
郭少南
韩云
钱忠清
李伟华
师君
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University of Electronic Science and Technology of China
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Abstract

本发明公开了一种前视线阵三维合成孔径雷达系统的构建方法,它是利用单激励线阵三维合成孔径雷达天线相位中心控制精度高和前视合成孔径雷达系统能够提前获取前方地形信息的特点,采用单激励线阵三维SAR系统和前视SAR系统相结合的模式,使单激励线阵三维SAR的波束前视照射。然后实时对接收到的回波数据我们采用标准的后向投影算法进行处理,得到前方测绘区域的三维成像结果。能够可以提前并实时的获取飞行器前方的三维地形信息,为精确制导以及飞行器的导航、进近着陆以及盲降提供了一种新方法。

Figure 200910059126

The invention discloses a construction method of a forward-looking three-dimensional synthetic aperture radar system, which utilizes the characteristics of high control precision of the single-excitation linear array three-dimensional synthetic aperture radar antenna phase center and the ability of the forward-looking synthetic aperture radar system to obtain terrain information ahead of time , using the mode of combining the single-excitation linear array 3D SAR system and the forward-looking SAR system, so that the beam of the single-excitation linear array 3D SAR is forward-looking. Then we use the standard back projection algorithm to process the received echo data in real time to obtain the three-dimensional imaging results of the front surveying and mapping area. The three-dimensional terrain information in front of the aircraft can be obtained in advance and in real time, which provides a new method for precise guidance and aircraft navigation, approach landing and blind landing.

Figure 200910059126

Description

一种前视线阵三维合成孔径雷达系统构建方法 A Construction Method of 3D Synthetic Aperture Radar System with Forward Line-of-Sight Array

技术领域: Technical field:

本技术发明属于雷达技术领域,它特别涉及了合成孔径雷达(SAR)成像技术领域。The technical invention belongs to the technical field of radar, and in particular relates to the technical field of synthetic aperture radar (SAR) imaging.

背景技术: Background technique:

合成孔径雷达(SAR)是一种高分辨率的微波成像系统,它依靠雷达和目标之间的相对运动来形成合成阵列来获得横向高分辨率,利用大带宽信号实现纵向高分辨率,而三维SAR是基于常规SAR横向维和纵向维的基础之上外加切横向维,它也是依靠雷达和目标之间的相对运动来获得切横向分辨率。三维成像是三维SAR区别于其他遥感成像系统的重要特征,由于其测绘时具有全天候、全天时、距离远等特点,在地形测绘、环境检测和灾害预报等方面具有不可替代的作用。Synthetic Aperture Radar (SAR) is a high-resolution microwave imaging system, which relies on the relative motion between the radar and the target to form a synthetic array to obtain horizontal high resolution, and uses large bandwidth signals to achieve vertical high resolution. SAR is based on the conventional SAR horizontal dimension and longitudinal dimension with an additional tangential horizontal dimension, and it also relies on the relative motion between the radar and the target to obtain the tangential horizontal resolution. 3D imaging is an important feature that distinguishes 3D SAR from other remote sensing imaging systems. Because of its all-weather, all-time, and long-distance characteristics, it plays an irreplaceable role in terrain mapping, environmental detection, and disaster forecasting.

前视SAR的出现使得SAR的应用范围得以扩展,目前对前视SAR做的比较出色的是德国宇航局(DLR),他们在1999年提出了一种能对飞行路线正前方扇形区域进行中/高分辨率成像的新型机载前视合成孔径雷达系统--“用于视景增强的新型区域成像雷达(SIREV)”,目前已完成了SIREV的理论研究、前视成像算法、计算机仿真与样机研制,并在DLR的E-SAR机载试验平台上进行飞行测试。在相关文献中对这个系统做了系统分析和描述。然而这种前视SAR只能得到二维的SAR图像,对地形的三维信息是无法获取的。The emergence of forward-looking SAR has expanded the application range of SAR. At present, the German Aerospace Agency (DLR) has done a good job in forward-looking SAR. A new type of airborne forward-looking synthetic aperture radar system for high-resolution imaging -- "New Area Imaging Radar for Vision Enhancement (SIREV)", the theoretical research, forward-looking imaging algorithm, computer simulation and prototype of SIREV have been completed so far Developed and flight tested on DLR's E-SAR airborne test platform. The system is analyzed and described in related literature. However, this kind of forward-looking SAR can only obtain two-dimensional SAR images, and the three-dimensional information of the terrain cannot be obtained.

我们这个前视三维SAR结合了三维SAR和前视SAR的优点,它除了具有三维SAR所起的作用外,由于波束是前视照射,能提前并实时的得知测绘地形信息,所以它还可以实现飞行器的导航与盲降,因此前视三维合成孔径雷达具有广阔的应用前景。Our forward-looking 3D SAR combines the advantages of 3D SAR and forward-looking SAR. In addition to the role played by 3D SAR, because the beam is forward-looking illumination, it can obtain surveying and mapping terrain information in advance and in real time, so it can also Realize the navigation and blind landing of the aircraft, so the forward-looking three-dimensional synthetic aperture radar has broad application prospects.

发明内容: Invention content:

本发明的目的是为了克服现有合成孔径雷达系统(简称SAR系统)不能实时获取前方三维地形信息的缺点,提供一种前视线阵三维合成孔径雷达系统(SAR系统)的构建方法。该系统采用线阵系统单阵元激励方式,波束前视照射,可以提前并实时的获取飞行器前方三维地形信息,为精确制导以及飞行器的导航、进近着陆以及盲降提供了一种新方法。The purpose of the present invention is to provide a method for constructing a forward line-of-sight array three-dimensional synthetic aperture radar system (SAR system) in order to overcome the shortcoming that the existing synthetic aperture radar system (SAR system for short) cannot obtain real-time three-dimensional terrain information ahead. The system adopts the single-array element excitation method of the linear array system, and the forward-looking beam can obtain the three-dimensional terrain information in front of the aircraft in advance and in real time, providing a new method for precise guidance, aircraft navigation, approach landing and blind landing.

为了方便描述本发明的内容,首先作以下术语定义:In order to describe content of the present invention conveniently, at first do following term definition:

定义1、线阵三维成像合成孔径雷达Definition 1. Linear array 3D imaging synthetic aperture radar

线阵三维成像合成孔径雷达是将线性阵列天线固定于运动平台上,结合运动平台的运动以合成二维平面阵列,并进行三维成像的一种合成孔径雷达系统。The linear array three-dimensional imaging synthetic aperture radar is a synthetic aperture radar system that fixes the linear array antenna on the moving platform, combines the movement of the moving platform to synthesize a two-dimensional planar array, and performs three-dimensional imaging.

定义2、单激励方式Definition 2. Single incentive mode

在一个飞行孔径内,对于固定在运动平台上的线性阵列天线,在每一个慢时间n,n=1……N,利用控制开关打开线阵天线中特定的某一个阵元来发射信号或者是接收回波。详细内容可参考文献:“APC Trajectory design for‘one-active’linear array 3-D imaging SAR”,Shi Jun等In a flight aperture, for a linear array antenna fixed on a moving platform, at each slow time n, n=1...N, use a control switch to turn on a specific array element in the linear array antenna to transmit signals or Receive echo. For details, please refer to the literature: "APC Trajectory design for'one-active'linear array 3-D imaging SAR", Shi Jun et al.

定义3、波束前视角Definition 3. Beam front angle of view

波束前视角是指合成孔径雷达波束中心与飞行器飞行速度方向之间的锐角夹角,一般地,飞行器沿直线飞行,因此波束角可认为是雷达波束中心与沿航迹直线之间夹角。当波束前视角为0°~20°时,称为大斜视,20°~90°称为小斜视。The beam front angle of view refers to the acute angle between the center of the synthetic aperture radar beam and the flight speed direction of the aircraft. Generally, the aircraft flies along a straight line, so the beam angle can be considered as the angle between the center of the radar beam and the straight line along the track. When the beam front angle of view is 0°-20°, it is called hypertropia, and when it is 20°-90°, it is called microstrabismus.

定义4、三维成像合成孔径雷达理论分辨率Definition 4. The theoretical resolution of 3D imaging SAR

三维合成孔径雷达理论分辨率是指根据三维合成孔径雷达系统参数,包括发射信号带宽,合成孔径长度以及线阵天线长度决定的三维合成孔径雷达所能达到的最大分辨率。详见文献“合成孔径雷达成像——算法与实现”,Frank H.Wong等编著,电子工业出版社出版。Theoretical resolution of 3D SAR refers to the maximum resolution that 3D SAR can achieve based on the parameters of the 3D SAR system, including the transmitted signal bandwidth, the length of the synthetic aperture and the length of the linear array antenna. For details, see the document "Synthetic Aperture Radar Imaging - Algorithm and Implementation", edited by Frank H. Wong et al., published by Electronic Industry Press.

定义5、标准后向投影算法Definition 5. Standard back projection algorithm

后向投影算法是基于匹配滤波原理的合成孔径雷达成像算法。详细内容可参考文献:“Research on A novel fast back projection algorithm for strip map bistaticSAR imaging”,Huang Yulin等The back projection algorithm is a synthetic aperture radar imaging algorithm based on the principle of matched filtering. For details, please refer to the literature: "Research on A novel fast back projection algorithm for strip map bistaticSAR imaging", Huang Yulin, etc.

定义6、发射/接收天线相位中心轨迹Definition 6. Transmitting/receiving antenna phase center locus

发射/接收天线相位中心轨迹是指不同脉冲重复周期内,前视线阵三维成像合成孔径雷达打开的发射/接收天线阵元位置所构成的轨迹,可看作服从某种分布的随机变量;The phase center trajectory of the transmitting/receiving antenna refers to the trajectory formed by the positions of the transmitting/receiving antenna elements opened by the forward line-of-sight array 3D imaging synthetic aperture radar in different pulse repetition periods, which can be regarded as a random variable that obeys a certain distribution;

定义7、合成孔径雷达发射机Definition 7. Synthetic Aperture Radar Transmitter

合成孔径雷达发射机是指目前合成孔径雷达采用的向观测区域发射电磁信号的系统,主要包括信号发生器、混频器、放大器等模块Synthetic aperture radar transmitter refers to the system used by synthetic aperture radar to transmit electromagnetic signals to the observation area, mainly including signal generators, mixers, amplifiers and other modules

定义8、合成孔径雷达接收机Definition 8. Synthetic Aperture Radar Receiver

合成孔径雷达接收机是指目前合成孔径雷达采用的接收观测区域回波的系统,主要包括混频器、放大器、模/数转换器、存储设备等。The synthetic aperture radar receiver refers to the system used by the current synthetic aperture radar to receive the echo of the observation area, mainly including mixers, amplifiers, analog/digital converters, storage devices, etc.

定义9、飞行孔径与慢时间Definition 9, flight aperture and slow time

双站线阵三维合成孔径雷达系统的飞行孔径是指对于测绘场景中的一个散射点从收发波束共同照射到开始到发射波束或接收波束任意一个照射不到结束收发波束中心所走过的距离。The flight aperture of the dual-station linear array 3D synthetic aperture radar system refers to the distance traveled by the center of the transmitting and receiving beam for a scattering point in the surveying and mapping scene from the common irradiation of the transmitting and receiving beams to the beginning to the end when either the transmitting beam or the receiving beam cannot be illuminated.

双站线阵三维合成孔径雷达系统的慢时间是指收发平台飞过一个飞行孔径所需要的时间,由于雷达以一定的重复周期Tr发射接收脉冲,慢时间可以表示为一个离散化的时间变量ts=nTr,n=1L N,N为一个飞行孔径内慢时间的离散个数,Tr为重复周期。The slow time of the dual station linear array 3D SAR system refers to the time required for the transceiver platform to fly through a flight aperture. Since the radar transmits and receives pulses with a certain repetition period Tr , the slow time can be expressed as a discretized time variable t s =nT r , n=1L N, N is the discrete number of slow times in a flight aperture, and T r is the repetition period.

本发明提供一种前视线阵三维合成孔径雷达系统的构建方法,它包括如下步骤:The invention provides a method for constructing a forward line-of-sight array three-dimensional synthetic aperture radar system, which comprises the following steps:

步骤1:发射系统和接收系统构建Step 1: Construction of transmitting system and receiving system

发射系统和接收系统包括:一台发射机,一台接收机,一个T/R转换开关,一个馈元控制开关,M条馈线和M个线阵馈元;M是自然数,M的大小由前视线阵三维合成孔径雷达系统在一个飞行孔径内脉冲重复频率的大小来决定,M=v×Na/L,其中,v为飞行平台速度,Na为合成孔径雷达方位向采样点数,L为线阵天线长度;发射机和接收机与控制开关之间用一个T/R转换开关相连,T/R转换开关的一边与控制开关相连,另一边分别与发射机和接收机相连,如图1所示;控制开关通过M条馈线和M个线阵馈元相连构成一个线阵天线,如图2所示;线阵天线的长度L的大小由前视线阵三维合成孔径雷达系统要求得到的分辨率决定,L=λ/ρ,其中,λ为前视线阵三维合成孔径雷达系统载波频率,ρ为系统分辨率;发射机和接收机共用一个线阵天线,使用一个T/R转换开关控制发射机和接收机在不同时段工作,即采用的是单激励工作方式。The transmitting system and the receiving system include: a transmitter, a receiver, a T/R switch, a feeder control switch, M feeders and M linear array feeders; M is a natural number, and the size of M is determined by the previous The line-of-sight array three-dimensional synthetic aperture radar system is determined by the pulse repetition frequency within a flight aperture, M=v×Na/L, where v is the speed of the flying platform, Na is the number of sampling points in the direction of the synthetic aperture radar, and L is the linear array Antenna length; the transmitter and receiver are connected to the control switch with a T/R switch, one side of the T/R switch is connected to the control switch, and the other side is connected to the transmitter and receiver respectively, as shown in Figure 1 The control switch is connected to form a linear array antenna through M feeders and M linear array feed elements, as shown in Figure 2; the length L of the linear array antenna is determined by the resolution required by the forward line-of-sight array three-dimensional synthetic aperture radar system , L=λ/ρ, where λ is the forward line-of-sight array 3D SAR system carrier frequency, ρ is the system resolution; the transmitter and the receiver share a linear array antenna, and a T/R switch is used to control the transmitter and The receiver works in different periods, that is, it adopts a single excitation mode.

步骤2:单激励线阵天线相位中心轨迹的确定Step 2: Determination of the phase center locus of single excitation linear array antenna

对于慢时间n,n=1……N,N为正整数,当n=1,控制开关按照三角周期函数打开线阵天线中任意一个线阵馈元M=M1,M1是M个线阵馈元中的任意一个线阵馈元的标记,记下慢时间n=1时工作的线阵馈元标记M1For slow time n, n=1...N, N is a positive integer, when n=1, the control switch opens any linear array feed element M=M 1 in the linear array antenna according to the triangular periodic function, M 1 is M lines The mark of any linear array feeder in the array feeder, write down the mark M 1 of the linear array feeder working when the slow time n=1;

当n=2,控制开关打开线阵天线中一个线阵馈元M=M2,M2≠M1,记下慢时间n=2时工作的线阵馈元标记M2When n=2, the control switch opens a linear array feed element M=M 2 in the linear array antenna, M 2 ≠ M 1 , and write down the mark M 2 of the linear array feed element working when the slow time n=2;

当n=3,控制开关打开线阵天线中一个线阵馈元M=M3,M3≠M2≠M1,记下慢时间n=3时工作的线阵馈元标记M3When n=3, the control switch opens a linear array feed element M=M 3 in the linear array antenna, M 3 ≠M 2 ≠M 1 , write down the line array feed element mark M 3 that works when the slow time n=3;

……;...;

依此类推,当n=N时,控制开关打开线阵天线中一个线阵馈元M=MN,M1,M2,M3,…,MN均不相同,记下慢时间n=N时工作的线阵馈元标记MN;这样,就得到慢时间和对应这个慢时间工作的线阵馈元标记的对应关系,即线阵天线相位中心轨迹,所述线阵天线相位中心轨迹构成的随机变量服从均匀分布。By analogy, when n=N, the control switch opens a linear array feed element M=M N in the linear array antenna, M 1 , M 2 , M 3 ,..., M N are all different, record the slow time n= The line array feed element mark M N of work at N; Like this, just obtain the corresponding relation of slow time and the line array feed element mark corresponding to this slow time work, namely line array antenna phase center locus, described line array antenna phase center locus The composed random variables obey the uniform distribution.

步骤3:发射/接收平台构建Step 3: Transmit/Receive Platform Construction

前视线阵三维合成孔径雷达系统发射/接收平台是将步骤1中的线阵发射系统/接收系统安置于运动平台上,线阵天线中的馈元排列方向垂直于运动平台的运动方向,运动平台以恒矢量速度

Figure A20091005912600071
运动,运动平台的初始化飞行高度为Ht0;如图3所示;The forward line-of-sight array 3D synthetic aperture radar system transmitting/receiving platform is to place the linear array transmitting system/receiving system in step 1 on the moving platform, the arrangement direction of the feed elements in the linear array antenna is perpendicular to the moving direction of the moving platform, and the moving platform at constant vector velocity
Figure A20091005912600071
Motion, the initial flight height of the motion platform is Ht0 ; as shown in Figure 3;

步骤4:发射系统和接收系统同步Step 4: Synchronize the Transmitter and Receiver Systems

在前视线阵三维成像合成孔径雷达进行三维成像过程中,在发射系统发射电磁信号后固定的延时时刻τ,转换T/R开关,让接收系统接收场景回波,以实现发射系统和接收系统的时间同步,其中,固定的延时时刻τ由观测区域到线阵天线的距离R决定,τ=0.8×2R/C,其中,C为光速。During the three-dimensional imaging process of the forward-looking array three-dimensional imaging synthetic aperture radar, the T/R switch is switched at a fixed delay time τ after the transmitting system transmits the electromagnetic signal, so that the receiving system receives the scene echo, so as to realize the transmission system and the receiving system. The time synchronization of , where the fixed delay time τ is determined by the distance R from the observation area to the linear array antenna, τ=0.8×2R/C, where C is the speed of light.

步骤5:前视线阵三维合成孔径雷达系统单激励发射/接收平台工作Step 5: Single-stimulus transmitting/receiving platform work of the forward-looking array 3D synthetic aperture radar system

通过T/R转换开关使线阵发射机和接收机按步骤2中的构建的天线相位中心轨迹对测绘场景不断的发射电磁波信号并接收回波信号,前视线阵三维合成孔径雷达系统采用单激励工作方式,即在每一个慢时间只有一个馈元工作,在这个慢时间,发射机和接收机只能通过一个馈元工作;接收机在n个慢时间得到n个测绘场景的回波信号就是前视线阵三维合成孔径雷达系统的采集数据。Through the T/R conversion switch, the linear array transmitter and receiver continuously transmit electromagnetic wave signals and receive echo signals to the surveying scene according to the antenna phase center trajectory constructed in step 2. The forward line-of-sight array 3D synthetic aperture radar system uses a single excitation Working mode, that is, only one feeder works at each slow time, and in this slow time, the transmitter and receiver can only work through one feeder; the receiver obtains the echo signals of n surveying and mapping scenes at n slow times. Acquisition data of 3D synthetic aperture radar system with forward-looking array.

通过以上步骤,即可完成前视线阵三维成像合成孔径雷达系统的构建,本发明流程图如图6所示。Through the above steps, the construction of the forward line-of-sight array three-dimensional imaging synthetic aperture radar system can be completed. The flow chart of the present invention is shown in FIG. 6 .

需要说明的是,It should be noted,

采用现有标准的后向投影算法,即可利用前视线阵三维成像合成孔径雷达系统步骤4所采集数据实现对观测区域的三维散射系数重建;Using the existing standard back projection algorithm, the data collected in step 4 of the forward line-of-sight array three-dimensional imaging synthetic aperture radar system can be used to reconstruct the three-dimensional scattering coefficient of the observation area;

步骤2中所述的控制开关按照三角周期函数打开线阵天线中任意一个线阵馈元,所述的控制开关也可以按照高斯函数、抛物线函数打开线阵天线中任意一个线阵馈元,最后得到的天线相位中心运动轨迹所服从的分布可以是三角周期函数分布或高斯函数分布或抛物线函数分布等,不影响本发明所构建前视线阵三维成像合成孔径雷达系统的有效性。The control switch described in step 2 opens any one of the linear array feed elements in the linear array antenna according to the triangular periodic function, and the described control switch can also open any one of the linear array feed elements in the linear array antenna according to the Gaussian function and the parabolic function, and finally The obtained distribution of the motion track of the antenna phase center can be a triangular periodic function distribution, a Gaussian function distribution or a parabolic function distribution, etc., which does not affect the effectiveness of the forward line-of-sight array three-dimensional imaging synthetic aperture radar system constructed by the present invention.

本发明的创新点在于该系统利用合成孔径雷达原理,结合单激励线阵三维合成孔径雷达天线相位中心控制精度高和现有前视合成孔径雷达系统能够提前获取前方地形信息,来实现实时的得知前方测绘地形的三维信息,可以实现飞行器的导航与盲降。The innovation of the present invention is that the system uses the principle of synthetic aperture radar, combined with the high control precision of the phase center of the three-dimensional synthetic aperture radar antenna of single-excitation linear array and the existing forward-looking synthetic aperture radar system, which can obtain the front terrain information in advance to realize real-time acquisition. Knowing the three-dimensional information of the terrain surveyed and mapped ahead can realize the navigation and blind landing of the aircraft.

本发明的基本原理:本发明是利用合成孔径雷达原理,结合单激励线阵三维合成孔径雷达天线相位中心控制精度高和前视合成孔径雷达系统能够提前获取前方地形信息的特点,因此我们就采用单激励线阵三维SAR系统和前视SAR系统相结合的模式,使单激励线阵三维SAR的波束前视照射。然后实时的对接收到的回波数据我们采用标准的后向投影算法(即三维BP算法)进行处理,最后就可以得到前方测绘区域的三维成像结果。The basic principle of the present invention: the present invention utilizes the principle of synthetic aperture radar, combines the characteristics of high precision of phase center control of single-excitation linear array three-dimensional synthetic aperture radar antenna phase center and forward-looking synthetic aperture radar system that can obtain terrain information in advance, so we just adopt The combination mode of the single-excitation linear array 3D SAR system and the forward-looking SAR system makes the beam of the single-excitation linear array 3D SAR forward-looking. Then we process the received echo data in real time using the standard back projection algorithm (namely the 3D BP algorithm), and finally we can get the 3D imaging result of the front surveying and mapping area.

本发明解决的技术问题:本发明提出的前视线阵三维合成孔径雷达系统主要是针对现有合成孔径雷达不能实时获取前方三维地形信息的缺点而提出的,该系统结合单激励线阵三维合成孔径雷达天线相位中心控制精度高和前视合成孔径雷达系统能够提前获取前方地形信息的优点,用线阵系统单阵元激励方式,波束前视照射,可以提前并实时的获取飞行器前方的三维地形信息,为精确制导以及飞行器的导航、进近着陆以及盲降提供了一种新方法。The technical problem solved by the present invention: the forward line-of-sight array three-dimensional synthetic aperture radar system proposed by the present invention is mainly proposed for the shortcoming that the existing synthetic aperture radar cannot obtain the front three-dimensional terrain information in real time. The radar antenna phase center control precision is high and the forward-looking synthetic aperture radar system can obtain the advantages of the front terrain information in advance. With the excitation method of the single array element of the linear array system and the forward-looking irradiation of the beam, the three-dimensional terrain information in front of the aircraft can be obtained in advance and in real time. , providing a new method for precision guidance and aircraft navigation, approach and landing, and blind landing.

本发明的优点在于采用了单激励线阵三维SAR和前视SAR相结合的特点,利用较低的硬件成本,实现了小数据处理量的前视线阵三维合成孔径雷达成像,最主要的就是实现了飞行器前方测绘区域的三维成像,可以提前并实时的获取飞行器前方的三维地形信息。The advantage of the present invention is that it adopts the characteristic of combining single-excitation linear array 3D SAR and forward-looking SAR, utilizes lower hardware cost, and realizes forward-looking array 3D synthetic aperture radar imaging with small data processing capacity, the most important thing is to realize The three-dimensional imaging of the mapping area in front of the aircraft can obtain the three-dimensional terrain information in front of the aircraft in advance and in real time.

附图说明 Description of drawings

图1是本发明发射系统/接收系统结构框图Fig. 1 is a structural block diagram of transmitting system/receiving system of the present invention

图2是本发明发射机/接收机的线阵天线结构框图Fig. 2 is the structural block diagram of the line array antenna of transmitter/receiver of the present invention

图3是本发明采用的前视线阵三维成像合成孔径雷达运动几何结构图Fig. 3 is the motion geometric structure diagram of the forward line-of-sight array three-dimensional imaging synthetic aperture radar adopted in the present invention

其中,

Figure A20091005912600091
为飞行器的速度矢量,θf为前视角;X、Y、Z为三维坐标系;in,
Figure A20091005912600091
is the velocity vector of the aircraft, θ f is the front viewing angle; X, Y, Z are the three-dimensional coordinate system;

图4是本发明具体实施例对三维点目标的成像结果图Fig. 4 is the imaging result diagram of the specific embodiment of the present invention to the three-dimensional point target

其中横坐标为切航迹方向,纵坐标为沿航迹方向,垂直坐标为高度向,1为三维点目标成像。The abscissa is the direction tangent to the track, the ordinate is the direction along the track, the vertical coordinate is the height direction, and 1 is the imaging of the three-dimensional point target.

图5是本发明具体实施例仿真时用的参数表Fig. 5 is the parameter table used when emulating the specific embodiment of the present invention

图6是本发明的流程图Fig. 6 is a flowchart of the present invention

具体实施方式 Detailed ways

本发明主要采用仿真实验的方法进行验证该系统模型的可行性,所有步骤、结论都在VC++、MATLAB7.0上验证正确。具体实施步骤如下:The present invention mainly uses the simulation experiment method to verify the feasibility of the system model, and all steps and conclusions are verified correctly on VC++ and MATLAB7.0. The specific implementation steps are as follows:

步骤1:线阵发射/接收系统构建Step 1: Construction of line array transmitting/receiving system

前视线阵三维合成孔径雷达系统运动平台上的线阵发射机/接收机包括以下部分:一台发射机,一台接收机,一个T/R转换开关,一个馈元控制开关,800条馈线和800个线阵馈元,其系统框图如附图1所示,发射机和接收机与控制开关之间用一个T/R转换开关相连,发射机和接收机分别与T/R转换开关相连控制开关和接收机相连,控制开关通过800条馈线和800个线阵馈元相连,线阵的长度为20。在一个飞行孔径内,T/R转换开关控制发射机与接收机之间的切换,控制开关控制每一个慢时间n,n=1L N所打开的馈元的位置,且在每一个慢时间n仅有一个馈元被打开。线阵馈元的方位波束宽度为

Figure A20091005912600092
i=1L 1000,水平波束宽度分别为
Figure A20091005912600101
单位为弧度,i=1L 1000。The linear array transmitter/receiver on the moving platform of the forward line-of-sight array three-dimensional synthetic aperture radar system includes the following parts: a transmitter, a receiver, a T/R switch, a feeder control switch, 800 feeders and 800 linear array feed elements, the system block diagram is shown in Figure 1, the transmitter and receiver are connected to the control switch with a T/R switch, and the transmitter and receiver are respectively connected to the T/R switch for control The switch is connected to the receiver, and the control switch is connected to 800 line array feeders through 800 feeders, and the length of the line array is 20. In a flight aperture, the T/R switch controls the switching between the transmitter and the receiver, and the control switch controls the position of the feed element opened by each slow time n, n=1L N, and at each slow time n Only one feed is opened. The azimuth beamwidth of the linear array feed is
Figure A20091005912600092
i=1L 1000, the horizontal beam widths are
Figure A20091005912600101
The unit is radian, i=1L 1000.

步骤2:单激励阵列天线相位中心轨迹的构建Step 2: Construction of the phase center locus of the single excitation array antenna

因为前视线阵三维合成孔径雷达采用的是单激励工作方式,在每一个慢时间n,n=1……N,利用控制开关按照三角周期函数来选择单激励阵列天线中的任意一个馈元来发射和接收信号,并记录每个打开馈元所在的位置,那么所有的慢时间,所有的工作的馈元的位置就构成了一个轨迹,定义为前视线阵三维合成孔径雷达的天线相位中心的轨迹。Because the forward line-of-sight array 3D synthetic aperture radar adopts a single-excitation working mode, at each slow time n, n=1...N, use the control switch to select any feed element in the single-excitation array antenna according to the triangular periodic function. Transmit and receive signals, and record the position of each open feed element, then all the slow times, the positions of all working feed elements constitute a trajectory, which is defined as the antenna phase center of the forward line-of-sight array three-dimensional synthetic aperture radar trajectory.

步骤3:发射/接收运动平台构建Step 3: Transmit/Receive Motion Platform Construction

前视线阵三维合成孔径雷达系统发射/接受运动平台是将步骤1中的线阵发射机/接收机安置于运动平台上,线阵天线排列方向沿垂直发射平台运动方向放置,运动平台以恒矢量速度[01000]运动,运动平台的初始化飞行高度为1000m。The forward line-of-sight array 3D synthetic aperture radar system transmits/receives the moving platform by placing the linear array transmitter/receiver in step 1 on the moving platform, the arrangement direction of the linear array antenna is placed along the vertical direction of the transmitting platform’s moving direction, and the moving platform is set with a constant vector Speed [01000] motion, the initial flight height of the motion platform is 1000m.

通过T/R转换开关使线阵发射机和接收机按步骤2中的构建的天线相位中心轨迹对测绘场景不断的发射电磁波信号并接收回波信号。Use the T/R switch to make the line array transmitter and receiver continuously transmit electromagnetic wave signals and receive echo signals to the surveying and mapping scene according to the antenna phase center trajectory constructed in step 2.

前视线阵三维合成孔径雷达的飞行几何结构图见附图3。The flight geometric structure diagram of the forward line-of-sight array three-dimensional synthetic aperture radar is shown in Figure 3.

本具体实施方式所采用的系统参数详见图5,最后我们对测绘点进行仿真成像,得到的3D成像如图4所示。The system parameters adopted in this specific embodiment are shown in FIG. 5 for details. Finally, we simulate and image the surveying and mapping points, and the obtained 3D imaging is shown in FIG. 4 .

通过本发明具体实施方式的仿真及测试,本发明所提供的前视线阵三维合成孔径雷达系统能够实现了前视线阵三维成像合成孔径雷达成像,与现有的三维合成孔径雷达系统相比,本发明在克服现有系统缺点,提前获取了飞行器前方三维地形信息,为精确制导以及飞行器的导航、进近着陆以及盲降提供了一种新方法。Through the simulation and testing of the specific embodiments of the present invention, the 3D synthetic aperture radar system provided by the present invention can realize the 3D imaging synthetic aperture radar imaging of the forward line of sight array. Compared with the existing 3D synthetic aperture radar system, this The invention overcomes the shortcomings of the existing system, obtains the three-dimensional terrain information in front of the aircraft in advance, and provides a new method for precise guidance, aircraft navigation, approach landing and blind landing.

Claims (2)

1. A construction method of a forward looking linear array three-dimensional synthetic aperture radar system is characterized by comprising the following steps:
step 1: single excitation transmitting system and receiving system construction
The transmitting system and the receiving system include: the system comprises a transmitter, a receiver, a T/R change-over switch, a feed element control switch, M feeder lines and M linear array feed elements; m is a natural number, the size of M is determined by the size of pulse repetition frequency of a foresight linear array three-dimensional synthetic aperture radar system in a flight aperture, and M is v multiplied by Na/L, wherein v is the speed of a flight platform, Na is the number of sampling points of the synthetic aperture radar in the azimuth direction, and L is the length of a linear array antenna; the transmitter and the receiver are connected with the control switch by a T/R change-over switch, one side of the T/R change-over switch is connected with the control switch, the other side of the T/R change-over switch is respectively connected with the transmitter and the receiver, the control switch is connected with M linear array feed elements by M feeder lines to form a linear array antenna, the length L of the linear array antenna is determined by the resolution ratio required by the foresight linear array three-dimensional synthetic aperture radar system, L is lambda/rho, wherein lambda is the carrier frequency of the foresight linear array three-dimensional synthetic aperture radar system, and rho is the system resolution ratio; the transmitter and the receiver share a linear array antenna, and a T/R change-over switch is used for controlling the transmitter and the receiver to work at different time intervals, namely, a single excitation working mode is adopted;
step 2: determination of phase center trajectory for single-excitation antenna
For slow time N, N is 1. N is a positive integer, and when N is 1, the control switch opens any linear array feed element M in the linear array antenna according to a triangular periodic function1,M1Is the mark of any one of M linear array feed elements, and marks the linear array feed element mark M working when the slow time n is equal to 11
When n is 2, the control switch opens one linear array feed element M in the linear array antenna2,M2≠M1Recording linear array feed element mark M working when slow time n is 12
When n is 3, the switch is controlled to open one linear array feed element M in the linear array antenna3,M3≠M2≠M1Recording linear array feed element mark M working when slow time n is 12
……;
And so on, when N equals to N, the control switch opens one linear array feed element M equals to MN, M in the linear array antenna1,M2,M3,…,MNDifferent, recording the line array feed element mark M working when the slow time N is equal to NN(ii) a Thus, the corresponding relation between the slow time and the linear array feed element mark working corresponding to the slow time is obtained, namely the phase center track of the linear array antenna, and the phase of the linear array antennaRandom variables formed by the central track are subjected to uniform distribution;
and step 3: transmit/receive platform construction
The forward looking linear array three-dimensional synthetic aperture radar system transmitting/receiving platform is characterized in that the linear array transmitting system/receiving system in the step 1 is arranged on a moving platform, the arrangement direction of feed elements in a linear array antenna is vertical to the moving direction of the moving platform, and the moving platform is at constant vector speed
Figure A2009100591260003C1
Initial flying height of moving platform is Ht0
And 4, step 4: transmission system and reception system synchronization
In the process of three-dimensional imaging of the front line-of-sight array three-dimensional imaging synthetic aperture radar, a T/R switch is switched at a fixed delay time tau after an emission system emits electromagnetic signals, and a receiving system is enabled to receive scene echoes to achieve time synchronization of the emission system and the receiving system, wherein the fixed delay time tau is determined by the distance R from an observation area to a linear array antenna, tau is 0.8 multiplied by 2R/C, and C is the speed of light;
and 5: single excitation transmitting/receiving platform work of forward looking linear array three-dimensional synthetic aperture radar system
Enabling the linear array transmitter and the receiver to continuously transmit electromagnetic wave signals and receive echo signals to a surveying and mapping scene according to the antenna phase center track constructed in the step 2 through a T/R (time to arrival) change-over switch, wherein the forward-looking linear array three-dimensional synthetic aperture radar system adopts a single excitation working mode, namely only one feed element works at each slow time, and the transmitter and the receiver can only work through one feed element at the slow time; the receiver obtains echo signals of n surveying and mapping scenes in n slow time, and the echo signals are acquired data of the forward looking linear array three-dimensional synthetic aperture radar system.
2. The method according to claim 1, wherein said control switch in step 2 opens any one of the linear array feed elements in the linear array antenna according to a triangular periodic function, said triangular periodic function is replaced by a gaussian function or a parabolic function, and the distribution obeyed by the antenna phase center motion trajectory obtained after replacement is gaussian function distribution or parabolic function distribution.
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