CN111722255A - A regional navigation and positioning system and method based on space-time modulation - Google Patents
A regional navigation and positioning system and method based on space-time modulation Download PDFInfo
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Abstract
本发明提供了一种基于空时调制的区域导航定位方法及系统,包括:导航基站产生数字导航信号,经过包括数模转换、上变频、滤波和功率放大后,由调制开关模块进行周期性空时调制,并由天线阵列向空间辐射;在移动端接收到导航信号后,经过包括低噪声放大、下变频、滤波和驱动放大后,由模数转换器将导航信号转换为数字导航信号;在数字域内对数字导航信号进行解调,获取当前导航基站位置信息;分析接收的数字导航信号中的基波与谐波分量,计算移动端相对于导航基站的方位角与俯仰角;获取多个导航基站的位置以及移动端相对于导航基站的方位角和俯仰角,解算移动端当前的三维坐标。本发明尤其适用于大量用户同时进行定位及导航的系统中。
The invention provides a method and system for regional navigation and positioning based on space-time modulation, including: a navigation base station generates a digital navigation signal; time-modulated, and radiated into space by the antenna array; after receiving the navigation signal at the mobile terminal, the navigation signal is converted into a digital navigation signal by an analog-to-digital converter after low-noise amplification, down-conversion, filtering and drive amplification; Demodulate the digital navigation signal in the digital domain to obtain the position information of the current navigation base station; analyze the fundamental wave and harmonic components in the received digital navigation signal, and calculate the azimuth and pitch angle of the mobile terminal relative to the navigation base station; obtain multiple navigation The position of the base station and the azimuth and pitch angles of the mobile terminal relative to the navigation base station are used to calculate the current three-dimensional coordinates of the mobile terminal. The present invention is especially suitable for a system in which a large number of users perform positioning and navigation at the same time.
Description
技术领域technical field
本发明涉及无线电导航与定位工程技术领域,具体地,涉及一种基于空时调制的区域导航定位系统及方法,更为具体地,涉及一种仅被动接收基站端发射的无线电信号来实现导航和定位的系统。The present invention relates to the technical field of radio navigation and positioning engineering, in particular, to a regional navigation and positioning system and method based on space-time modulation, and more particularly, to a method of passively receiving radio signals transmitted by a base station to realize navigation and positioning. positioning system.
背景技术Background technique
无线电导航和定位技术在军事国防以及国民生活中均有着广泛的应用。在全球定位系统诞生以前,无线电导航是飞机的主要导航方式,例如无线电罗兰C、塔康等导航系统。在GPS、北斗等全球性定位系统部署后,作为安全性备份,无线电导航至今仍在民航等领域有着广泛的应用。例如VOR/DME(指向台)导航技术,该技术需要大型的环形天线阵来发射导航信号,技术非常复杂。Radio navigation and positioning technology has a wide range of applications in military defense and national life. Before the birth of the global positioning system, radio navigation was the main navigation method for aircraft, such as radio Roland C, Tacan and other navigation systems. After the deployment of global positioning systems such as GPS and Beidou, as a safety backup, radio navigation is still widely used in civil aviation and other fields. For example, the VOR/DME (pointing station) navigation technology requires a large loop antenna array to transmit navigation signals, and the technology is very complex.
专利文献CN106842263A(申请号:201710046067.2)公开了一种基于导航信号空时处理与矢量跟踪相结合的卫星导航方法,包括以下步骤:坐标系的建立;接收机对卫星导航信号进行接收;将接收到的卫星信号进行空时处理;空时相干约束,利用相干的本地合成载波和扩频信号,实现阵列的相干调向约束,相干调向约束后的数据送入滤波器组,最后提取观测量送至后端实现导航解算;卫星导航信号的捕获跟踪和矢量跟踪,利用空时联合相干约束,得到相对于载体坐标系原点的卫星信号,对该信号进行载波和码相位鉴相,则可获取该卫星信号的星历数据,利用该通道的EPL数据进一步获取载波和码相位,形成观测量,并可实现定位运算。Patent document CN106842263A (application number: 201710046067.2) discloses a satellite navigation method based on the combination of space-time processing of navigation signals and vector tracking, including the following steps: establishing a coordinate system; receiving satellite navigation signals by a receiver; space-time processing of satellite signals; space-time coherence constraints, using coherent local composite carrier and spread spectrum signals to achieve coherent steering constraints of the array, the data after coherent steering constraints are sent to the filter bank, and finally the observation data is extracted. Navigation solution is realized at the back end; for satellite navigation signal acquisition tracking and vector tracking, using space-time joint coherence constraints, the satellite signal relative to the origin of the carrier coordinate system is obtained. From the ephemeris data of the satellite signal, the carrier and code phase are further obtained by using the EPL data of this channel to form the observation quantity, and the positioning operation can be realized.
发明内容SUMMARY OF THE INVENTION
针对现有技术中的缺陷,本发明的目的是提供一种基于空时调制的区域导航定位方法及系统。In view of the defects in the prior art, the purpose of the present invention is to provide a method and system for regional navigation and positioning based on space-time modulation.
根据本发明提供的一种基于空时调制的区域导航定位方法,包括:According to a method for regional navigation and positioning based on space-time modulation provided by the present invention, the method includes:
步骤M1:导航基站产生数字导航信号,经过包括数模转换、驱动放大、上变频、滤波和功率放大后,由调制开关模块进行周期性空时调制;Step M1: the navigation base station generates a digital navigation signal, which is subjected to periodic space-time modulation by a modulation switch module after including digital-to-analog conversion, drive amplification, up-conversion, filtering and power amplification;
步骤M2:经过周期性空时调制的导航信号,由天线阵列向空间辐射;Step M2: the periodic space-time modulated navigation signal is radiated into space by the antenna array;
步骤M3:在移动端接收到导航信号后,经过包括低噪声放大、下变频、滤波和驱动放大后,由模数转换器将导航信号转换为数字导航信号;Step M3: After the mobile terminal receives the navigation signal, after including low-noise amplification, down-conversion, filtering and drive amplification, the analog-to-digital converter converts the navigation signal into a digital navigation signal;
步骤M4:在数字域内对数字导航信号进行解调,获取当前导航基站位置信息;同时分析接收的数字导航信号中的基波与谐波分量,估计移动端相对于导航基站的方位角与俯仰角;Step M4: demodulate the digital navigation signal in the digital domain to obtain the position information of the current navigation base station; analyze the fundamental wave and harmonic components in the received digital navigation signal at the same time, and estimate the azimuth angle and pitch angle of the mobile terminal relative to the navigation base station ;
步骤M5:在获取多个导航基站的位置以及移动端相对于导航基站的方位角和俯仰角后,通过角度交叉定位的方法,解算移动端当前的三维坐标,实现移动端的导航和定位。Step M5: After obtaining the positions of multiple navigation base stations and the azimuth and pitch angles of the mobile terminal relative to the navigation base stations, the current three-dimensional coordinates of the mobile terminal are solved by the method of angle cross positioning, so as to realize the navigation and positioning of the mobile terminal.
优选地,所述步骤M1包括:天线阵列1、调制开关模块2、功率放大器3、带通滤波器4、混频器5、射频本振6、低通滤波器7、数模转换器8和发射端信号处理模块9;Preferably, the step M1 includes: an
步骤M1.1:发射端信号处理模块9产生数字导航信号;Step M1.1: the transmitter
步骤M1.2:数模转换器8将数字导航信号转换成模拟导航信号;Step M1.2: the digital-to-
步骤M1.3:通过低通滤波器7过滤掉模拟导航信号中的高频分量;Step M1.3: filter out high-frequency components in the analog navigation signal through the low-
步骤M1.4:射频本振6结合混频器5将模拟导航信号中的中频导航信号变换至高频;Step M1.4: the RF
步骤M1.5:通过带通滤波器4选取混频后的高频导航信号;Step M1.5: select the mixed high-frequency navigation signal through the
步骤M1.6:通过功率放大器3对高频导航信号进行功率放大;Step M1.6: Power amplify the high-frequency navigation signal through the
步骤M1.7:由发射端信号处理模块9控制调制开关模块2对功率放大的高频导航信号进行周期性空时调制。Step M1.7: The transmitter
优选地,所述天线阵列包括三个天线单元组成的天线阵列或多个天线单元组成的天线阵列;所述三个天线单元组成的天线阵列排列方式为L形;所述多个天线单元组成的天线阵列排列方式为圆形。Preferably, the antenna array includes an antenna array composed of three antenna elements or an antenna array composed of multiple antenna elements; the antenna array composed of the three antenna elements is arranged in an L-shape; The arrangement of the antenna array is circular.
优选地,所述所述调制开关模块2组成方式包括单刀多掷射频开关或单刀单掷射频开关与功分器的组合形式;Preferably, the composition of the
所述功率放大器3是对导航信号进行功率放大;The
所述带通滤波器4选取混频后的高频导航信号,抑制不需要的边带;The
所述混频器5将中频导航信号变换至高频;The
所述射频本振6为混频器提供本地振荡信号;The radio frequency
所述低通滤波器7过滤掉数模转换后的导频信号中的高频分量;The low-
所述数模转换器8将数字导航信号转换成模拟导航信号;The digital-to-
所述发射端信号处理模块9产生数字导航信号,并控制调制开关模块对导航信号进行周期性空时调制。The transmitter
优选地,所述步骤M3包括:接收天线10、低噪声放大器11、混频器12、射频本振13、低通滤波器14、驱动放大器15和模数转换器16;Preferably, the step M3 includes: a
步骤M3.1:接收天线10接收导航基站发出的导航信号;通过低噪声放大器11对接收的导航信号进行低噪声放大;Step M3.1: the
步骤M3.2:射频本振13结合混频器12将通过低噪声放大器放大之后的导航信号混频至中频;Step M3.2: the RF
步骤M3.3:通过低通滤波器14过滤掉混频后的导航信号中的高频分量;Step M3.3: filter out the high-frequency components in the mixed navigation signal through the low-
步骤M3.4:驱动放大器15将通过低通滤波器过滤后的导航信号进行驱动放大;Step M3.4: the
步骤M3.5:模数转换器16将驱动放大的模拟导航信号转换为数字导航信号。Step M3.5: The analog-to-
优选地,所述接收天线10能够接收导航基站发出的导航信号;Preferably, the
所述低噪声放大器11能够对接收的导航信号进行低噪声放大;The low-
所述混频器12能够将射频的导航信号混频至中频;The
所述射频本振13能够为接收混频器提供本地振荡信号;The radio frequency
所述低通滤波器14能够过滤掉混频后的导航信号中的高频分量;The low-
所述驱动放大器15能够对混频后的导航信号进行驱动放大,使得输出信号满足模数转换器16的输入量程;The
所述数模转换器16能够将接收的模拟导航信号转换为数字信号。The digital-to-
优选地,所述步骤M4包括:利用移动端信号处理模块17在数字域内对数字导航信号进行解调,获取当前导航基站位置信息;同时分析移动端信号处理模块17接收的数字导航信号中的基波与谐波分量,计算移动端相对于导航基站的方位角与俯仰角;Preferably, the step M4 includes: using the mobile terminal
优选地,所述步骤M5包括:在移动端利用单天线对接收的导航信号进行无线电测向实现角度交叉定位的方法。Preferably, the step M5 includes: using a single antenna at the mobile terminal to perform radio direction finding on the received navigation signal to achieve angular cross positioning.
根据本发明提供的一种基于空时调制的区域导航定位系统,包括:A space-time modulation-based regional navigation and positioning system provided according to the present invention includes:
天线阵列1、调制开关网络2、发射链路18、发射端信号处理模块9、接收天线10、接收链路19和移动端信号处理模块17;
所述发射端信号处理模块9与发射链路18和调制开关模块2连接,所述发射链路18与调制开关模块2连接,调制开关模块2与天线阵列1连接;The transmitter
所述移动端信号处理模块17与所述接收链路19连接;所述接收链路19与所述接收天线10连接;The mobile terminal
所述发射端信号处理模块9产生数字导航信号,并控制调制开关模块2对模拟导航信号进行周期性空时调制;The transmitter
所述发射链路18能够将数字导航信号转换为模拟导航信号,并进行包括驱动放大、上变频、带通滤波、功率放大操作;The transmitting
所述调制开关模块2能够对输入的模拟导航信号进行周期性空时调制,并将调制后的导航信号馈入天线阵列1的各单元;The
所述天线阵列1能够向空间辐射经过周期性空时调制的导航信号;The
所述接收天线10能够接收导航基站发出的导航信号;The receiving
所述接收链路19能够对接收的导航信号进行包括低噪声放大、下变频、低通滤波、模数转换的操作,使模拟导航信号转换为数字导航信号;The receiving
所述移动端信号处理模块17能够对接收的导航信号的谐波频谱进行分析,计算移动端相对于基站端的方向;并在已知基站端的位置的条件下,根据移动端相对于多个基站端的方向来解算移动端当前的位置,实现导航和定位。The mobile terminal
优选地,所述发射链路18包括功率放大器3、带通滤波器4、混频器5、射频本振6、低通滤波器7和数模转换器8;Preferably, the
所述数模转换器8与所述低通滤波器7连接;所述低通滤波器7与所述混频器5连接;所述混频器5与所述射频本振6和所述带通滤波器4连接;所述带通滤波器4与所述功率放大器3连接;所述功率放大器3与所述调制开关模块2连接;The digital-to-
所述功率放大器3能够对导航信号进行功率放大;The
所述带通滤波器4选取混频后的高频导航信号,抑制不需要的边带;The
所述混频器5将中频导航信号变换至高频;The
所述射频本振6为混频器提供本地振荡信号;The radio frequency
所述低通滤波器7过滤掉数模转换后的导频信号中的高频分量;The low-
所述数模转换器8将数字导航信号转换成模拟导航信号;The digital-to-
所述接收链路19包括:低噪声放大器11、混频器12、射频本振13、低通滤波器14、驱动放大器15和模数转换器16;The receiving
所述模数转换器16与所述驱动放大器15连接;所述驱动放大器15与所述低通滤波器14连接;所述低通滤波器14与所述混频器12连接;所述混频器12与所述射频本振13和所述低噪声放大器11连接;所述低噪声放大器11与所述接收天线10连接;The analog-to-
所述低噪声放大器11能够对接收的导航信号进行低噪声放大;The low-
所述混频器12能够将射频的导航信号混频至中频;The
所述射频本振13能够为接收混频器提供本地振荡信号;The radio frequency
所述低通滤波器14能够过滤掉混频后的导航信号中的高频分量;The low-
所述驱动放大器15能够对混频后的导航信号进行驱动放大,使得输出信号满足模数转换器16的输入量程;The
所述数模转换器16能够将接收的模拟导航信号转换为数字信号。The digital-to-
与现有技术相比,本发明具有如下的有益效果:Compared with the prior art, the present invention has the following beneficial effects:
1、本发明无需大型精密的导航基站,同时无需导航基站与移动端之间的双向通信;1. The present invention does not require a large and precise navigation base station, and at the same time does not require two-way communication between the navigation base station and the mobile terminal;
2、本发明中的移动端相对于导航基站进行了二维测向,与之相比,现有的两站VOR测向定位仅测量一维的方位角。因此,本发明能测量移动端的三维坐标,其预期的定位精度更高;2. The mobile terminal in the present invention performs two-dimensional direction finding with respect to the navigation base station. Compared with the existing two-station VOR direction finding positioning, only one-dimensional azimuth is measured. Therefore, the present invention can measure the three-dimensional coordinates of the mobile terminal, and its expected positioning accuracy is higher;
3、本发明通过在导航基站端对导航进行进行周期性空时调制,使得发射的导航信号携带了空间方位信息,在移动端无需采用多天线进行方位测量,就可获得移动端相对于导航基站端的方位;3. The present invention performs periodic space-time modulation on the navigation at the navigation base station, so that the transmitted navigation signal carries the spatial orientation information, and the mobile terminal does not need to use multiple antennas for orientation measurement, and the relative position of the mobile terminal to the navigation base station can be obtained. the orientation of the end;
4、本发明尤其适用于大量用户同时进行定位及导航的系统中。4. The present invention is especially suitable for a system in which a large number of users perform positioning and navigation at the same time.
附图说明Description of drawings
通过阅读参照以下附图对非限制性实施例所作的详细描述,本发明的其它特征、目的和优点将会变得更明显:Other features, objects and advantages of the present invention will become more apparent by reading the detailed description of non-limiting embodiments with reference to the following drawings:
图1为本发明提供的区域导航定位系统的基站端与移动端的结构框图;Fig. 1 is the structural block diagram of the base station end and the mobile end of the regional navigation and positioning system provided by the present invention;
图2为本发明提供的区域导航定位系统的基站端与移动端的结构框图;Fig. 2 is the structural block diagram of the base station end and the mobile end of the regional navigation and positioning system provided by the present invention;
图3为实施例3中移动端接收到的导航信号的频谱;Fig. 3 is the frequency spectrum of the navigation signal received by the mobile terminal in
图4为实施例3中不同信噪比条件下移动端估计其相对于基站端的方位角与俯仰角误差的均方根值;Fig. 4 is the root mean square value of the azimuth angle and pitch angle error estimated by the mobile end relative to the base station end under different signal-to-noise ratio conditions in
图5为实施例2中移动端利用两个导航基站进行定位的结果示意图;5 is a schematic diagram of the result of positioning the mobile terminal using two navigation base stations in
图6为实施例3中进行100次定位的定位误差结果。FIG. 6 shows the positioning error results of 100 positionings performed in Example 3. FIG.
具体实施方式Detailed ways
下面结合具体实施例对本发明进行详细说明。以下实施例将有助于本领域的技术人员进一步理解本发明,但不以任何形式限制本发明。应当指出的是,对本领域的普通技术人员来说,在不脱离本发明构思的前提下,还可以做出若干变化和改进。这些都属于本发明的保护范围。The present invention will be described in detail below with reference to specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that, for those skilled in the art, several changes and improvements can be made without departing from the inventive concept. These all belong to the protection scope of the present invention.
实施例1Example 1
根据本发明提供的一种基于空时调制的区域导航定位方法,包括:如图1所示,According to a method for regional navigation and positioning based on space-time modulation provided by the present invention, the method includes: as shown in FIG. 1 ,
步骤M1:导航基站产生数字导航信号,经过包括数模转换、驱动放大、上变频、滤波和功率放大后,由调制开关模块进行周期性空时调制;Step M1: the navigation base station generates a digital navigation signal, which is subjected to periodic space-time modulation by a modulation switch module after including digital-to-analog conversion, drive amplification, up-conversion, filtering and power amplification;
步骤M2:经过周期性空时调制的导航信号,由天线阵列向空间辐射;Step M2: the periodic space-time modulated navigation signal is radiated into space by the antenna array;
步骤M3:在移动端接收到导航信号后,经过包括低噪声放大、下变频、滤波和驱动放大后,由模数转换器将导航信号转换为数字导航信号;Step M3: After the mobile terminal receives the navigation signal, after including low-noise amplification, down-conversion, filtering and drive amplification, the analog-to-digital converter converts the navigation signal into a digital navigation signal;
步骤M4:在数字域内对数字导航信号进行解调,获取当前导航基站位置信息;同时分析接收的数字导航信号中的基波与谐波分量,估计移动端相对于导航基站的方位角与俯仰角;Step M4: demodulate the digital navigation signal in the digital domain to obtain the position information of the current navigation base station; analyze the fundamental wave and harmonic components in the received digital navigation signal at the same time, and estimate the azimuth angle and pitch angle of the mobile terminal relative to the navigation base station ;
步骤M5:在获取多个导航基站的位置以及移动端相对于导航基站的方位角和俯仰角后,通过角度交叉定位的方法,解算移动端当前的三维坐标,实现移动端的导航和定位。Step M5: After obtaining the positions of multiple navigation base stations and the azimuth and pitch angles of the mobile terminal relative to the navigation base stations, the current three-dimensional coordinates of the mobile terminal are solved by the method of angle cross positioning, so as to realize the navigation and positioning of the mobile terminal.
具体地,所述步骤M1包括:天线阵列1、调制开关模块2、功率放大器3、带通滤波器4、混频器5、射频本振6、低通滤波器7、数模转换器8和发射端信号处理模块9;Specifically, the step M1 includes: an
步骤M1.1:发射端信号处理模块9产生数字导航信号;Step M1.1: the transmitter
步骤M1.2:数模转换器8将数字导航信号转换成模拟导航信号;Step M1.2: the digital-to-
步骤M1.3:通过低通滤波器7过滤掉模拟导航信号中的高频分量;Step M1.3: filter out high-frequency components in the analog navigation signal through the low-
步骤M1.4:射频本振6结合混频器5将模拟导航信号中的中频导航信号变换至高频;Step M1.4: the RF
步骤M1.5:通过带通滤波器4选取混频后的高频导航信号;Step M1.5: select the mixed high-frequency navigation signal through the
步骤M1.6:通过功率放大器3对高频导航信号进行功率放大;Step M1.6: Power amplify the high-frequency navigation signal through the
步骤M1.7:由发射端信号处理模块9控制调制开关模块2对功率放大的高频导航信号进行周期性空时调制。Step M1.7: The transmitter
具体地,所述天线阵列包括三个天线单元组成的天线阵列或多个天线单元组成的天线阵列;所述三个天线单元组成的天线阵列排列方式为L形;所述多个天线单元组成的天线阵列排列方式为圆形。Specifically, the antenna array includes an antenna array composed of three antenna units or an antenna array composed of multiple antenna units; the antenna array composed of the three antenna units is arranged in an L-shape; The arrangement of the antenna array is circular.
具体地,所述所述调制开关模块2组成方式包括单刀多掷射频开关或单刀单掷射频开关与功分器的组合形式;Specifically, the composition of the
所述功率放大器3是对导航信号进行功率放大;The
所述带通滤波器4选取混频后的高频导航信号,抑制不需要的边带;The
所述混频器5将中频导航信号变换至高频;The
所述射频本振6为混频器提供本地振荡信号;The radio frequency
所述低通滤波器7过滤掉数模转换后的导频信号中的高频分量;The low-
所述数模转换器8将数字导航信号转换成模拟导航信号;The digital-to-
所述发射端信号处理模块9产生数字导航信号,并控制调制开关模块对导航信号进行周期性空时调制。The transmitter
具体地,所述步骤M3包括:接收天线10、低噪声放大器11、混频器12、射频本振13、低通滤波器14、驱动放大器15和模数转换器16;Specifically, the step M3 includes: a receiving
步骤M3.1:接收天线10接收导航基站发出的导航信号;通过低噪声放大器11对接收的导航信号进行低噪声放大;Step M3.1: the receiving
步骤M3.2:射频本振13结合混频器12将通过低噪声放大器放大之后的导航信号混频至中频;Step M3.2: the RF
步骤M3.3:通过低通滤波器14过滤掉混频后的导航信号中的高频分量;Step M3.3: filter out the high-frequency components in the mixed navigation signal through the low-
步骤M3.4:驱动放大器15将通过低通滤波器过滤后的导航信号进行驱动放大;Step M3.4: the driving
步骤M3.5:模数转换器16将驱动放大的模拟导航信号转换为数字导航信号。Step M3.5: The analog-to-
具体地,所述接收天线10能够接收导航基站发出的导航信号;Specifically, the receiving
所述低噪声放大器11能够对接收的导航信号进行低噪声放大;The low-
所述混频器12能够将射频的导航信号混频至中频;The
所述射频本振13能够为接收混频器提供本地振荡信号;The radio frequency
所述低通滤波器14能够过滤掉混频后的导航信号中的高频分量;The low-
所述驱动放大器15能够对混频后的导航信号进行驱动放大,使得输出信号满足模数转换器16的输入量程;The
所述数模转换器16能够将接收的模拟导航信号转换为数字信号。The digital-to-
具体地,所述步骤M4包括:利用移动端信号处理模块17在数字域内对数字导航信号进行解调,获取当前导航基站位置信息;同时分析移动端信号处理模块17接收的数字导航信号中的基波与谐波分量,计算移动端相对于导航基站的方位角与俯仰角;Specifically, the step M4 includes: using the mobile terminal
具体地,所述步骤M5包括:在移动端利用单天线对接收的导航信号进行无线电测向实现角度交叉定位的方法。Specifically, the step M5 includes: using a single antenna at the mobile terminal to perform radio direction finding on the received navigation signal to achieve angular cross positioning.
根据本发明提供的一种基于空时调制的区域导航定位系统,包括:如图2所示,A regional navigation and positioning system based on space-time modulation provided according to the present invention includes: as shown in FIG. 2 ,
天线阵列1、调制开关网络2、发射链路18、发射端信号处理模块9、接收天线10、接收链路19和移动端信号处理模块17;
所述发射端信号处理模块9与发射链路18和调制开关模块2连接,所述发射链路18与调制开关模块2连接,调制开关模块2与天线阵列1连接;The transmitter
所述移动端信号处理模块17与所述接收链路19连接;所述接收链路19与所述接收天线10连接;The mobile terminal
所述发射端信号处理模块9产生数字导航信号,并控制调制开关模块2对模拟导航信号进行周期性空时调制;The transmitter
所述发射链路18能够将数字导航信号转换为模拟导航信号,并进行包括驱动放大、上变频、带通滤波、功率放大操作;The transmitting
所述调制开关模块2能够对输入的模拟导航信号进行周期性空时调制,并将调制后的导航信号馈入天线阵列1的各单元;The
所述天线阵列1能够向空间辐射经过周期性空时调制的导航信号;The
所述接收天线10能够接收导航基站发出的导航信号;The receiving
所述接收链路19能够对接收的导航信号进行包括低噪声放大、下变频、低通滤波、模数转换的操作,使模拟导航信号转换为数字导航信号;The receiving
所述移动端信号处理模块17能够对接收的导航信号的谐波频谱进行分析,计算移动端相对于基站端的方向;并在已知基站端的位置的条件下,根据移动端相对于多个基站端的方向来解算移动端当前的位置,实现导航和定位。The mobile terminal
具体地,所述发射链路18包括功率放大器3、带通滤波器4、混频器5、射频本振6、低通滤波器7和数模转换器8;Specifically, the transmit
所述数模转换器8与所述低通滤波器7连接;所述低通滤波器7与所述混频器5连接;所述混频器5与所述射频本振6和所述带通滤波器4连接;所述带通滤波器4与所述功率放大器3连接;所述功率放大器3与所述调制开关模块2连接;The digital-to-
所述功率放大器3能够对导航信号进行功率放大;The
所述带通滤波器4选取混频后的高频导航信号,抑制不需要的边带;The
所述混频器5将中频导航信号变换至高频;The
所述射频本振6为混频器提供本地振荡信号;The radio frequency
所述低通滤波器7过滤掉数模转换后的导频信号中的高频分量;The low-
所述数模转换器8将数字导航信号转换成模拟导航信号;The digital-to-
所述接收链路19包括:低噪声放大器11、混频器12、射频本振13、低通滤波器14、驱动放大器15和模数转换器16;The receiving
所述模数转换器16与所述驱动放大器15连接;所述驱动放大器15与所述低通滤波器14连接;所述低通滤波器14与所述混频器12连接;所述混频器12与所述射频本振13和所述低噪声放大器11连接;所述低噪声放大器11与所述接收天线10连接;The analog-to-
所述低噪声放大器11能够对接收的导航信号进行低噪声放大;The low-
所述混频器12能够将射频的导航信号混频至中频;The
所述射频本振13能够为接收混频器提供本地振荡信号;The radio frequency
所述低通滤波器14能够过滤掉混频后的导航信号中的高频分量;The low-
所述驱动放大器15能够对混频后的导航信号进行驱动放大,使得输出信号满足模数转换器16的输入量程;The
所述数模转换器16能够将接收的模拟导航信号转换为数字信号。The digital-to-
实施例2Example 2
实施例2是实施例1的变化例Example 2 is a modification of Example 1
本发明的基本原理是在基站端对导航进行周期性空时调制。经过周期性空时调制的导航信号中,包含基波分量与谐波分量,并通过基站端的天线阵列向空间辐射。在空间不同方位,接收到的导航信号中的基波和谐波分量是不同的。因此,在移动端通过分析接收到的导航信号中的基波分量与谐波分量的信号,就可估计出其相对于导航基站的方位角与俯仰角。若移动端同时测量其相对于两个或多个导航基站的方位角与俯仰角,在已知导航基站位置的条件下,利用角度交叉定位的方法,就可测得移动端的三维坐标,实现导航和定位。The basic principle of the present invention is to perform periodic space-time modulation on navigation at the base station. The periodic space-time modulated navigation signal contains fundamental and harmonic components, and is radiated into space through the antenna array at the base station. In different spatial orientations, the fundamental and harmonic components in the received navigation signals are different. Therefore, by analyzing the signals of fundamental wave components and harmonic components in the received navigation signal at the mobile terminal, the azimuth angle and pitch angle relative to the navigation base station can be estimated. If the mobile terminal simultaneously measures its azimuth and pitch angles relative to two or more navigation base stations, under the condition that the positions of the navigation base stations are known, the three-dimensional coordinates of the mobile terminal can be measured by using the angle cross positioning method to realize navigation. and positioning.
一种基于空时调制的区域导航定位系统,其工作过程是:导航基站产生数字导航信号,其中包含导航基站的位置等信息。经过数模转换、上变频、滤波和功率放大后,由调制开关模块进行周期性空时调制。经过周期性空时调制的导航信号中包含基波分量与谐波分量,并由天线阵列向空间辐射。在移动端,接收到导航信号后,经过低噪声放大、下变频、滤波和驱动放大后,由模数转换器将其转换为数字导航信号。在数字域内,一方面对导航信号进行解调,获取当前导航基站的位置等信息;一方面分析接收的导航信号中的基波与谐波分量,估计移动端相对于导航基站的方位角与俯仰角。在获取两个或多个导航基站的位置,以及移动端相对于导航基站的方位角和俯仰角后,通过角度交叉定位的方位,解算移动端当前的三维坐标,实现移动端的导航和定位。An area navigation and positioning system based on space-time modulation, the working process of which is as follows: a navigation base station generates a digital navigation signal, which contains information such as the position of the navigation base station. After digital-to-analog conversion, frequency up-conversion, filtering and power amplification, periodic space-time modulation is performed by the modulation switch module. The periodic space-time modulated navigation signal contains fundamental and harmonic components, and is radiated into space by the antenna array. At the mobile terminal, after receiving the navigation signal, it is converted into a digital navigation signal by an analog-to-digital converter after low-noise amplification, down-conversion, filtering and drive amplification. In the digital domain, on the one hand, the navigation signal is demodulated to obtain information such as the position of the current navigation base station; on the other hand, the fundamental wave and harmonic components in the received navigation signal are analyzed to estimate the azimuth and pitch of the mobile terminal relative to the navigation base station. horn. After obtaining the positions of two or more navigation base stations, as well as the azimuth and pitch angles of the mobile terminal relative to the navigation base stations, the current three-dimensional coordinates of the mobile terminal are solved through the azimuth of the angle cross positioning to realize the navigation and positioning of the mobile terminal.
假设导航基站端采用三单元天线阵列并呈L型排列,分析导航与定位过程如下:Assuming that the navigation base station adopts a three-element antenna array and is arranged in an L-shape, the analysis of the navigation and positioning process is as follows:
设天线阵列的三个天线单元分别为E1,E2,E3,其位置分别为:Let the three antenna elements of the antenna array be E1, E2, and E3 respectively, and their positions are:
E1[D1,0,0],E2[0,0,0],E3[0,D2,0];调制开关网络控制发射的导航信号周期性地接通三个天线单元。在一个调制周期Tp内,(0,Tp/3]时间内接通E1,(Tp/3,2Tp/3]内接通E2,(2Tp/3,Tp]内接通E3。发射的导航信号为载频为Fc的窄带信号,为分析方便,将其视为点频信号,则发射的导航信号为:E1[D1,0,0], E2[0,0,0], E3[0,D2,0]; the modulation switch network controls the transmitted navigation signal to periodically turn on the three antenna units. In one modulation period T p , E1 is turned on within (0, T p /3], E2 is turned on within (T p /3, 2T p /3], and E2 is turned on within (2T p /3, T p ]. E3. The transmitted navigation signal is a narrow-band signal with a carrier frequency of Fc . For the convenience of analysis, it is regarded as a point frequency signal, and the transmitted navigation signal is:
其中,A为发射的导航信号的幅度,m表示周期序号,为整数。Δφi,i=1,2,3为导航信号由于空时调制产生的相位,其值可用下式计算:Among them, A is the amplitude of the transmitted navigation signal, and m is the cycle number, which is an integer. Δφ i , i=1, 2, 3 is the phase of the navigation signal due to space-time modulation, and its value can be calculated by the following formula:
其中,xi,yi,zi,i=1,2,3为三个天线单元的坐标。θ为移动端相对于导航基站的俯仰角,为方位角。λ表示波长,在导航基站端,第i个天线单元上发射的信号为:Wherein, x i , y i , z i , i=1, 2, 3 are the coordinates of the three antenna elements. θ is the pitch angle of the mobile terminal relative to the navigation base station, is the azimuth angle. λ represents the wavelength. At the navigation base station, the signal transmitted by the i-th antenna unit is:
周期信号Si(t)可用傅里叶级数展开,假设其基波分量以及第一次、第二次谐波分量的傅里叶系数分别为ai,0,ai,1,ai,2,i=1,2,3。在移动端,对接收的导航信号进行傅里叶变换,得到导航信号中的基波分量γ0,以及第一、二次谐波分量γ1和γ2。接收的导航信号中的基波分量和谐波分量可以看成是导航基站端的三个天线单元上发射的基波分量与谐波分量在空间中的叠加,因此有下列的线性方程组:The periodic signal S i (t) can be expanded by Fourier series, assuming that the Fourier coefficients of its fundamental component and the first and second harmonic components are a i,0 , a i,1 , a i respectively ,2 ,i=1,2,3. At the mobile terminal, Fourier transform is performed on the received navigation signal to obtain the fundamental component γ 0 , and the first and second harmonic components γ 1 and γ 2 in the navigation signal. The fundamental and harmonic components in the received navigation signal can be regarded as the superposition in space of the fundamental and harmonic components emitted by the three antenna units at the navigation base station, so there are the following linear equations:
其中,Ar为传播路径带来的损耗量。由于上式左边的矩阵是与调制时序有关的已知量,上式右边的向量可通过对接收的导航信号进行傅里叶变换求得,因此求解线性方程组如下:Among them, Ar is the loss caused by the propagation path. Since the matrix on the left side of the above equation is a known quantity related to the modulation timing, the vector on the right side of the above equation can be obtained by performing Fourier transform on the received navigation signal, so the linear equations are solved as follows:
其中,D1表示天线单元E1的横坐标,D2表示天线单元E2的纵坐标。等式左边的向量包含方位角与俯仰角信息;等式右边的矩阵可由调制时序计算,为已知量;等式右边的向量可通过对接收的导航信号进行傅里叶变换得到。因此,求解式所示的线性方程组,可求出方位角和俯仰角θ的值。Among them, D 1 represents the abscissa of the antenna element E 1 , and D 2 represents the ordinate of the antenna element E 2 . The vector on the left side of the equation contains the azimuth and pitch angle information; the matrix on the right side of the equation can be calculated from the modulation timing and is a known quantity; the vector on the right side of the equation can be obtained by Fourier transforming the received navigation signal. Therefore, by solving the system of linear equations shown in Eq., the azimuth angle can be obtained and the value of the pitch angle θ.
移动端同时对接收的导航信号进行解调,获得导航基站的位置等信息。若移动端接收到两组或以上的导航基站的信号,并进行测向得到移动端相对于导航基站的俯仰角和方位角。同时,移动端对导航信号进行解调,得到两组或以上的导航基站的位置能信息,即可通过角度交叉定位的方法求解移动端的三维位置坐标,实现移动端的导航和定位,如图5所示。At the same time, the mobile terminal demodulates the received navigation signal to obtain information such as the location of the navigation base station. If the mobile terminal receives signals from two or more sets of navigation base stations, and performs direction finding to obtain the pitch and azimuth angles of the mobile terminal relative to the navigation base stations. At the same time, the mobile terminal demodulates the navigation signal to obtain the position energy information of two or more sets of navigation base stations, and then the three-dimensional position coordinates of the mobile terminal can be solved by the method of angle cross positioning to realize the navigation and positioning of the mobile terminal, as shown in Figure 5. Show.
实施例3Example 3
实施例3是实施例2和/或实施例1的变化例Example 3 is a variation of Example 2 and/or Example 1
移动端测量相对于导航基站的方位角与俯仰角The mobile terminal measures the azimuth and pitch angles relative to the navigation base station
假设导航基站发射载频为1GHz的窄带信号。导航基站的天线阵列包含三个天线单元,并且呈L形分布,三个天线单元为E1、E2和E3。其中,E1与E2,E2与E3之间的距离均为15cm(半波长)。发射的导航信号经过周期性空时调制,再由天线阵列向空间辐射。其中,调制周期为1us,在前三分之一个周期,导航信号馈入E1单元;中间三分之一个周期,导航信号馈入E2单元;后三分之一个周期,导航信号馈入E3单元。共向空间辐射10个调制周期的导航信号,信噪比为20dB。It is assumed that the navigation base station transmits a narrowband signal with a carrier frequency of 1 GHz. The antenna array of the navigation base station includes three antenna units and is distributed in an L shape, and the three antenna units are E1, E2 and E3. Wherein, the distances between E1 and E2, and E2 and E3 are all 15 cm (half wavelength). The transmitted navigation signal undergoes periodic space-time modulation, and is then radiated into space by the antenna array. Among them, the modulation period is 1us. In the first third of the period, the navigation signal is fed into the E1 unit; in the middle one third of the period, the navigation signal is fed into the E2 unit; in the last third of the period, the navigation signal is fed into the E2 unit. Unit E3. The navigation signal with 10 modulation cycles is radiated in the co-directional space, and the signal-to-noise ratio is 20dB.
设移动端相对于基站端的方位角为65°,俯仰角为20度。在移动端,天线接收到经过空时调制的导航信号,其频谱如图3所示。从图中可以看出,接收的导航信号的基波分量在1GHz处,第一、二次谐波分量分别在1.001GHz、1.002GHz处。将得到的基波分量与第一、第二次谐波分量代入式和式计算移动端相对于基站端的方位角和俯仰角,得到方位角为65.05°,俯仰角为20.00度。Assume that the azimuth angle of the mobile terminal relative to the base station terminal is 65°, and the pitch angle is 20°. At the mobile terminal, the antenna receives the space-time modulated navigation signal, and its frequency spectrum is shown in Figure 3. As can be seen from the figure, the fundamental component of the received navigation signal is at 1 GHz, and the first and second harmonic components are at 1.001 GHz and 1.002 GHz, respectively. Substitute the obtained fundamental wave component and the first and second harmonic components into the formula and calculate the azimuth angle and pitch angle of the mobile terminal relative to the base station terminal, and the azimuth angle is 65.05° and the pitch angle is 20.00 degrees.
仍设置移动端相对于基站端的方位角为65°,俯仰角为20度。设置信噪比从-10dB到+20dB,步进为2dB。在每个信噪比条件下,分别进行1000次蒙特卡洛仿真,计算估计得到的方位角与俯仰角的均方误差,得到的仿真结果如图4所示。从图4中可以看出,当信噪比从-10dB增加到+20dB时,方位角与俯仰角的均方估计误差均从约1.2°下降至0.1°。It is still set that the azimuth angle of the mobile terminal relative to the base station terminal is 65°, and the pitch angle is 20 degrees. Set the SNR from -10dB to +20dB in 2dB steps. Under each signal-to-noise ratio condition, 1000 times of Monte Carlo simulations were performed to calculate the mean square error of the estimated azimuth and pitch angles. The simulation results obtained are shown in Figure 4. It can be seen from Figure 4 that when the SNR increases from -10dB to +20dB, the mean square estimation errors of both the azimuth and pitch angles decrease from about 1.2° to 0.1°.
移动端利用两个导航基站的信号实现导航和定位The mobile terminal uses the signals of the two navigation base stations to achieve navigation and positioning
设置两个导航基站的位置分别为[0,-500m,0],[0,500m,0],移动台的真实位置为[100m,200m,80m]。第一个导航基站的天线阵列为三单元L形,单元之间的距离为半波长,发射的窄带导航信号的载频为1GHz。调制开关网络控制导航信号周期性地接通三个天线单元,其调制周期为1us。在前1/3us内,导航信号接通天线单元1;中间1/3us内,导航信号接通天线单元2;后1/3us内,导航信号接通天线单元3。同位,将导航基站的位置信号进行编码,并进行BPSK调制,符号周期为10us。在一个码元周期内,共发射10个调制周期的导航信号。The positions of the two navigation base stations are set as [0,-500m,0], [0,500m,0] respectively, and the real position of the mobile station is [100m, 200m, 80m]. The antenna array of the first navigation base station is a three-unit L-shaped, the distance between the units is half a wavelength, and the carrier frequency of the transmitted narrow-band navigation signal is 1GHz. The modulation switch network controls the navigation signal to turn on the three antenna units periodically, and its modulation period is 1us. In the first 1/3us, the navigation signal is connected to the
同样的,对于第二个导航基站,其天线阵列配置、发射的导航信号及调制方式均与第一个导航基站相同,不同之处是发射的导航信号的载频为1.1GHz,用于在移动端实现频分同时接收。Similarly, for the second navigation base station, the antenna array configuration, the transmitted navigation signal and the modulation method are the same as those of the first navigation base station, the difference is that the carrier frequency of the transmitted navigation signal is 1.1GHz, which is used for mobile The terminal realizes frequency division simultaneous reception.
设接收的导航信号的信噪比为20dB,对接收的导频信号进行频谱分析并计算移动端相对于两个导航基站的方位角与俯仰角,得到的仿真结果如下。移动端相对于第一个导航基站的俯仰角与方位角的真实值为(83.55°,81.87°),测量值为(83.91°,81.86°);相对于第二个导航基站的俯仰角与方位角的真实值为(75.80°,-71.57°),测量值为(75.87°,-71.59°)。假设移动端能正确解调得到两个导航基站的位置,利用角度交叉定位方位可解算得到当前移动端的三维坐标为[99.67m,203.84m,77.13m]。与真实值相比,空间距离误差为4.8m。Assuming that the signal-to-noise ratio of the received navigation signal is 20dB, the spectrum analysis of the received pilot signal is performed and the azimuth and pitch angles of the mobile terminal relative to the two navigation base stations are calculated. The simulation results obtained are as follows. The actual value of the pitch angle and azimuth angle of the mobile terminal relative to the first navigation base station is (83.55°, 81.87°), and the measured value is (83.91°, 81.86°); the pitch angle and azimuth angle relative to the second navigation base station are The true value of the angle is (75.80°, -71.57°) and the measured value is (75.87°, -71.59°). Assuming that the mobile terminal can correctly demodulate the positions of the two navigation base stations, the three-dimensional coordinates of the current mobile terminal can be calculated by using the angle cross positioning azimuth to be [99.67m, 203.84m, 77.13m]. Compared with the true value, the spatial distance error is 4.8m.
在上述条件下,进行100次蒙特卡洛仿真。得到的定位误差如图6所示。经计算得到定位误差的均方根值为2.55m。Under the above conditions, 100 Monte Carlo simulations were performed. The resulting positioning errors are shown in Figure 6. The root mean square value of the positioning error is calculated to be 2.55m.
在本申请的描述中,需要理解的是,术语“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本申请和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本申请的限制。In the description of this application, it should be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", The orientation or positional relationship indicated by "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the accompanying drawings, which is only for the convenience of describing the present application and simplifying the description, rather than indicating or implying the indicated device. Or elements must have a particular orientation, be constructed and operate in a particular orientation, and therefore should not be construed as a limitation of the present application.
本领域技术人员知道,除了以纯计算机可读程序代码方式实现本发明提供的系统、装置及其各个模块以外,完全可以通过将方法步骤进行逻辑编程来使得本发明提供的系统、装置及其各个模块以逻辑门、开关、专用集成电路、可编程逻辑控制器以及嵌入式微控制器等的形式来实现相同程序。所以,本发明提供的系统、装置及其各个模块可以被认为是一种硬件部件,而对其内包括的用于实现各种程序的模块也可以视为硬件部件内的结构;也可以将用于实现各种功能的模块视为既可以是实现方法的软件程序又可以是硬件部件内的结构。Those skilled in the art know that, in addition to implementing the system, device and each module provided by the present invention in the form of pure computer readable program code, the system, device and each module provided by the present invention can be completely implemented by logically programming method steps. The same program is implemented in the form of logic gates, switches, application specific integrated circuits, programmable logic controllers, and embedded microcontrollers, among others. Therefore, the system, device and each module provided by the present invention can be regarded as a kind of hardware component, and the modules used for realizing various programs included in it can also be regarded as the structure in the hardware component; A module for realizing various functions can be regarded as either a software program for realizing a method or a structure within a hardware component.
以上对本发明的具体实施例进行了描述。需要理解的是,本发明并不局限于上述特定实施方式,本领域技术人员可以在权利要求的范围内做出各种变化或修改,这并不影响本发明的实质内容。在不冲突的情况下,本申请的实施例和实施例中的特征可以任意相互组合。Specific embodiments of the present invention have been described above. It should be understood that the present invention is not limited to the above-mentioned specific embodiments, and those skilled in the art can make various changes or modifications within the scope of the claims, which do not affect the essential content of the present invention. The embodiments of the present application and features in the embodiments may be combined with each other arbitrarily, provided that there is no conflict.
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