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卫星导航接收天线相位中心的测量 被引量:10
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作者 杨社年 王迎节 《无线电工程》 2006年第5期33-35,共3页
通常天线的相位中心与其几何中心是不一致的。为了确立天线相位中心与几何中心位置的相对偏差,提出了采用室内测量法和室外测量法对天线相位中心进行测量,描述了2种测量方法的测量原理。详细介绍了在测量过程中找出天线相位中心的方法步... 通常天线的相位中心与其几何中心是不一致的。为了确立天线相位中心与几何中心位置的相对偏差,提出了采用室内测量法和室外测量法对天线相位中心进行测量,描述了2种测量方法的测量原理。详细介绍了在测量过程中找出天线相位中心的方法步骤,并指出了2种测量方法的特点。 展开更多
关键词 卫星导航接收天线 天线相位中心 天线几何中心 室内测量法 室外测量法
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一种GPS天线相位中心偏移量的测定与计算方法 被引量:5
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作者 戴水财 刘庆元 +1 位作者 张学庄 王潜心 《矿山测量》 2005年第1期17-18,24,共3页
文中结合GPS接收机天线检测实例,提出了一种新的GPS天线相位中心偏移量的测定与计算方法,并从空间 基线向量的角度对其进行了论证。该法不仅能测定GPS天线相位中心偏移量,还能利用测定结果对空间基线向量 进行改正。经实例测试,按... 文中结合GPS接收机天线检测实例,提出了一种新的GPS天线相位中心偏移量的测定与计算方法,并从空间 基线向量的角度对其进行了论证。该法不仅能测定GPS天线相位中心偏移量,还能利用测定结果对空间基线向量 进行改正。经实例测试,按文中方法测得的三台GPS接收机天线相位中心偏差分别为2.9mm、4.3mm和3.7mm。 由测试实例可知:文中的测定与计算方法简便易行,实用性强,是一种行之有效的GPS天线相位中心偏移量检测方 法。 展开更多
关键词 GPS接收机 天线相位中心 天线几何中心 偏移
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基于D-optimality准则的多输入多输出雷达阵列设计
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作者 顾帅楠 郑娜娥 秦文利 《太赫兹科学与电子信息学报》 北大核心 2018年第3期423-430,共8页
为了最小化参数估计的均方误差,提出了基于D-optimality准则(DOBC)的多输入多输出雷达天线几何设计方法。严格推导了天线几何在DOBC准则下需要满足的约束条件;进行了敏感性分析,DOBC准则下的天线几何只与目标方位角之差有关,而与具体的... 为了最小化参数估计的均方误差,提出了基于D-optimality准则(DOBC)的多输入多输出雷达天线几何设计方法。严格推导了天线几何在DOBC准则下需要满足的约束条件;进行了敏感性分析,DOBC准则下的天线几何只与目标方位角之差有关,而与具体的方位角值无关;并推导了远场条件下参数估计的克拉美罗界(CRLB),DOBC准则可以看成一种修正的CRLB,其为最大似然估计算法提供了更严格的下界约束。仿真结果表明,与最小冗余阵列、均匀阵列相比,DOBC准则下的天线几何具有更优越的参数估计性能,且其不受阵列孔径的约束,可以通过扩大孔径,进一步提高分辨力。但随着孔径的提高,方向图的伪峰值会升高,在低信噪比条件下,会造成很大的参数估计误差,因此需要根据实际应用需求,选择合适的孔径大小。 展开更多
关键词 多输入多输出雷达 天线几何 D-optimality准则 敏感性 克拉美罗界
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北斗导航接收机综合测试微波暗室结构设计分析
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作者 蔡金珠 《环境技术》 2021年第5期32-34,共3页
针对北斗卫星导航接收机测试任务需求,给出了卫星导航接收机天线相位中心精确测量,综合指标测试、抗干扰验证的综合性微波暗室结构估算方法,并给出了一个具体事例。
关键词 卫星导航接收机 天线相位中心 接收天线几何中心 多波束天线
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A Study on The Multi-Antenna Geometrical Depolarization Channel Modeling 被引量:2
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作者 SUN Xuehong YANG Xiaoli +2 位作者 ZENG Zhimin ZHANG Cheng BAI Bing 《China Communications》 SCIE CSCD 2016年第3期105-114,共10页
The traditional geometrical depolarization model that single transmitter to single receiver provides a simple method of polarization channel modeling. It can obtain the geometrical depolarization effect of each path i... The traditional geometrical depolarization model that single transmitter to single receiver provides a simple method of polarization channel modeling. It can obtain the geometrical depolarization effect of each path if known the antenna configuration, the polarization field radiation pattern and the spatial distribution of scatters. With the development of communication technology, information transmission spectrum is more and more scarce. The original model provides only a single channel polarization state, so the information will be limited that the polarization state carries in the polarization modulation. The research is so significance that how to carries polarization modulation information by using multi-antenna polarization state. However, the present study shows that have no depolarization effect model for multi-antenna systems. In this paper, we propose a multi-antenna geometrical depolarization model. On the basis of a single antenna to calculate the depolarization effect of the model, and through simulation to analysis the main factors that influence the depolarization effect. This article provides a multi-antenna geometrical depolarization channel modeling that can applied to large-scale array antenna, and to some extent increase the speed of information transmission. 展开更多
关键词 large-scale array antenna multi-antenna channel modeling depolarization effect cross polarization discrimination
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Development simulation of an inflatable membrane antenna based on extended position-based dynamics
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作者 Haijun Peng Na Li +2 位作者 Fei Li Liang Zhang Kaijun Dong 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2022年第7期135-147,I0003,共14页
Inflatable membrane antennas have been extensively applied in space missions;however,the simulation methods are not perfect,and many simulation methods still have many difficulties in accuracy,efficiency,and stability... Inflatable membrane antennas have been extensively applied in space missions;however,the simulation methods are not perfect,and many simulation methods still have many difficulties in accuracy,efficiency,and stability.Therefore,the extended position-based dynamics(XPBD)method is employed and improved for the simulation of folded inflatable structures in this paper.To overcome the problem that the original XPBD method with only geometric constraints does not contain any mechanical information and cannot reflect the mechanical characteristics of the structure,we improve the XPBD method by introducing the strain energy constraint.Due to the complicated nonlinear characteristics of the membrane structures,the results with the traditional finite element method(Abaqus)cannot converge,while the tension field theory(TFT)can,but some pretreatments are needed.Compared with them,the method in this paper is simple and has better stability to accurately predict the displacement,stress,and wrinkle region of the membrane structure.In addition,the present method is also compared with the experiment in the reference to verify the feasibility of the folded tube simulation.Finally,the present method is applied to simulate inflatable membrane antennas and analyze the deployable driving force and deployable process sequence of each component. 展开更多
关键词 Position-based dynamics Physical simulation Pneumatic membrane structure Aerospace inflatable antenna
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