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GNSS Patch Antenna Design Parameter Optimization using FEKO, Design of Experiments P-Transform Technique

机译:GNSS补丁天线设计参数优化使用FEKO,实验设计和P变换技术

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The next generation of Automotive Radios, Navigation Systems, Connectivity, Connected Services, Positioning Services, Cloud Services, CV-X cellular network technologies, HD maps in autonomous domain needs and require an optimized and robust future GNSS (GPS and GLONASS) patch antenna solution to operate effectively and deliver services, features, functionality and that allows the V model process (Verification and Validation) of the above outlined items software stack at the engineering development component and vehicle level and as well as in the production intent vehicles out in the field.Conducted literature review and published paper studied however, observed that there is a problem related to the Center Frequency of 1.555 [GHz] GNSS antenna which has not been investigated. The proposed work involved a modeling of New GNSS (GPS and GLONASS) rectangular patch antenna. The design focus will be on the operating frequency range of 1.500 [GHz] to 1.610 [GHz] and FEKO 3D Electromagnetic simulation software package from Altair [4] will be used, Design of Experiments (DoE) [5], and as well as applying an optimization P-Transform algorithm [6] on the presented dual band GNSS (GPS and GLONASS) patch antenna passive gain. To be more direct, the GNSS microstrip patch antenna is designed to resonate and operate at 1.555 [GHz] frequency. The demonstrated GNSS patch antenna was designed to capture both the GPS and GLONASS signals and data targeting automotive and non-automotive industries as its intended application.Furthermore, the ground plane length, ground plane width and the substrate material dielectric constant design parameters were varied at each FEKO simulation run, in order to obtain the simulation of GNSS patch antenna passive gain output results for the purpose of the optimization study using P-Transform technique within the MATLAB environment. The presented GNSS patch antenna 2D far field and/or average passive gain measurement of GPS and GLONASS at carrier frequency of 1.555 [GHz] was plotted and analyzed. The computation and analysis involved taking the delta between elevation angle 30 and 90 degrees from the average passive gain graph and this step was conducted for 120 FEKO simulation iteration runs. In other words, for each FEKO simulation run the Far field (objective function) was computed separately unique for that specific design parameters and recorded in a lookup matrix. This four columns lookup matrix was called out for the purposes of the P-Transform algorithm utilization and execution within the MATLAB environment.To be more precise, the FEKO simulation studies were undertaken to determine the GNSS (GPS and GLONASS) patch antenna average passive gain, in turn we call it the Objection Function in which the P-Transform optimization process will be applied. Moreover, Design of Experiments (DoE) was applied on the presented GNSS patch antenna, in order to reduce the number of required simulation test runs and therefore improve the proposed antenna design cycle.
机译:下一代汽车收音机,导航系统,连接,连接服务,定位服务,云服务,CV-X蜂窝网络技术,高清地图在自治域的需求和要求的优化和强大的未来全球导航卫星系统(GPS和GLONASS)贴片天线解决方案有效运作和提供服务,特性,功能和允许V模型的过程(验证和确认)以上,以及在生产的工程开发组件和车身高度概括项目的软件堆栈和意图的车辆在外地然而,.Conducted文献综述和发表了研究观察到,关系到1.555中心频率的问题[千兆赫] GNSS天线,并没有受到调查。拟议的工作涉及新的全球导航卫星系统(GPS和GLONASS)的矩形贴片天线的造型。设计重点将放在1.500 [GHz]的操作频率范围,以1.610从牵牛星[GHz]的和FEKO 3D电磁仿真软件包[4]将被使用,实验设计(DOE)[5],和以及施加优化P-变换算法[6]上所呈现的双波段GNSS(GPS和GLONASS)的贴片天线的无源增益。为了更直接,所述GNSS微带贴片天线被设计成谐振在1.555 [GHz]的频率下操作。所表现出的GNSS贴片天线被设计为捕获两个GPS和GLONASS信号和数据靶向汽车和非汽车行业作为其预期application.Furthermore,接地面长度,接地平面宽度和基片材料的介电常数设计参数在改变每个FEKO模拟运行,以便获得的GNSS贴片天线被动增益输出结果的仿真使用MATLAB环境内变换P-技术优化研究的目的。所呈现的GNSS贴片天线2D远场和/或GPS和GLONASS的平均被动增益测量在1.555 [GHz]的载波频率进行作图和分析。计算和分析涉及服用仰角30度和90度之间的增量从平均被动增益图表和该步骤120个FEKO仿真迭代运行进行。换言之,对于每个模拟FEKO运行远场(目标函数)被分别计算为独特的具体设计参数和记录在查找矩阵。这四列查找矩阵被叫出而言的P型变换的MATLAB environment.To内算法利用和执行更精确地,所述FEKO模拟研究开展了来确定GNSS(GPS和GLONASS)的贴片天线的平均增益被动反过来,我们把它叫做目标函数,其中P-变换优化过程将被应用。此外,(DOE)实验设计涂布于所呈现的GNSS贴片天线中,为了减少所需的模拟测试运行的数目,并因此提高所提出的天线设计周期。

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