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Precise phase calibration of a controlled reception pattern GPS antenna for JPALS

机译:JPALS受控接收方向图GPS天线的精确相位校准

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The Joint Precision Approach and Landing System (JPALS) is being developed to provide navigation to support aircraft landings for the U.S. military. One variant of JPALS is the Shipboard Relative GPS (SRGPS), which will be implemented on an aircraft carrier. In order to meet strict accuracy, integrity, continuity, and availability goals in the presence of hostile jamming and in a harsh multipath environment, advanced technologies are required. One of those being studied is a controlled reception pattern antenna (CRPA) array with beam steering/adaptive forming capabilities. The Stanford University GPS Laboratory has developed a software tool to study CRPA algorithms and their effects on GPS signal and tracking characteristics. A testbed has been constructed to investigate hardware issues including the phase center offset of the antenna elements and mutual coupling effects. This testbed consists of a 3 element antenna array with a baseline of 1m, using high-quality survey-grade or lower-quality patch antennas. Data has been taken using this array in conjunction with sufficient satellite constellation and antenna array motion to ensure complete azimuth and elevation signal coverage. A carrier phase-based attitude determination algorithm was used to generate inter-antenna bias residuals, allowing characterization of the virtual phase center of the array. Repeating the testing procedure both with survey-grade antennas, for which the phase center characteristics are well known, and with a patch antenna possessing unknown phase center behavior, allows characterization of the azimuth- and elevation-dependent properties of the patch antenna phase center. In addition, mutual coupling effects have been investigated by adding inactive patch elements around the active patch antenna. All results are compared to predictions from detailed simulation of the patch antenna used using an EM modeling software package.
机译:正在开发联合精确进近和着陆系统(JPALS),以提供导航以支持美​​军飞机的着陆。 JPALS的一种变体是舰载相对GPS(SRGPS),它将在航空母舰上实现。为了在存在敌对干扰且在恶劣的多路径环境中达到严格的准确性,完整性,连续性和可用性目标,需要先进的技术。研究的对象之一是具有波束控制/自适应形成功能的受控接收模式天线(CRPA)阵列。斯坦福大学GPS实验室开发了一种软件工具,用于研究CRPA算法及其对GPS信号和跟踪特性的影响。已经构建了一个测试平台来研究硬件问题,包括天线元件的相位中心偏移和相互耦合效应。该测试台由一个3元素的天线阵列组成,其基线为1m,使用高质量的调查级或较低质量的贴片天线。使用该阵列结合足够的卫星星座和天线阵列运动来获取数据,以确保完整的方位角和仰角信号覆盖范围。基于载波相位的姿态确定算法用于生成天线间偏置残差,从而可以表征阵列的虚拟相位中心。重复测试过程既要使用众所周知的相位中心特性的测量级天线,又要使用具有未知相位中心特性的贴片天线,就可以表征贴片天线相位中心的方位角和仰角相关特性。另外,已经通过在有源贴片天线周围添加非有源贴片元件来研究互耦效应。将所有结果与使用EM建模软件包对使用的贴片天线进行详细仿真得到的预测结果进行比较。

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