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System overview on electromagnetic compensation for reflector antenna surface distortion

机译:用于反射器天线表面变形的电磁补偿系统概述

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摘要

The system requirements and hardware implementation for electromagnetic compensation of antenna performance degradations due to thermal effects was investigated. Future commercial space communication antenna systems will utilize the 20/30 GHz frequency spectrum and support very narrow multiple beams (0.3 deg) over wide angle field of view (15-20 beamwidth). On the ground, portable and inexpensive very small aperture terminals (VSAT) for transmitting and receiving video, facsimile and data will be employed. These types of communication system puts a very stringent requirement on spacecraft antenna beam pointing stability (less than .01 deg), high gain (greater than 50 dB) and very lowside lobes (less than -25 dB). Thermal analysis performed on the advanced communication technology satellite (ACTS) has shown that the reflector surfaces, the mechanical supporting structures and metallic surfaces on the spacecraft body will distort due thermal effects from a varying solar flux. The antenna performance characteristics (e.g., pointing stability, gain, side lobe, etc.) will degrade due to thermal distortion in the reflector surface and supporting structures. Specifically, antenna RF radiation analysis has shown that pointing error is the most sensitive antenna performance parameter to thermal distortions. Other antenna parameters like peak gain, cross polarization level (beam isolation), and side lobe level will also degrade with thermal distortions. In order to restore pointing stability and in general antenna performance several compensation methods were proposed. In general these compensation methods can be classified as being either of mechanical or electromagnetic type. This paper will address only the later one. In this approach an adaptive phased array antenna feed is used to compensate for the antenna performance degradation. Extensive work has been devoted to demonstrate the feasibility of adaptive feed compensation on space communication antenna systems. This paper addresses the system requirements for such a system and identify candidate technologies (analog and digital) for possible hardware implementation.
机译:研究了由于热效应而对天线性能下降进行电磁补偿的系统要求和硬件实现。未来的商用空间通信天线系统将利用20/30 GHz频谱,并在广角视场(15-20波束宽度)上支持非常窄的多波束(0.3度)。在地面上,将使用便携式和廉价的非常小孔径的终端(VSAT)来发送和接收视频,传真和数据。这些类型的通信系统对航天器天线波束指向稳定性(小于0.01度),高增益(大于50 dB)和非常低的旁瓣(小于-25 dB)提出了非常严格的要求。在先进通信技术卫星(ACTS)上进行的热分析表明,航天器主体上的反射器表面,机械支撑结构和金属表面将因变化的太阳通量产生的热效应而变形。天线性能特征(例如,指向稳定性,增益,旁瓣等)将由于反射器表面和支撑结构中的热变形而降低。具体而言,天线RF辐射分析表明,指向误差是对热变形最敏感的天线性能参数。其他天线参数(例如峰值增益,交叉极化电平(波束隔离)和旁瓣电平)也会因热变形而降低。为了恢复指向稳定性和一般的天线性能,提出了几种补偿方法。通常,这些补偿方法可以分类为机械或电磁类型。本文将仅针对后一篇。在这种方法中,自适应相控阵天线馈源用于补偿天线性能下降。已经进行了大量的工作来证明在空间通信天线系统上进行自适应馈电补偿的可行性。本文介绍了这种系统的系统要求,并确定了可能的硬件实现方法的候选技术(模拟和数字)。

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