深空上行链路抛物面天线发射阵列的系统概念

W. Hurd
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引用次数: 8

摘要

与美国宇航局深空网络目前使用的34米和70米天线相比,抛物面天线相控阵是一种潜在的低成本上行传输方式,可以向遥远的航天器提供上行传输。一个大的发射阵列可以在航天器紧急情况需要时提供非常高的EIRP,例如相当于从70米天线辐射1兆瓦。通过将阵列划分成更小的阵列,同时为多个航天器提供日常支持,实现了成本效益。这些天线的直径可能小到12米,多达100个天线覆盖0.5公里到1公里的范围。这种阵列在相位对准方面提出了重大的技术挑战,相位对准必须保持在接近1mm的位置。这个概念需要一个非常稳定的系统,具有精确已知的天线相位中心位置。该系统首先通过从所有天线发射来校准,并在位于单个天线远场的目标处观察信号。然后天线被指向作战目标,信号相位和时间延迟被设置为在目标方向上加强。这需要精确地了解目标方向并计算所需相位。系统必须在所有方向和校准之间的时间内保持相位稳定,这至少是一天。本文提出了系统的概念,识别了主要误差源,建立了粗略的误差预算,并讨论了系统的关键要素。提出了一种以卫星为雷达目标的标定方法。性能目标是在良好天气下实现小于0.2 dB的组合损耗,在除极端恶劣天气外的所有天气下实现小于1 dB的组合损耗
本文章由计算机程序翻译,如有差异,请以英文原文为准。
System concepts for transmit arrays of parabolic antennas for deep space uplinks
Phased arrays of parabolic antennas are a potentially lower-cost way to provide uplink transmission to distant spacecraft, compared to the 34-m and 70-m antennas now used by the NASA Deep Space Network. A large transmit array could provide very high EIRP when needed for spacecraft emergencies, such as the equivalent of 1 MW radiated from a 70-m antenna. Cost-effectiveness is realized by dividing the array into smaller arrays to provide routine support to many spacecraft simultaneously. The antennas might be as small as 12-m in diameter, with as many as 100 antennas covering an area of 0.5 km to 1 km in extent. Such arrays present significant technical challenges in phase alignment, which must be maintained at close to 1 mm. The concept requires a very stable system with accurately known antenna phase center locations. The system is first calibrated by transmitting from all antennas, and observing the signals at a target located in the far fields of the individual antennas. The antennas are then pointed to the operational targets, with the signal phases and time delays set to reinforce in the target directions. This requires accurate knowledge of the target directions and calculation of the required phases. The system must be phase-stable for all directions and over the time between calibrations, which is desired to be at least one day. In this paper, a system concept is presented, the major error sources are identified, a rough error budget is established, and key elements of the system are discussed. A calibration method is recommended which uses satellites as radar targets. The performance goal is to achieve a combining loss of less than 0.2 dB in good weather, and of less than 1 dB in all but extremely bad weather
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