Influence of Antenna Configuration and Relative Rotations on Intersatellite Distance Precision of Two Satellites Flying in Formation

Elkedrouci Kamel, Liu Rongke, Yang Xinxin, Mu Weiqing
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Abstract

Formation flying consists of replacing a complex and expensive conventional satellite, by a set of smaller satellites, able of carrying out the same functions with better performance and at a lower cost. Therefore, satellites in formation must precisely control their positions and orientations relative to each other in the group, as if they were a single large satellite. This need for precision rises especially when these satellites are operating in close formation. The location and the configuration of the antennas is one crucial among other factors influencing the precision of the relative position. This paper investigates the influence of the configuration of the antennas and the relative attitude on the precision of the relative position between two satellites flying in formation. The first satellite holds three transmitting antennas and the second satellite holds three receiving antennas, simulations results that changing the locations of these latter does have a minim impact on the precision of the relative position for a determined close intersatellite distance.
天线构型和相对旋转对编队飞行卫星间距离精度的影响
编队飞行是用一组更小的卫星取代一颗复杂而昂贵的传统卫星,这些卫星能够以更好的性能和更低的成本执行相同的功能。因此,在编队中的卫星必须精确地控制它们相对于其他卫星的位置和方向,就好像它们是一个单独的大卫星一样。特别是当这些卫星以紧密的队形运行时,对精度的要求就更高了。在影响相对位置精度的诸多因素中,天线的位置和结构是一个至关重要的因素。本文研究了天线构型和相对姿态对编队飞行的两颗卫星相对位置精度的影响。第一颗卫星拥有三个发射天线,第二颗卫星拥有三个接收天线,模拟结果表明,在确定的近星间距离内,改变后者的位置对相对位置的精度影响最小。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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