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A Novel Location-Awareness Method Using CubeSats for Locating the Spot Beam Emitters of Geostationary Communications Satellites

机译:一种使用CubeSat定位地球静止通信卫星点波束发射器的新颖位置感知方法

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摘要

As more spacecraft are launched into the Geostationary Earth Orbit (GEO) belt, the possibility of fatal collisions or unnecessary interference between spacecraft increases. In this paper, a new location-awareness method that uses CubeSats is proposed to assist with radiofrequency (RF) domain verification by means of awareness and identification of the positions of the spot beam emitters of communications satellites in geostationary orbit. By flying a CubeSat (or a constellation of CubeSats) through the coverage area of a spot beam, the spot beam emitter's position is identified and the spot beam's pattern knowledge is characterized. The geometry, the equations of motion of the spacecraft, the measurement process, and the filtering equations in a location system are addressed with respect to the location methods investigated in this study. A realistic scenario in which a CubeSat receives signals from GEO communications satellites is simulated using the Systems Tool Kit (STK). The results of the simulation and the analysis presented in this study provide a thorough verification of the performance of the location-awareness method.
机译:随着越来越多的航天器被发射到地球静止轨道(GEO)带中,致命的碰撞或航天器之间不必要的干扰的可能性增加。在本文中,提出了一种使用CubeSats的新的位置感知方法,以通过感知和识别对地静止轨道上通信卫星点波束发射器的位置来辅助射频(RF)域验证。通过使CubeSat(或CubeSat星座)在点光束的覆盖区域内飞行,可以识别点光束发射器的位置,并表征点光束的模式知识。相对于本研究中研究的定位方法,解决了定位系统中的几何形状,航天器的运动方程,测量过程以及滤波方程。使用系统工具包(STK)模拟了CubeSat从GEO通信卫星接收信号的实际情况。本研究中提供的仿真和分析结果为位置感知方法的性能提供了全面的验证。

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