在低轨道卫星系统中使用延迟和多普勒测量来确定用户位置

Y. Vasavada, Deepak Arur, C. Ravishankar, C. Barnett
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引用次数: 1

摘要

虽然通常依赖外部全球导航卫星系统(GNSS)解决方案来固定用户终端(UT)的位置,但在LEO卫星系统中自主固定UT位置是一个可处理的问题,具有系统效益。如果GNSS解决方案暂时(例如,由于初始GNSS位置固定的延迟)或长时间(由于重大中断或监管限制)不可用,或者如果系统安全策略不允许通过空中传输用户位置,则需要使用自主解决方案。在本文中,我们描述了两种非线性寻根算法(适用于UT或卫星网关(GW)),它们将物理层接收器的延迟和多普勒偏移测量作为输入,并生成用户位置(以及可选的速度)的估计作为输出。算法模拟结果表明,当UT对一颗以上卫星可见时,可以实现高精度估计(在不到10%的情况下位置误差超过1公里),而在单个卫星情况下,可以实现较低精度的结果(例如,位置误差超过2公里的机会约为20%)。
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User location determination using delay and Doppler measurements in LEO satellite systems
Although an external Global Navigational Satellite System (GNSS) solution is often relied upon for fixing the location of user terminals (UTs), fixing the UT position autonomously in LEO satellite systems is a tractable problem which has a system benefit. An autonomous solution comes to use if the GNSS solution becomes unavailable either temporarily (e.g., due to a delay in initial GNSS position fix) or for prolonged periods (due to major outages or regulatory constraints), or if the system security policies do not allow transmission of the user position over the air. In this paper, we describe two nonlinear root-finding algorithms (applicable either at the UT or at the satellite Gateway (GW)) that take as the inputs the delay and Doppler offset measurements from the physical layer receiver and generate an estimate of the user location (and optionally velocity) as the output. Algorithm simulation results suggest that a high accuracy estimate (in which position error exceeds 1 km in less than 10% cases) is possible when UT has visibility to more than one satellite, while less accurate results (e.g., ∼ 20% chance of position errors exceeding 2 km) are achievable in a single satellite scenario.
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