Circumlunar Spacecraft Navigation Using the Measurements from Global Navigation Satellite Systems GLONASS, GPS, Galileo and BeiDou

被引：3
|
作者：
Mikrin E.A. [1 ]
Mikhailov M.V. [1 ]
Orlovskii I.V. [1 ]
Rozhkov S.N. [1 ]
Semenov A.S. [1 ]
Krasnopol’skii I.A. [1 ]
机构：
[1] Korolev Rocket and Space Public Corporation Energia (RSC Energia), Korolev, 141070, Moscow oblast
来源：
Gyroscopy and Navigation | 2019年 / 10卷 / 04期
关键词：
BeiDou; GALILEO; GLONASS; GPS; measurement; model; navigation; satellite navigation on the Moon;
D O I：
10.1134/S2075108719040126
中图分类号：
学科分类号：
摘要：
Abstract: The study makes an approach to the problem of circumlunar spacecraft navigation using the measurements from the global navigation satellite systems (GNSS) GLONASS, GPS, Galileo and BeiDou. Algorithms have been developed for determining the orbits of low- and high-orbit circumlunar spacecraft, based on the method of dynamic filtering of pseudo-range measurements from “reverse” navigation satellites (NS). The solution to the navigation problem has been simulated by the measurements from four GNSS, and by those from the NS of GLONASS and GPS only. Accuracy and dynamic characteristics of the obtained solutions have been determined and compared to similar solutions for geostationary spacecraft. © 2019, Pleiades Publishing, Ltd.
引用
收藏
页码：187 / 195
页数：8
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