基于太阳敏感器的静止轨道卫星轨道估计方法研究

Abstract

Abstract: In order to estimate orbit position of GEO satellites using existing on-board equipments, this paper describes the system composed of sun sensors and earth sensors. According to nature of orbit of GEO satellites combined with Hill equation, state equations and measurement equations of this system are established by using measurement information from sun sensors and earth sensors, as well as orbit perturbation characteristics. Simulation results show that longitude’s excursion of the satellite can be accurately estimated by this method, and it is a feasible autonomous navigation method for GEO satellites.

Key words: GEO satellite')">GEO satellite, sun sensor, earth sensor, ')">orbit’s estimation

CLC Number:

V249.32

XU Jingyu, GAO Yijun. Sun Sensor-Based Orbit Position Estimating Method for GEO Satellites[J].Aerospace Contrd and Application, 2009, 35(6): 41-44.

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/ / Recommend GEO satellite; sun sensor; earth sensor; orbit’s estimation”. Please open it by linking:http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/abstract/abstract9373.shtml" name="neirong"> GEO satellite; sun sensor; earth sensor; orbit’s estimation">

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2009/V35/I6/41

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Sun Sensor-Based Orbit Position Estimating Method for GEO Satellites

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