| 卫星轨道变化规律的综合分析 |
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| 引用本文： | 刘世元 刘春保 刘林. 卫星轨道变化规律的综合分析[J]. 飞行器测控学报, 2005, 24(3): 43-50 |
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| 作者姓名： | 刘世元 刘春保 刘林 |
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| 作者单位： | 南京大学天文系·南京·210093;南京大学天文系·南京·210093;南京大学空间环境与航天动力学研究所·南京·210093 |
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| 摘 要： | 对于航天工程而言，无论是航天器的发射，卫星轨道设计，地面测控系统的跟踪、定轨和预报．还是卫星在轨运行过程中的轨道控制策略等，均需了解卫星轨道变化的规律。为此，本文对人造卫星(包括中心天体为快自转天体和慢自转天体两种引力源的绕飞轨道器)的轨道变化特征以及轨道寿命进行系统的综合分析。为各种应用提供简明信息。
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| 关 键 词： | 快自转天体 慢自转天体 人造卫星 摄动源 轨道变化特征 |
Integrated Analysis of Spacecraft Orbit Variation |
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| LIU Shi-yuan LIU Chun-bao LIU Lin. Integrated Analysis of Spacecraft Orbit Variation[J]. Journal of Spacecraft TT&C Technology, 2005, 24(3): 43-50 |
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| Authors: | LIU Shi-yuan LIU Chun-bao LIU Lin |
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| Affiliation: | LIU Shi-yuan~1 LIU Chun-bao~1 LIU Lin~ |
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| Abstract: | For astronautics engineering, spacecraft orbit variation should be understood not only for spacecraft launches, orbit design, tracking, orbit determination and forecast using ground-based TT&C systems, but also for determination of orbit control strategies for in-orbit operation spacecraft. This paper presents an analysis of the variation characteristics of orbits for probes orbiting two different celestial bodies: quick-rotational and slow-rotational ones, and their orbit lifetime problem. It aims to provide compendious information for various applications. |
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| Keywords: | Quick-rotational Celestial Body Slow-rotational Celestial Body Artificial Satellite Perturbation Source Orbit Variation Characteristics |
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