| 摄动对编队飞行星座相对构型的影响分析 |
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| 引用本文： | 侯育卓,赵军.摄动对编队飞行星座相对构型的影响分析[J].飞行器测控学报,2003,22(3):30-35. |
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| 作者姓名： | 侯育卓 赵军 |
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| 作者单位： | 北京跟踪与通信技术研究所 北京·100094
(侯育卓)，北京跟踪与通信技术研究所 北京·100094(赵军) |
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| 摘 要： | 在近圆轨道编队飞行的假设条件下，根据动力学关系推导出了环绕卫星相对参考卫星的运动学简化模型，并以此简化模型为基础，分别研究了大气阻力摄动、日月引力摄动、太阳光压摄动和地球扁率摄动对编队飞行星座的构型影响，着重分析了地球扁率摄动周期项和长期项对构型的影响，并以此对编队轨道设计提出建议。
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| 关 键 词： | 编队飞行 星座 影响分析 近圆轨道 轨道设计 摄动周期 |
Analysis of the Impact of Perturbation on Relative Configuration of Formation Flight Satellite Constellations |
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| HOU Yu,zhuo,ZHAO Jun.Analysis of the Impact of Perturbation on Relative Configuration of Formation Flight Satellite Constellations[J].Journal of Spacecraft TT&C Technology,2003,22(3):30-35. |
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| Authors: | HOU Yu zhuo ZHAO Jun |
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| Abstract: | Based on kinematic relationship,simplified motion equations of surrounding satellites with respect to reference satellite is deduced under near circular orbit formation flying assumption.Then based on this simplified motion equations,atmospheric drag effects perturbation,solar and lunar pressure perturbation and non center earth gravitational potential perturbation are discussed and the non center earth gravitational potential perturbation is mainly discussed.Finally,suggestions are presented to the orbit design of formation flying. |
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| Keywords: | Formation Flying Perturbation Orbit Design |
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