| 大气阻力摄动对卫星编队飞行队形的影响分析 |
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| 引用本文： | 吴宝林,曹喜滨.大气阻力摄动对卫星编队飞行队形的影响分析[J].航天控制,2006,24(1):19-23. |
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| 作者姓名： | 吴宝林 曹喜滨 |
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| 作者单位： | 哈尔滨工业大学卫星技术研究所,哈尔滨,150001 |
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| 摘 要： | 为了分析大气阻力摄动对卫星编队队形的影响,利用相对轨道根数法推导了包含大气阻力摄动的卫星编队相对运动的状态转移方程。仿真结果表明当几何形状和质量不同的两颗卫星在低轨道做编队飞行时,大气阻力摄动对编队队形的影响很大而不能忽略;当主卫星的半长轴相等时,主卫星轨道的偏心率越大编队飞行受大气阻力摄动的影响也越大;大气阻力摄动主要影响编队飞行迹向相对距离。
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| 关 键 词： | 大气阻力摄动 卫星编队飞行 相对轨道根数 状态转移方程 |
| 文章编号： | 1006-3242(2006)01-0019-05 |
| 修稿时间： | 2004年12月8日 |
The Analysis of the Effects on Satellite Formation Caused by Drag Perturbation |
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| Wu Baolin,Cao Xibing.The Analysis of the Effects on Satellite Formation Caused by Drag Perturbation[J].Aerospace Control,2006,24(1):19-23. |
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| Authors: | Wu Baolin Cao Xibing |
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| Abstract: | In order to analyze the effects of drag perturbation on the satellite formation flying,using relative orbit elements method a state transition function for the relative motion that includes the effects caused by drag perturbation is proposed.Simulation results show that three conclusions can be obtained.Firstly,the effects caused by drag perturbation are very large when satellites within the formation are of different geometry and mass.Secondly,when the satellites have the same semi-axis,the effect caused by drag perturbation grows larger as the eccentricity grows larger.Thirdly,the drag perturbation mainly affects the tangential distance of the formation. |
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| Keywords: | Drag perturbation Satellite formation Relative orbit elements State transition function |
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