| 近圆参考轨道卫星编队的安全性 |
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| 引用本文： | 胡敏,曾国强,姚红,李晓明.近圆参考轨道卫星编队的安全性[J].中国空间科学技术,2010,30(4). |
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| 作者姓名： | 胡敏 曾国强 姚红 李晓明 |
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| 作者单位： | 装备指挥技术学院,北京,101416 |
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| 摘 要： | 针对近圆参考轨道卫星,利用相对轨道要素对编队构形进行了统一描述,提出了编队卫星在垂直于轨道平面方向相对运动最小距离的计算公式,分析了J2摄动对卫星编队安全性的影响。仿真结果表明环绕星在轨道平面内和垂直于轨道平面内的相位差对编队安全性的影响较大,给出的提高编队卫星安全性的措施可为卫星编队的实际工程应用提供参考。
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| 关 键 词： | 相对轨道要素 近圆参考轨道 编队构形 安全性 编队飞行 航天器 |
Safety for Near Round Reference Orbit Satellites Formation |
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| Hu Min,Zeng Guoqiang,Yao Hong,Li Xiaoming.Safety for Near Round Reference Orbit Satellites Formation[J].Chinese Space Science and Technology,2010,30(4). |
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| Authors: | Hu Min Zeng Guoqiang Yao Hong Li Xiaoming |
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| Institution: | Hu Min Zeng Guoqiang Yao Hong Li Xiaoming (Academy of Equipment Command & Technology,Beijing 101416) |
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| Abstract: | The safety of close formation flying satellites was investigated. Aiming at the near round reference orbit satellites,the formation configuration was described based on the relative orbit elements,formulas of the minimize distance of formation flying satellites in the cross-track direction were proposed,and the influence of J2 perturbation to the safety of satellites formation was analyzed. The simulation results demonstrate that the phase difference in the orbital plane and the plane perpendicular to the o... |
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| Keywords: | Relative orbit elements Near round reference orbit Formation configuration Safety Formation flight Spacecraft |
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