| 引用本文: | 罗成,高大远,沈辉,等.椭圆轨道上空间飞行器的编队飞行轨道设计.[J].国防科技大学学报,2006,28(4):22-26.[点击复制] |
| LUO Cheng,GAO Dayuan,SHEN hui,et al.Orbit Design for Spacecraft Formation Flying in Eccentric Orbits[J].Journal of National University of Defense Technology,2006,28(4):22-26[点击复制] |
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| 椭圆轨道上空间飞行器的编队飞行轨道设计 |
| 罗成, 高大远, 沈辉, 胡德文 |
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(国防科技大学 机电工程与自动化学院，湖南 长沙 410073)
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| 摘要: |
| 针对椭圆轨道上空间飞行器的编队飞行，基于开普勒轨道方程推导了一组新的相对运动方程，该方程组采用轨道要素表示，可直接用于编队的轨道设计。分析了一些典型的相对运动轨迹及编队轨道的精度，在此基础上，设计了线性编队和垂直圆编队。仿真结果验证了这种方法是有效的。 |
| 关键词: 编队飞行 椭圆轨道 轨道设计 |
| DOI： |
| 投稿日期：2006-03-02 |
| 基金项目:国家杰出青年科学基金资助项目(60225015)；高等学校优秀青年教师教学科研奖励计划资助项目 |
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| Orbit Design for Spacecraft Formation Flying in Eccentric Orbits |
| LUO Cheng, GAO Dayuan, SHEN hui, HU Dewen |
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(College of Mechatronics Engineering and Automation, National Univ. of Defense Technology, Changsha 410073, China)
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| Abstract: |
| Based on the Kepler's equation, a new set of relative motion equations with elliptical reference orbits were derived. The equations are expressed by orbit elements, and can be used directly for formation flying orbit design. Several typical relative motions and the precision of the equations were analyzed. Furthermore, a linear formation and a perpendicular circles formation were suggested. The effectiveness was verified by the simulation results. |
| Keywords: formation flying eccentric orbits orbit design |
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