日地平动点卫星两脉冲转移轨道设计
文献类型：期刊论文
| 作者 | 李明涛 ; 郑建华 ; 于锡峥 ; 高东 |
| 刊名 | 北京航空航天大学学报
 |
| 出版日期 | 2009 |
| 卷号 | 35期号:7页码:865-868 |
| 关键词 | Halo轨道 转移轨道 微分修正 不变流形 |
| ISSN号 | 1001-5965 |
| 其他题名 | Two impulses transfer tra jectory design for Sun-Earth libration point missions |
| 通讯作者 | 北京8701信箱 |
| 中文摘要 | 研究基于最小二乘微分修正方法的平动点卫星两脉冲转移轨道设计,推导了考虑高度和航迹角约束的微分修正公式,讨论了该方法的收敛性.以日地L1点附近的Halo轨道为目标轨道,在圆型限制性三体问题模型下设计了其转移轨道,系统地研究了HOI(HaloOrbit Insertion)点和Halo轨道幅值对转移轨道的影响,给出了HOI点的选择策略,并讨论了应急情况下快速转移轨道设计.数值仿真验证了方法的有效性,选择Halo轨道靠近地球侧的点作HOI点可以获得飞行时间适中的转移轨道. |
| 英文摘要 | Two impulses transfer trajectory design based on the least differential corrections method was studied, differential correction equation with the altitude and the flight path angle constraints was concluded,and the convergence of the method was discussed. Halo orbit around the L1 libration point of the Sun-Earth system was taken as the objective orbit, two impulses transfer trajectory was designed in the framework of the circular restricted three2body p roblem. Effect of Halo orbit insertion (HO I) point and amp litude was studied in a systematic way, a strategy for the selection of HO I point was given, and the fast transfer trajectory for emergency was also studied. Numerical simulation shows that the p roposed method is very effective, and transfer trajectory with moderate flight time can be obtained by choosing points on the near Earth side of Halo orbit as HOI point. |
| 学科主题 | 空间技术 |
| 收录类别 | CSCD |
| 语种 | 中文 |
| CSCD记录号 | CSCD:3708828 |
| 源URL | [http://ir.cssar.ac.cn/handle/122/704]  |
| 专题 | 国家空间科学中心_空间技术部 |
| 推荐引用方式 GB/T 7714 | 李明涛,郑建华,于锡峥,等. 日地平动点卫星两脉冲转移轨道设计[J]. 北京航空航天大学学报,2009,35(7):865-868. |
| APA | 李明涛,郑建华,于锡峥,&高东.(2009).日地平动点卫星两脉冲转移轨道设计.北京航空航天大学学报,35(7),865-868. |
| MLA | 李明涛,et al."日地平动点卫星两脉冲转移轨道设计".北京航空航天大学学报 35.7(2009):865-868. |
入库方式： OAI收割
来源：国家空间科学中心
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