| 载人飞船自动化轨道设计方法研究 |
| |
| 引用本文： | 刘鲁华,郑伟,汤国建.载人飞船自动化轨道设计方法研究[J].上海航天,2011,28(3):23-25,31. |
| |
| 作者姓名： | 刘鲁华 郑伟 汤国建 |
| |
| 作者单位： | 国防科学技术大学,航天与材料工程学院,湖南,长沙,410073 |
| |
| 摘 要： | 为提高戢人飞船轨道设计的自动化程度和快速性,对自动化轨道设计方法进行了研究.分析了裁人飞船不同阶段飞行轨道的约束条件,用约束条件首先确定了轨道的半长轴取值范围,由回归条件可确定回归圈数的取值范围;在给定的回归和返回条件下,迭代求解运行轨道的轨道半长轴与倾角;根据运行轨道设计结果,反推初始轨道和留轨轨道的轨道根数.自动化...
|
| 关 键 词： | 载人飞船 轨道设计 轨道根数 自动化设计 |
Automatic Orbit Design Approach Research of Manned Spacecraft |
| |
| LIU Lu-hua,ZHENG Wei,TANG Guo-jian.Automatic Orbit Design Approach Research of Manned Spacecraft[J].Aerospace Shanghai,2011,28(3):23-25,31. |
| |
| Authors: | LIU Lu-hua ZHENG Wei TANG Guo-jian |
| |
| Institution: | LIU Lu-hua,ZHENG Wei,TANG Guo-jian(College of Astronautical & Material Engineering,NUDT,Changsha 410073,Hunan,China) |
| |
| Abstract: | The automatic orbit design problem was researched in order to improve the automatic and rapid capability of spacecraft orbit design in this paper.The constraints in different phase of spacecraft were analyzed.The span of orbit semi-axis was determined using the contstrains,and the span of regressing circle was deduced by combining regressing condition.Under the regressing and returning conditions,the orbit semi-axis and inclination were solved using iterative method;and the other orbit roots could be deduce... |
| |
| Keywords: | Manned spacecraft Orbit design Orbit roots Automatic design |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
