| 空间交会调相特殊点变轨求解算法 |
| |
| 引用本文： | 张进,李海阳,罗亚中,唐国金.空间交会调相特殊点变轨求解算法[J].航天控制,2009,27(4). |
| |
| 作者姓名： | 张进 李海阳 罗亚中 唐国金 |
| |
| 作者单位： | 国防科技大学航天与材料工程学院,长沙,410073 |
| |
| 摘 要： | 空间交会调相是交会轨道控制的关键问题,本文给出了摄动条件下交会调相特殊点变轨求解算法.算法由粗求解器和细求解器组成:粗求解器中仅迭代部分设计变量,其余设计变量由Gauss型摄动运动方程解析计算;细求解器以粗求解器计算结果为初值,迭代所有设计变量获得较精确满足终端条件的解.算法简单可靠,适用于工程实际,算法的有效性得到了STK高精度轨道预报模块的验证.
|
| 关 键 词： | 空间交会 调相 特殊点变轨 迭代算法 |
A Method for Solving Rendezvous Phasing Special-point Maneuvers |
| |
| ZHANG Jin,LI Haiyang,LUO Yazhong,TANG Guojin.A Method for Solving Rendezvous Phasing Special-point Maneuvers[J].Aerospace Control,2009,27(4). |
| |
| Authors: | ZHANG Jin LI Haiyang LUO Yazhong TANG Guojin |
| |
| Institution: | ZHANG Jin LI Haiyang LUO Yazhong TANG Guojin College of Aerospace , Material Engineering,National University of Defense Technology,Changsha 410073,China |
| |
| Abstract: | Rendezvous phasing plays a key role in rendezvous orbit control.A method considering orbit perturbations is proposed for solving rendezvous phasing special-point maneuvers problem.The method is composed by a rough solver and an accurate solver.In the rough solver,only parts of design variables are iterated and the rest are analytically defined by Gaussian form perturbed equations of motion.In the accurate solver,the result gained by rough solver is used as initial reference solution and the solution which s... |
| |
| Keywords: | Space rendezvous Phasing Special-point maneuvers Iteration method |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
|
