| 交会对接绕飞段临界安全轨迹研究 |
| |
| 引用本文： | 梁静静,解永春. 交会对接绕飞段临界安全轨迹研究[J]. 空间控制技术与应用, 2014, 0(1): 37-40,57 |
| |
| 作者姓名： | 梁静静 解永春 |
| |
| 作者单位： | [1]北京控制工程研究所,北京100190 [2]空间智能控制技术重点实验室,北京100190 |
| |
| 基金项目： | 重点基础研究发展计划（973）资助项目（2013CB733100）. |
| |
| 摘 要： | 以Hill方程为基础对圆轨道近距离双脉冲绕飞安全策略进行研究.首先给出双脉冲绕飞的模型,通过仿真遍历得到不会进入球形安全区的绕飞轨迹,然后绘制出这些安全的绕飞轨迹所对应的绕飞时间、燃料消耗、追踪器与目标器的初始距离三个量之间的关系曲面,进而得到临界安全条件下的关系曲线并拟合出关系表达式,最后对拟合误差进行分析发现导致轨迹偏离的程度很小.
|
| 关 键 词： | 绕飞 安全 燃料消耗 拟合 |
Trajectory of Critical Safety of Fly-Around in Rendezvous and Docking |
| |
| LIANG Jingjing,XIE Yongchun,SUN Shuai. Trajectory of Critical Safety of Fly-Around in Rendezvous and Docking[J]. Aerospace Contrd and Application, 2014, 0(1): 37-40,57 |
| |
| Authors: | LIANG Jingjing XIE Yongchun SUN Shuai |
| |
| Affiliation: | 1. Beijing Institute of Control Engineering, Beijing 100080, China ; 2. Science and Technology on Space Intelligent Control Laboratory, Beijing 100190, China) |
| |
| Abstract: | Based on the Hill equation, the safety strategy of double-impulsive fly-around process is researched. Firstly, the model of double-impulsive fly-around is given and all the fly-around trajectories outside the global safety area are obtained by ergodic simulation. Then a curved surface can be plotted, which expresses the relations among fly-around time, the consumption of the fuel and the starting point. Furthermore, the curve which is critically safe can be obtained and fitted. Finally, the fitting error is analyzed and it is showed that the trajectory deviates slightly. |
| |
| Keywords: | fly-around safety the consumption of the fuel fitting |
| 本文献已被 CNKI 维普 等数据库收录！ |
|
