地基激光清除椭圆轨道空间碎片特性的计算分析
收稿日期: 2013-04-10
修回日期: 2013-06-18
网络出版日期: 2013-06-25
基金资助
空间碎片专项科研项目(K0103110)
Simulation Analysis of Removal of Elliptic Orbit Space Debris Using Ground-based Laser
Received date: 2013-04-10
Revised date: 2013-06-18
Online published: 2013-06-25
Supported by
Space Debris Special Research Project of China (K0103110)
金星 , 洪延姬 , 常浩 . 地基激光清除椭圆轨道空间碎片特性的计算分析[J]. 航空学报, 2013 , 34(9) : 2064 -2073 . DOI: 10.7527/S1000-6893.2013.0310
Space debris poses great threat to human aviation activity. High power laser is considered a feasible method to clean it. Cleaning methods with single laser pulse and multi laser pulse orbitial variation are advanced in this paper based on an analysis of the removal of elliptical orbit space debris. The simulation results show that the initial true anomaly for effective de-orbiting effect is 100°-150° the widest range for ground-based laser distribution is at the vicinity of space debris true anomaly of 180° the two methods for de-orbiting space debris have very similar effects when the laser duration is extremely short or when the interaction distance is small, so that the single laser pulse orbitial variation method can be selected to represent approximately the multi-pluses method.
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