地基激光清除椭圆轨道空间碎片特性的计算分析

doi:10.7527/S1000-6893.2013.0310

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2013, Vol. 34 ›› Issue (9): 2064-2073.doi: 10.7527/S1000-6893.2013.0310

• Fluid Mechanics and Flight Mechanics • Previous Articles Next Articles

Simulation Analysis of Removal of Elliptic Orbit Space Debris Using Ground-based Laser

JIN Xing¹, HONG Yanji¹, CHANG Hao²

1. State Key Laboratory of Laser Propulsion & Application, Academy of Equipment, Beijing 101416, China;
2. Postgraduate School, Academy of Equipment, Beijing 101416, China

Received:2013-04-10 Revised:2013-06-18 Online:2013-09-25 Published:2013-06-25
Supported by:
Space Debris Special Research Project of China (K0103110)

Abstract

Abstract:

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.

Key words: space debris, laser removal, single laser pulse, multi laser pulses, orbitial variation

CLC Number:

V416.5
TN249

JIN Xing, HONG Yanji, CHANG Hao. Simulation Analysis of Removal of Elliptic Orbit Space Debris Using Ground-based Laser[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(9): 2064-2073.

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Simulation Analysis of Removal of Elliptic Orbit Space Debris Using Ground-based Laser

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