基于激光烧蚀冲量耦合的空间碎片主动变轨建模与仿真

doi:10.7527/S1000-6893.2013.0311

流体力学与飞行力学

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基于激光烧蚀冲量耦合的空间碎片主动变轨建模与仿真

常浩¹, 金星², 洪延姬²

1. 装备学院研究生院, 北京 101416;
2. 装备学院激光推进及其应用国家重点实验室, 北京 101416

收稿日期:2013-04-11 修回日期:2013-06-18 出版日期:2013-10-25 发布日期:2013-06-24
通讯作者: 金星,Tel.: 010-66364435 E-mail: jinxing_beijing@sina.com E-mail:jinxing_beijing@sina.com
作者简介:常浩男, 博士研究生。主要研究方向: 激光烧蚀推进技术。 Tel: 010-66364435 E-mail: changhao5976911@sina.com;金星男, 博士, 研究员, 博士生导师。主要研究方向: 激光推进应用技术及可靠性工程。 Tel: 010-66364435 E-mail: jinxing_beijing@sina.com;洪延姬女, 博士, 研究员, 博士生导师。主要研究方向: 激光推进技术。 Tel: 010-66364435 E-mail: hongyanji@vip.sina.com
基金资助:
部级项目

Modeling and Simulation on Active Space Debris Orbit Maneuver Based on Laser Ablation Impulse Coupling

CHANG Hao¹, JIN Xing², HONG Yanji²

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

Received:2013-04-11 Revised:2013-06-18 Online:2013-10-25 Published:2013-06-24
Supported by:
Province Level Project

摘要/Abstract

摘要：

空间碎片对人类航天活动的危害很大,用高能激光减缓其危害性被认为是最有效的手段。分析了空间碎片在激光作用下的变轨过程,建立了相应的物理模型,并给出了空间碎片受地基激光辐照后轨道变化的数值模拟过程。对空间碎片主动离轨防止碰撞在轨卫星实例进行了仿真计算,并对仿真时间内空间碎片的轨道根数、空间碎片与卫星之间的相对距离变化进行了数值模拟。仿真结果表明,地基激光能有效改变空间碎片的飞行轨迹,是避免空间碎片与空间目标碰撞的一种新的解决途径。

关键词: 空间碎片, 激光烧蚀, 冲量耦合, 变轨, 数值模拟

Abstract:

Orbital debris poses a great thread to human space activities and high power laser is considered to be the most feasible method to migrate its hazard. A physical model is built in this paper based on an analysis of the process of laser radiation against space debris. The orbital elements of space debris under laser radiation are studied numerically and the findings are applied to space debris collision avoidance with a satellite. A simulation example is set up to study the space debris avoiding process. In addition, numerical results of the orbital elements of space debris and their relative distance from the satellite are obtained in the circumstance of laser interaction. The simulation results show that a ground-based laser may effectively control the orbit of space debris realize the avoidance of satellite collision.

Key words: space debris, laser ablation, impulse coupling, orbit maneuver, numerical simulation

中图分类号:

V416.5
TN249

常浩, 金星, 洪延姬. 基于激光烧蚀冲量耦合的空间碎片主动变轨建模与仿真[J]. 航空学报, 2013, 34(10): 2325-2332.

CHANG Hao, JIN Xing, HONG Yanji. Modeling and Simulation on Active Space Debris Orbit Maneuver Based on Laser Ablation Impulse Coupling[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(10): 2325-2332.

参考文献

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[5] Phipps C, Albrecht G, Friedman H, et al. Orion: clearing near-earth space debris using a 20-kW, 530-nm, earth-based, repetitively pulse laser. Laser and Particle Beams, 1996(1): 1-44.

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[8] Esmiller B, Jacquelardb C. CLEANSPACE "small debris removal by laser illumination and complementary technologies"//Beamed energy propulsion. AIP Conference Proceedings, 2011, 1402: 347-353.

[9] Chang H, Jin X, Hong Y J, et al. Modeling and simulation on ground-based laser cleaning space debris process. Acta Aeronautica et Astronautica Sinica, 2012, 33(6): 994-1001. (in Chinese) 常浩, 金星, 洪延姬, 等. 地基激光清除空间碎片过程建模与仿真. 航空学报, 2012, 33(6): 994-1001.

[10] Jin X, Hong Y J, Li X Q. Removal processes analysis of centimeter-scale space debris using laser radiation. High Power Laser and Particle Beams, 2012, 24(2): 281-284. (in Chinese) 金星, 洪延姬, 李修乾. cm级空间碎片的激光清除过程分析. 强激光与粒子束, 2012, 24(2): 281-284.

[11] Wu Z N, Hu R F, Qu X, et al. Space debris reentry analysis methods and tools. Chinese Journal of Aeronautics, 2011, 24(4): 387-395.

[12] Badhwar G D, Anz-Meador P D. Relationship of radar cross section to the geometric size of orbital debris. AIAA, NASA, and DOD, Orbital Debris Conference: Technical Issues and Future Directions, 1990.

[13] Lambour R, Rajan N, Morgan T. Assessment of orbital debris size estimation from radar cross-section measurement. Advances in Space Research, 2004, 34(5): 1013-1020.

[14] Schall W O. Laser radiation for cleaning space debris from lower earth orbits. Journal of Spacecraft and Rockets, 2002, 39(1): 81-91.

E-mail：hkxb@buaa.edu.cn

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基于激光烧蚀冲量耦合的空间碎片主动变轨建模与仿真

Modeling and Simulation on Active Space Debris Orbit Maneuver Based on Laser Ablation Impulse Coupling

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