基于激光烧蚀冲量耦合的空间碎片主动变轨建模与仿真
收稿日期: 2013-04-11
修回日期: 2013-06-18
网络出版日期: 2013-06-24
基金资助
部级项目
Modeling and Simulation on Active Space Debris Orbit Maneuver Based on Laser Ablation Impulse Coupling
Received date: 2013-04-11
Revised date: 2013-06-18
Online published: 2013-06-24
Supported by
Province Level Project
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 . DOI: 10.7527/S1000-6893.2013.0311
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
[1] Payne T. First "confirmed" natural collision between two cataloged satellites. Second European Conference on Space Debris. Germany: ESA, 1997: 579-600.
[2] Kaplan M H. Survey of space debris reduction methods. AIAA-2009-6619, 2009.
[3] Klinkrad H. Space debris-model and risk analysis. Chichester, UK: Praxis Publishing Ltd, 2006.
[4] Campbell J W. Project orion: orbital debris removal using ground-based sensors and lasers. NASA Technical Memorandum, 1996, 108522: 1-352.
[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.
[6] Rubenchik A, Barty C, Beach R, et al. Laser systems for space orbital debris removal. LLNL-PROC-423323, 2010.
[7] Early J, Bibeau C, Phipps C, et al. Space debris de-orbiting by vaporization impulse using short pulse laser. Proceedings of SPIE, 2004, 5448: 441-449.
[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.
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