A Population Dynamics Approach to the Distribution of Space Debris in Low Earth Orbit

被引:0
作者
John Jurkiewicz
Peter Hinow
机构
[1] University of Wisconsin-Milwaukee,Department of Mathematical Sciences
来源
Communications on Applied Mathematics and Computation | 2024年 / 6卷
关键词
Population dynamics; Space debris; Kessler syndrome; Diffusion; Low-Earth orbit; 92D25;
D O I
暂无
中图分类号
学科分类号
摘要
The presence of the debris in the Earth’s orbit poses a significant risk to human activity in outer space. This debris population continues to grow due to ground launches, the loss of external parts from space ships, and uncontrollable collisions between objects. A computationally feasible continuum model for the growth of the debris population and its spatial distribution is therefore critical. Here we propose a diffusion-collision model for the evolution of the debris density in the low-Earth orbit and its dependence on the ground-launch policy. We parametrize this model and test it against data from publicly available object catalogs to examine timescales for the uncontrolled growth. Finally, we consider sensible launch policies and cleanup strategies and how they reduce the future risk of collisions with active satellites or space ships.
引用
收藏
页码:340 / 353
页数:13
相关论文
共 35 条
[1]  
Bonnal C(2020)Just in time collision avoidance—a review Acta Astronaut. 170 637-651
[2]  
McKnight D(1959)Solution of the problem of artificial satellite theory without drag Astron. J. 64 378-396
[3]  
Phipps C(1981)Reformulation of the Brouwer geopotential theory for improved computational efficiency Celest. Mech. 24 367-375
[4]  
Dupont C(1978)Collision frequency of artificial satellites: the creation of a debris belt J. Geophys. Res. 83 2637-2646
[5]  
Missonnier S(2018)Space debris removal: learning to cooperate and the price of anarchy Front. Robot. AI 5 54-1876
[6]  
Lequette L(2011)An active debris removal parametric study for LEO environment remediation Adv. Space Res. 47 1865-986
[7]  
Merle M(2004)LEGEND—a three-dimensional LEO-to-GEO debris evolutionary model Adv. Space Res. 34 981-558
[8]  
Rommelaere S(1963)Small eccentricities or inclinations in the Brouwer theory of the artificial satellite Astron. J. 68 555-305
[9]  
Brouwer D(1993)An analytical model for the catastrophic production of orbital debris ESA J. 17 293-135
[10]  
Hoots FR(1995)A comparison of debris environment projections using the EVOLVE and CHAIN models Adv. Space Res. 16 127-undefined