With the accelerated deployment of mega constellations,the risk of collisions between satellites has sharply increased.In order to study the situation and evolution characteristics of two debris clouds generated by the collisions of two satellites,this paper simulates and calculates the situation and evolution of the two debris clouds generated by the collisions of two satellites,including the overall situation and debris situation after the generation of the debris clouds,and discusses the dispersion of the debris clouds in positional space,including the distribution characteristics of relevant parameters.Research has shown that both the inclination vector and the velocity clustering of fragments in the geocentric inertial frame can effectively identify the source of disintegrated fragments.The research results can provide reference suggestions for space traffic management and space safety protection.
JIANG Yu
. The Situation and Evolution of Two Debris Clouds Generated by the Collision of Two Satellites[J]. Journal of Space Science and Experiment, 2023
, 23(4)
: 36
-45
.
DOI: 10.19963/j.cnki.2096-4099.2023.04.004
[1] Space Environment Statistics.https://sdup.esoc.esa.int/discosweb/statistics/
[2] 姜宇,姜春生,李恒年.流星体与空间碎片模型综述[J].动力学与控制学报.2022,20(4),32-39.
[3] ESA Space Debris Office.ESA's Annual Space Environment Report.12 June 2023
[4] NASA Orbital Debris Program Office(ODPO).ISS Maneuvers Twice in a Weeks Span to Avoid Potential Collisions[J].Orbital Debris Quarterly News.2023.27(2),1.
[5] AMBROSIO A D,SERVADIO S,SIEW P M,et al.Novel source-sink model for space environment evolution with orbit capacity assessment.2023.60(4),473.
[6] LIU YONGJIE,JIANG Y,LI H N et al.Determining origins of satellite breakup events in LEO region[J].Astrodynamics,2023,7(4),465-476.
[7] KRAG H,SERRANO M,BRAUN V,et al.A 1 cm space debris impact onto the sentinel-1a solar array[J].Acta Astronaut.2017,137:434-443.
[8] SCHAUS V,ALESSI E M,SCHETTINO G,et al.On the practical exploitation of perturbative effects in low Earth orbit for space debris mitigation[J].Adv.Space Res.2019,63:1979-1991.
[9] 李正宇,贾光辉,张品亮,等.超高速斜撞击下航天器Whipple结构碎片特性研究[J].空间碎片研究,2023,23(2):21-33.
[10] Journal of Brief Ideas.Space Debris Fingerprint Definition and Identification.
[11] 吴健发,魏春岭,张海博.航天器反应式碎片规避动作规划方法[J].宇航学报,2023,44(2):221-232.
[12] JIANG Y,LI H N,YANG Y.Evolution of space debris for spacecraft in the Sun-synchronous orbit[J].Open Astronomy.2020,29:265-274.
[13] HENRY S,ARMELLIN R,GATEAU T.Safe-event pruning in spacecraft conjunction management[J].Astrodynamics,2023,7(4):401-413.
[14] TAN A,REYNOLDS.Velocity perturbations analysis of the fragmentation of USA-193 Satellite in orbit[J].Advances in Aerospace Science and Applications.2021,11(1),1-10.
[15] ANZ-MEADOR P,LIOU J C.Analysis and consequences of the Iridium 33-Cosmos 2251 Collision[C].38th Scientific Assembly of the Committee on Space Research(COSPAR).2010.Bremen,Germany
[16] TAN A,ZHANG T X,DOKHANIAN M.Analysis of the Iridium 33 and Cosmos 2251 Collision using Velocity Perturbations of the Fragments[J].Advances in Aerospace Science and Applications,2013,3(1),13-25.
[17] KELSO T S.Analysis of the Iridium 33-Cosmos 2251 Collision[C].10th Advanced Maui Optical and Space Surveillance Technologies Conference,Maui,HI,2009.
[18] JOHNSON N L,KRISKO P H,LIOU J C,et al.NASA's new breakup model of EVOLVE 4.0[J].
Advances in Space Research,2001,28(9):1377-1384.
[19] JIANG Y.Debris cloud of India Anti-Satellite Test to Microsat-R Satellite.2020.DOI:10.1016/j.heliyon.2020.e04692.
[20] PRICE M C ,COLE M J ,BURCHELL M J ,et al.Impacts into metals targets at velocities greater than 1 km/s~(-1):A new online resource for the hypervelocity impact community and an illustration of the geometric change of debris cloud impact patterns with impact velocity[J].International journal of impact engineering,2013,56:47-60.
[21] PIEKUTOWSKI A J,POORMON K L.Meeting the challenges of hypervelocity impact testing at 10 km/s[J].International Journal of Impact Engineering,2023,180,104665.
[22] MARTIN C ,WALKER R ,KLINKRAD H.The sensitivity of the ESA DELTA model[J].Advances in Space Research,2004,34(5):969-974.
[23] SMIRNOV N N,KISELEV A B,NAZARENKO A I,et al.Physical and mathematical models for space objects breakup and fragmentation in hypervelocity collisions[J].Acta Astronautica,2020,176:598-608.
[24] 章仁为.卫星轨道姿态动力学与控制[M].北京航空航天大学出版社.1998
[25] THÉBAULT E,FINLAY C C,BEGGAN C D,et al.International geomagnetic reference field:the 12th generation[J].Earth,Planets and Space,2015,67(1):79.
[26] GRÜN E,GUSTAFSON B,MANN I,et al.Interstellar dust in the heliosphere[J].Astron.Astrophys,1994,286:915-924.
[27] BURNS J A,LAMY P L,SOTER S.Radiation forces on small particles in the solar system[J].Icarus,1979,40(1):1-48.
[28] ANSELMO L,PARDINI C,.Analysis of the consequences in low Earth orbit of the collision between Cosmos 2251 and Iridium 33[C].In:Proceedings of the 21st International Symposium on Space Flight Dynamics.2009.September.Centre nationale d'etudes spatiales,Paris,France,1-15.
