Autonomous satellite observation and removal planning simulation for small and medium-sized debris

被引：0
|
作者：
Liao H. [1 ]
Xu Z. [1 ]
Wang X. [2 ]
Wang D. [1 ]
机构：
[1] Institute of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing
[2] DFH Satellite Company Limited, Beijing
来源：
Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics | 2023年 / 45卷 / 02期
关键词：
combining design; optical observation; removal planning; small and medium-sized debris;
D O I：
10.12305/j.issn.1001-506X.2023.02.20
中图分类号：
学科分类号：
摘要：
Aiming at the problem that the ground-based detection system cannot clearly observe the small and medium-sized debris, an autonomous satellite optical observation and removal planning simulation method is proposed. The simulation platform is adopted based on the combining design of the C++, QT and STK(satellite tool kit). Its main functions include self-generation of massive debris, optical observation, debris and satellite rendezvous and autonomous debris removal planning. It can effectively achieve the screening of massive debris data and the time sequence planning of satellite attitude and on-off time of removal payload during satellite autonomous observation and removal tasks. Finally, by downloading data from the space-track website and artificially generating debris around the satellite orbit as the input conditions, the feasibility of the simulation platform is effectively verified. © 2023 Chinese Institute of Electronics. All rights reserved.
引用
收藏
页码：490 / 496
页数：6
相关论文
共 32 条
  • [1] SHANM H, GUOJ, GILLE, Review and comparison of active space debris capturing and removal methods, Progress in Aerospace Sciences, 80, pp. 18-32, (2016)
  • [2] LIM, GONGZ Z, LIUG Q., Advanced technology and system development of space debris monitoring and removal[J], Science Bulletin, 63, 25, pp. 2570-2591, (2018)
  • [3] DUR H, ZHANGX, LIAOW H., Fast initial relative orbit determination method of angles-only relative navigation[J], Systems Engineering and Electronics, 43, 4, pp. 1057-1068, (2021)
  • [4] HUD Q, PANGB J, CHIR Q, Et al., Survivability assessment of spacecraft impacted by orbit debris[J], Defence Technology, 17, 3, pp. 961-970, (2021)
  • [5] RAOH P, ZHONGR, LIP J., Fuel-optimal deorbit scheme of space debris using tethered space-tug based on pseudospectral method[J], Chinese Journal of Aeronautics, 34, 9, pp. 210-223, (2021)
  • [6] ZHAOP Y, LIUJ G, WUC C., Survey on research and deve-lopment of on-orbit active debris removal methods[J], Science China(Technological Sciences), 63, 11, pp. 2188-2210, (2020)
  • [7] HAMEDA, ZHANGJ R., Cutting-edge space exploration technology maturity level facilitation with support of space debris removal missions[J], Journal of Beijing Institute of Technology, 27, 4, pp. 477-484, (2018)
  • [8] CHENC, YANGW L, GONGZ Z, Et al., Research progress in laser active debris removal of CAST[J], Aerospace China, 19, 4, pp. 3-19, (2018)
  • [9] MURRAYJ, JENETF, The arecibo observatory as an instrument for investigating orbital debris: legacy and next generation performance, The Planetary Science Journal, 3, 3, (2022)
  • [10] GSAA, BTA, SFA, Et al., The active space debris removal mission remove debris. Part 2: in orbit operations, Acta Astronautica, 168, pp. 310-322, (2020)
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