面向中小型碎片的卫星自主观驱规划仿真研究

doi:10.12305/j.issn.1001-506X.2023.02.20

Abstract

Abstract:

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.

Key words: small and medium-sized debris, optical observation, removal planning, combining design

CLC Number:

V446+.5

He LIAO, Zhihao XU, Xiaodan WANG, Daixin WANG. Autonomous satellite observation and removal planning simulation for small and medium-sized debris[J]. Systems Engineering and Electronics, 2023, 45(2): 490-496.

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References 32

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参数	取值	参数	取值
轨道半长轴A/km	6 757.8	升交点赤经Ω/(°)	2.0
轨道倾角I/(°)	53.0	近地点幅角ω/(°)	0
偏心率e	0	平近点角M/(°)	39.5

参数	星载观测载荷
参数	光学相机	光照锥
观测视场范围/km	0~100	0~100
形状	矩形(30°×10°)	圆锥(半锥角50°)

碎片编号	起始时	终止时间	总持续时
40号	0.000	2 329.565	2 329.565
41号	5 197.450	7 924.798	2 727.347
39号	11 020.531	14 052.738	3 032.207

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

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