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

系统工程与电子技术 ›› 2023, Vol. 45 ›› Issue (2): 490-496.doi: 10.12305/j.issn.1001-506X.2023.02.20

• 系统工程 • 上一篇

面向中小型碎片的卫星自主观驱规划仿真研究

廖鹤¹^,*, 许志豪¹, 王晓丹², 王代薪¹

1. 南京航空航天大学航天学院, 江苏南京 211106
2. 航天东方红卫星有限公司, 北京 100854

收稿日期:2022-01-24 出版日期:2023-01-13 发布日期:2023-02-04
通讯作者: 廖鹤
作者简介:廖鹤(1984—), 男, 副研究员, 博士, 主要研究方向为卫星总体设计、卫星动力学与控制
许志豪(1999—), 男, 硕士研究生, 主要研究方向为卫星轨道设计及其系统仿真
王晓丹(1984—), 女, 高级工程师, 硕士, 主要研究方向为卫星轨道设计及其系统仿真
王代薪(1999—), 男, 硕士研究生, 主要研究方向为卫星姿态动力学与控制
基金资助:
国家自然科学基金(12172168)

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

He LIAO¹^,*, Zhihao XU¹, Xiaodan WANG², Daixin WANG¹

1. Institute of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China
2. DFH Satellite Company Limited, Beijing 100854, China

Received:2022-01-24 Online:2023-01-13 Published:2023-02-04
Contact: He LIAO

摘要/Abstract

摘要：

针对目前地基探测系统无法对中小型碎片清晰成像的问题, 提出了一种面向中小型碎片的卫星自主光学观测与驱离规划仿真方法。该仿真方法采用C++、QT、STK(satellite tool kit)进行联合设计, 主要包含批量碎片生成模块、光学观测模块、碎片与卫星交会模块和自主驱离规划模块, 可有效实现海量碎片数据的筛选, 以及自主观测与驱离任务下的卫星姿态与驱离载荷的开关机时间的时序规划。最后, 通过space-track网站和在卫星轨道周围批量生成碎片作为输入条件, 有效验证了该仿真方法的可行性。

关键词: 中小型碎片, 光学观测, 驱离规划, 联合设计

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

中图分类号:

V446+.5

廖鹤, 许志豪, 王晓丹, 王代薪. 面向中小型碎片的卫星自主观驱规划仿真研究[J]. 系统工程与电子技术, 2023, 45(2): 490-496.

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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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

面向中小型碎片的卫星自主观驱规划仿真研究

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

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