基于星载光电成像跟踪测距的空间目标定轨

王卫兵; 王挺峰; 郭劲

doi:10.3788/OPE.20152302.0528

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基于星载光电成像跟踪测距的空间目标定轨

信息科学 | 更新时间：2020-08-13

- 基于星载光电成像跟踪测距的空间目标定轨
- Orbit determination for space target based on opto-electrical imaging, tracking and ranging on satellite
- 光学精密工程 2015年23卷第2期页码：528-539
- 作者机构：
  
  中国科学院长春光学精密机械与物理研究所激光与物质相互作用国家重点实验室,吉林长春,130033
- 作者简介：
  
  [ "王卫兵(1986-),男,陕西杨凌人,研究实习员。2013年于中国科学院长春光学精密机械与物理研究所获得硕士学位,主要从事星载光电跟踪控制技术研究。E-mail:wangweibing10@126.com" ]
  [ "王挺峰(1977-),男,山东文登人,研究员,硕士生导师。2005年于中国科学院长春光学精密机械与物理研究所获得博士学位,主要从事激光应用与光电总体技术研究。Email:wtfeng@sina.com" ]
  [ "郭劲(1964-),男,吉林长春人,研究员,博士生导师,2007年于中国科学院长春光学精密机械与物理研究所获得博士学位,主要从事光电测控与光电总体技术的研究。Email:guojin1964@126.com" ]
- 基金信息：
  
  激光与物质相互作用国家重点实验室基金资助项目(SKLLIM1309)
- DOI：10.3788/OPE.20152302.0528
  中图分类号： V529
- 收稿日期：2014-01-13，
  
  修回日期：2014-03-10，
  
  纸质出版日期：2015-02-25
- 稿件说明：
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王卫兵, 王挺峰, 郭劲. 基于星载光电成像跟踪测距的空间目标定轨[J]. 光学精密工程, 2015,23(2): 528-539

WANG Wei-bing, WANG Ting-feng, GUO Jin. Orbit determination for space target based on opto-electrical imaging, tracking and ranging on satellite[J]. Editorial Office of Optics and Precision Engineering, 2015,23(2): 528-539
王卫兵, 王挺峰, 郭劲. 基于星载光电成像跟踪测距的空间目标定轨[J]. 光学精密工程, 2015,23(2): 528-539 DOI： 10.3788/OPE.20152302.0528.

WANG Wei-bing, WANG Ting-feng, GUO Jin. Orbit determination for space target based on opto-electrical imaging, tracking and ranging on satellite[J]. Editorial Office of Optics and Precision Engineering, 2015,23(2): 528-539 DOI： 10.3788/OPE.20152302.0528.

摘要

以获得空间未知目标的轨迹运动信息为目的

研究了一种基于星载光电成像跟踪测距方式的空间目标定轨技术。该技术从测量学角度出发

利用星载光学测量系统获得目标的相对运动信息

利用角度传感测量系统获得卫星的姿态角变化和跟踪架的角随动信息

最后通过坐标变换解算出目标在地球惯性坐标系中的绝对运动信息。文中依次从物理模型、坐标体系、基本原理等方面对该项技术进行了描述和推导

获得了目标在地球坐标系下的状态方程和观测方程。最后

在对天基监视卫星轨道模型、星载光电跟踪控制模型、目标特性及光学成像测距模型进行分析后

建立了具体的数学模型

并对计算结果进行了分析讨论。得到的结果显示理想模型的目标轨迹测量精度优于0.5 km。

Abstract

A kind of orbit determination technology for a space target based on satellite borne electro-optical imaging

tracking and ranging was proposed to obtain the orbit movement information of the space target. On the basis of surveying

the relative movement information between satellite and target was obtained by the satellite borne optical measuring system

the angle flowing information of satellite attitude angles and rotation angles of tracking frame was captured by corresponding angle sensors

and the absolute motion information of the space target in an earth coordinate system was computed completely through a series of coordinate transformations. The state equation and measurement equation of the target in earth coordinate system were gained after describing physical model

coordinate systems and basic principle in turn. Furthermore

a mathematic simulation was researched after analyzing many models including space-based surveillance satellite orbit

opto-electronic tracking and control

target characteristics and optical imaging and ranging

and the computation results were discussed.The experiments show that the precision of orbit determination is better than 0.5 km for ideal models.

关键词

Keywords

references

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