双星光学观测体系的目标定位误差分析

杨虹; 张占月; 丁文哲; 陈峰

doi:10.3788/CO.20160904.0452

Volume 9 Issue 4

Jul. 2016

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Chinese Optics > 2016 > 9(4): 452-462.

YANG Hong, ZHANG Zhan-yue, DING Wen-zhe, CHEN Feng. Position error analysis of double satellites optical observation system[J]. Chinese Optics, 2016, 9(4): 452-462. doi: 10.3788/CO.20160904.0452

Citation:

YANG Hong, ZHANG Zhan-yue, DING Wen-zhe, CHEN Feng. Position error analysis of double satellites optical observation system[J]. Chinese Optics, 2016, 9(4): 452-462. doi: 10.3788/CO.20160904.0452

YANG Hong, ZHANG Zhan-yue, DING Wen-zhe, CHEN Feng. Position error analysis of double satellites optical observation system[J]. Chinese Optics, 2016, 9(4): 452-462. doi: 10.3788/CO.20160904.0452

Citation:

YANG Hong, ZHANG Zhan-yue, DING Wen-zhe, CHEN Feng. Position error analysis of double satellites optical observation system[J]. Chinese Optics, 2016, 9(4): 452-462. doi: 10.3788/CO.20160904.0452

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Position error analysis of double satellites optical observation system

doi: 10.3788/CO.20160904.0452

1.
Department of Graduate Management, Equipment Academy, Beijing 101416, China
2.
Department of Space Command, Equipment Academy, Beijing 101416, China

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Corresponding author: E-mail:zhangzhan-yue@163.com
Received Date: 06 Apr 2016
Rev Recd Date: 26 Apr 2016
Publish Date: 01 Aug 2016

Abstract

Abstract

In order to improve the positioning accuracy of double satellites optical observation system, a new type of optical positioning system is constructed. Based on the modeling of the satellite and the optical observation platform, the observation vector model between the platform and the target is constructed. According to the geometric location algorithm, the target location model and the location error model are derived, and the location error distribution is obtained by the Monte Carlo method. On this basis, wavelet theory is brought to optimize and reconstruct error for improving the positioning accuracy of double satellites optical observation system. Using the measured data for simulation, the results show that the wavelet theory introduced to reconstruct the position error can make the positioning accuracy increase by 30%. It provides a new way to reduce the location error in engineering.

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References(19)

References

[1]	杨琴,宋锐,马燕新,等.天基空间目标成像仿真系统设计与实现[J].激光与光电子学进展,2015,11:115-123. YANG Q,SONG R,MA Y X,et al.. Design and implement of space-based target imaging simulation system[J]. Laser & Optoelectronics Progress,2015,11:115-123.(in Chinese)
[2]	BLACKMAN S,POPOLI R. Design and Analysis of Modern Tracking Systems[M]. Norwood,M A:Artech House,1999:700-735.
[3]	Space Based Space Surveillance(SBSS)[EB/OL].[2010-09-26].http://www.globalsecurity.org/space/systems/sbss.htm.
[4]	TANG Y,ZHONG W N,LI SH. An improved double r-iteration IOD method for GEO UCTs based on SBSS system[J]. Chinese J. Space Science,2014,34(6):867-871.
[5]	STAIR A T,MILL J D. The Midcourse Space Experiment(MSX)[C]. Proceedings of the 1997 IEEE Aerospace Conference,Snowmass,CO:IEEE,1997:233-245.
[6]	VANDENBERG AFB C. STSS Demo Satellites Track Two-Stage Interceptor in Missile Defense Test[EB/OL].[2010-07-08].http://www.asdnews.com/news.
[7]	张萍,易东云,吴翊,等.空间预警系统的视线测量误差特性研究[J].中国空间科学技术,2004,6:51-56. ZHANG P,YI D Y,WU Y,et al.. The LOS measurement error modeling of space early warning system[J]. Chinese Space Science and Technology,2004,6:51-56.(in Chinese)
[8]	谢恺,韩裕生,薛模根,等.低轨红外预警星座无源定位精度分析[J].信号处理,2008,3:343-348. XIE K,HAN Y SH,XUE M G,et al.. Analysis of passive location accuracy in LEO infrared early warning constellation[J]. Signal Processing,2008,3:343-348.(in Chinese)
[9]	盛卫东,徐洋,周一宇,等.天基光学传感器的视线测量误差分析[J].宇航学报,2011,1:129-135. SHENG W D,XU Y,ZHOU Y Y,et al.. Analysis of LOS measurement error for space-based optical sensor[J]. J. Astronautics,2011,1:129-135.(in Chinese)
[10]	盛卫东,龙云利,周一宇.天基光学传感器网络目标定位精度分析[J].光学学报,2011,31(2):0228001. SHENG W D,LONG Y L,ZHOU Y Y. Analysis of target location accuracy in space-based optical-sensor network[J]. Acta Optica Sinica,2011,31(2):0228001.(in Chinese)
[11]	王秀红,李俊峰,王彦荣.天基照相监测空间目标定轨方法及精度分析[J].光学精密工程,2013,21(6):1394-1403. WANG X H,LI J F,WANG Y R. Orbit determination and precision analysis of space object with space-based camera[J]. Opt. Precision Eng.,2013,21(6):1394-1403.(in Chinese)
[12]	王卫兵,王锐,姜振华,等.天基监视中的双星相对运动模型研究[J].红外与激光工程,2015,44(12):3782-3787. WANG W B,WANG R,JIANG ZH H,et al.. Research on relative movement model of two satellites in space-based surveillance[J]. Infrared and Laser Engineering,2015,44(12):3782-3787.(in Chinese)
[13]	ESA Engineering Standardization Board. Pointing Error Engineering Handbook ESSB-HB-E-003[S]. ESA-ESTEC Requirements & Standards Division,2011.
[14]	OTT T,BENOIT A,VAN DEN BRAEMBUSSCHE P,et al.. ESA pointing error engineering handbook[C]. 8th International ESA Conference on Guidance,Navigation and Control Systems,Karlovy Vary,Czech,2011.
[15]	EISENBIES S K,HOCKEN R J. Error budget by constraints[D]. Charlotte:University of North Carolina at Charlotte,2001.
[16]	李罗钢.临近空间飞行器定位跟踪及拦截弹制导问题研究[D]. 哈尔滨:哈尔滨工业大学,2013. LI L G. Research on the location and of near space aircraft and the guidance of intercepter[D]. Harbin:Harbin Institute of Technology,2013.(in Chinese)
[17]	周晓尧,范大鹏,张智永.升降式光电探测平台定位原理与误差分析[J].宇航学报,2011,32(6):1416-1422. ZHOU X Y,FAN D P,ZHANG ZH Y. Positioning principle and error analysis for lift electro optical detection platform[J]. J. Astronautics,2011,32(6):1416-1422.(in Chinese)
[18]	王卫兵,王挺峰,郭劲.基于双星双目跟踪方式的空间目标定轨技术研究[J].光学学报,2015,35(1):0112006. WANG W B,WANG T F,GUO J. Research on orbit determination technology for space target based on method of tracking with double satellites and double cameras[J]. Acta Optica Sinica,2015,35(1):0112006.
[19]	刘卫,王荣兰,刘四清,等.基于小波变换的卫星阻力系数分析[J].宇航学报,2015,36(2):142-150. LIU W,WANG R L,LIU S Q,et al.. Analysis of satellite drag coefficient based on wavelet transformation[J]. J. Astronautics,2015,36(2):142-150.(in Chinese)