星光折射连续修正方法及制导规划

魏诗卉; 杨春伟; 刘炳琪; 王继平; 苏国华

doi:10.7527/S1000-6893.2020.23734

航空学报 >

2020 , Vol. 41 >Issue 8: 623734 - 623734

DOI: https://doi.org/10.7527/S1000-6893.2020.23734

星光导航技术专栏

星光折射连续修正方法及制导规划

魏诗卉 ,
杨春伟 ,
刘炳琪 ,
王继平 ,
苏国华

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火箭军研究院, 北京 100096

收稿日期: 2019-12-16

修回日期: 2019-12-30

网络出版日期: 2020-03-20

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Stellar refraction: Continuous correction and guidance planning

WEI Shihui ,
YANG Chunwei ,
LIU Bingqi ,
WANG Jiping ,
SU Guohua

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Rocket Military Institute, Beijing 100096, China

Received date: 2019-12-16

Revised date: 2019-12-30

Online published: 2020-03-20

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摘要

针对星光折射模型本身固有的缺点，对星光折射连续修正方法进行了研究，该方法首先探索折射星的分布规律，而后采用Unscented卡尔曼滤波算法+多星连续观测的方案实现定位。同时，对可用星与选星要素和基于突防规划的星光制导弹道设计两方面进行了研究，在星光制导制约机理研究的基础上，提出了惯性/星光制导规划方法，该方法包括导航星的优选策略、导航星优选技术和星点位置的精确计算3步。最后，介绍了星光制导系统的系统组成和功能原理。

关键词： 星光折射; 指数模型; 组合导航; 连续修正; 制导规划

本文引用格式

魏诗卉 , 杨春伟 , 刘炳琪 , 王继平 , 苏国华 . 星光折射连续修正方法及制导规划[J]. 航空学报, 2020 , 41(8) : 623734 -623734 . DOI: 10.7527/S1000-6893.2020.23734

Abstract

To overcome the intrinsic shortcomings of the stellar refraction model, this study examines the continuous correction of stellar refraction. First of all, the distribution rule of refraction stars is explored, followed by the location of the stars through Unscented Kalman Filter and continuous observation of multiple stars. Meanwhile, the constraint mechanism of stellar guidance is studied, involving available stars, star selection elements and design of the stellar guidance trajectory based on penetration planning. Furthermore, an inertial/stellar guidance planning method involving the optimal selection strategy and technology of the navigation star and the accurate calculation of star position is proposed. Finally, the composition and working principle of the stellar guidance system are introduced.

Key words： stellar refraction; exponent model; integrated navigation; continuous correction; guidance planning

参考文献

[1] 吕沧海,冯艳,师海涛. 中远程导弹组合导航技术[M]. 北京:国防工业出版社, 2014:1-3. LV C H, FENG Y, SHI H T. Middle-long-range missile integrated navigation technology[M]. Beijing:National Defense Industry Press, 2014:1-3(in Chinese).
[2] 钱华明,郎希开,钱林琛,等. 弹道导弹的捷联/天文组合导航方法[J]. 北京航空航天大学学报, 2017, 43(5):857-864. QIAN H M, LANG X K, QIAN L C, et al. Ballistic missile SINS/CNS integrated navigation method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(5):857-864(in Chinese).
[3] 全伟,刘百奇,宫晓琳,等. 惯性/天文/卫星组合导航技术[M]. 北京:国防工业出版社, 2011:1-2. QUAN W, LIU B Q, GONG X L, et al. INC/CNS/GNSS integrated navigation technology[M]. Beijing:National Defense Industry Press, 2011:1-2(in Chinese).
[4] 王鑫,王新龙. 弹道导弹SINS/CNS组合导航系统建模与性能仿真[J]. 航空兵器, 2015(2):21-25. WANG X, WANG X L. System modeling and performance simulation on SINS/CNS integrated navigation system for ballistic missile[J]. Aero Weaponry, 2015(2):21-25(in Chinese).
[5] YANG L H, LI B, GE L. A novel SINS/CNS integrated navigation algorithm used in a ballistic missile[J]. International Journal of Security and its Applications, 2015, 9(9):65-76.
[6] 张承,熊智,王融,等.直接敏感地平的空天飞行器惯性/天文组合方法[J]. 中国空间科学技术, 2013, 33(3):64-71. ZHANG C, XIONG Z, WANG R, et al. New INS/CNS integrated algorithm on aerospace vehicle with directly sensing horizon[J]. Chinese Space Science and Technology, 2013, 33(3):64-71(in Chinese).
[7] JAMSHAID A, FANG J C. Realization of an autonomous integrated suite of strap-down astro-inertial navigation systems using unscented particle filtering[J]. Computers and Mathematics with Applications, 2009, 57(2):169-183.
[8] QUAN W, FANG J C, XU F, et al. Hybrid simulation system study of SINS/CNS integrated navigation[J]. IEEE Aerospace & Electronic Systems Magazine, 2008, 23(2):17-24.
[9] WANG X L, MA S. A celestial analytic positioning method by stellar horizon atmospheric refraction[J]. Chinese Journal of Aeronautics, 2009, 22(3):293-300.
[10] NING X L, FANG J C. A new autonomous celestial navigation method for the lunar rover[J]. Robotics and Autonomous Systems, 2009, 57(1):48-54.
[11] 刘炳琪,魏诗卉,苏国华,等. 中远程导弹惯性/星光组合导航关键技术及研究现状[J]. 系统工程理论与实践,2019,39(5):1351-1362. LIU B Q, WEI S H, SU G H, et al. Key technologies and current research status of INS/CNS integrated navigation on intermediate-range missile[J]. System Engineering-Theory & Practice, 2019, 39(5):1351-1362(in Chinese).
[12] 李琳琳,孙辉先. 基于星敏感器的星光折射卫星自主导航方法研究[J]. 系统工程与电子技术,2004, 26(3):352-357. LI L L, SUN H X. Satellite autonomous navigation by stellar refraction based on a star sensor[J]. Systems Engineering and Electronics, 2004, 26(3):352-357(in Chinese).
[13] 王国权,金声震,孙才红, 等. 组合大视场星敏感器星光折射卫星自主导航方法及仿真[J]. 系统仿真学报, 2005, 17(3):529-532. WANG G Q, JIN S Z, SUN C H, et al.Method and simulation of autonomous navigation for satellite by a combination star sensor with large view field and starlight refraction[J]. Journal of System Simulation, 2005, 17(3):529-532(in Chinese).
[14] 王国权,宁书年,金声震,等. 卫星自主导航中星光大气折射模型的研究方法[J]. 中国矿业大学学报, 2004, 33(6):616-620. WANG G Q, NING S N, JIN S Z, et al. Research on star light atmospheric refraction model in autonomous satellite navigation[J]. Journal of China University of Mining & Technology, 2004, 33(6):616-620(in Chinese).
[15] 温永智,吴杰. 基于卫星导航数据在线拟合星光折射模型方法[J]. 国防科技大学学报, 2011, 33(1):7-10. WEN Y Z, WU J. Fitting starlight atmosphere refraction model on line using satellite navigation data[J]. Journal of National University of Defense Technology, 2011, 33(1):7-10(in Chinese).
[16] National Oceanic and Atmospheric Administration, National Aeronautics and Space Administration, U. S. Air Force. U. S. standard atmosphere 1976[M]. 1976.
[17] REES D, BARNETT J J, LABITZKE K. CIRA 1986, COSPAR international reference atmosphere, Part Ⅱ:Middle atmosphere models[J]. Advances in Space Research, 1990, 10(12):1-20.
[18] PICONE J M, HEDIN A E, DROB P, et al. NRLMSISE-00 empirical model of the atmosphere:Statistical comparisons and scientific issues[J]. Journal of Geophysical Research, 2002, 107(A12):SIA 15-1-16.
[19] 王国权,金声震,孙才红, 等.卫星自主导航中25~60公里星光大气折射模型研究[J]. 科技通报,2005,21(1):107-111. WANG G Q, JIN S Z, SUN C H, et al. Study on model of starlight refraction from 25 km to 60 km in autonomous navigation for satellite[J]. Bulletin of Science and Technology, 2005, 21(1):107-111(in Chinese).
[20] 胡静,杨博. 一种改进的星光大气折射观测模型[J]. 红外与激光工程, 2009, 38(2):272-277. HU J, YANG B. Modified measurement model of stellar horizon atmospheric refraction[J]. Infrared and Laser Engineering, 2009, 38(2):272-277(in Chinese).
[21] 武鹏飞,宋峰,魏合理. 星光导航大气折射模型及数据模式研究[J]. 现代防御技术,2017,45(2):6-13. WU P F, SONG F, WEI H L. Atmospheric refraction model and data mode for starlight navigation[J]. Modern Defence Technology, 2017, 45(2):6-13(in Chinese).
[22] MORADI E. Design a low price and high performance sensor network using constrained-based unscented Kalman filter[C]//International Conference on Control, Automation and Systems, 2010:124-129.
[23] 房建成,宁晓琳.天文导航原理及应用[M].北京:北京航空航天大学出版社,2006:185-203. FANG J C, NING X L. Principle and application of astronomical navigation[M]. Beijing:University of Beijing Aeronautics and Astronautics Press, 2006:185-203(in Chinese).

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