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捷联惯导与天文导航组合导航系统仿真研究 被引量:2

Simulation of SINS/CNS Integrated Navigation System
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摘要 介绍了捷联惯导与天文导航(SINS/CNS)组合导航仿真方案,简要设计和实现了SINS/CNS组合导航软件仿真平台;以Kalman滤波为基础,通过将SINS和CNS所测得的飞行器相关姿态和位置信息进行数据融合,估计出组合导航系统的误差状态量,进而修正SINS的位置、速度和姿态,最后在该系统下进行仿真,验证了这种设计方案的可行性和有效性。 The research on simulation software of SINS/CNS is very important to the conceptual definition,system design and development.In this paper,a scheme of integrated SINS/CNS is proposed and a simulation software of the integrated SINS/CNS Navigation system is designed and implemented.SINS and CNS can provide corresponding attitude data.Fusing these data can estimate the error state value of integrated navigation system and correct the position of aircraft,velocity and attitude angle based on Kalman filter.The applicability of the design method is tested and analyzed.Result shows that the simulation software is feasible and useful for further studies.
作者 陈坡 孙付平
出处 《海洋测绘》 2010年第6期55-58,共4页 Hydrographic Surveying and Charting
关键词 SINS/CNS KALMAN滤波 仿真 软件设计 SINS/CNS Kalman filter simulation software design
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  • 1刘朝山,何鸣,刘光斌.星敏感器测量导弹姿态的方法研究[J].战术导弹控制技术,2005(3):23-25. 被引量:7
  • 2林雪原,刘华章,史佩.一种低成本、低精度SINS/GPS组合导航系统及试验研究[J].武汉大学学报(信息科学版),2006,31(10):871-874. 被引量:11
  • 3[5]Titterton D H,Weston J L.Strapdown Inetial Navigation Technology[M].PeterPeregrinus,U.K.,1997
  • 4以光衢.惯性导航原理[M].北京:航空工业出版社,1987..
  • 5王觉先. 星光-惯性制导在战略导弹上的应用研究[R]. 北京: 航天情报研究报告,1994.
  • 6Ritland J I, Spalding K J. Impact of inertial system quality on GPS-inertial performance in a jamming environment[R]. AIAA Guidance Navigation and Control Conference, 1987: 1459-1467
  • 7林来兴.空间交会对接技术[M].北京:宇航出版社,1994:63-65.
  • 8Gaylor D E. Integrated GPS/INS navigation system design for autonomous spacecraft rendezvous[D]. Austin: The University of Texas, December 2003.
  • 9Jekeli C. Inertial navigation systems with geodetic applications[M]. Berlin: Walter de Gruyter, 2001 : 150-201.
  • 10Upadhyay T, Cotterill S. Autonomous GPS/INS navigation experiment for space transfer vehicle[J]. IEEE Transactions on Aerospace and Electronic Systems, 1993, 20(3): 29-39.

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  • 1祝刚,苏伟,魏可惠,李世玲.自由段航天器惯性/星光组合定位方法研究[J].宇航学报,2007,28(6):1589-1592. 被引量:4
  • 2王新龙,马闪.A Celestial Analytic Positioning Method by Stellar Horizon Atmospheric Refraction[J].Chinese Journal of Aeronautics,2009,22(3):293-300. 被引量:13
  • 3GUL F, FANG Jian-cheng. Alternate of GPS for Ballis- tic Vehicle Navigation [ C ]//Proceedings of the 1 st In-ternational Symposium on Systems and Control in Aero- space and Astronautics, 2006 : 19 -24.
  • 4PITTELKAU M E. Kalman Filter for Spacecraft System Alignment Calibration[ J]. Journal of Guidance, Control and Dynamics, 2001 , 24(6) : 1187-1195.
  • 5Quang Lain, WOODRUFF C, ASHTON S, et al. Noise Estimation for Star Tracker Calibration and Enhanced Precision Attitude Determination [ C ]// Proceedings of the Fifth International Conference on Information Fu- sion, 2002:235-242.
  • 6KAPLAN G H, Determining the Position and Motion of a Vessel fi'om Celestial Observations[ J]. Journal of the In- stitute of Navigation, 1995,42 ( 4 ) : 631 -638.
  • 7Jason L Speyer, David Dannemiller, David Walker. Pe- riodic Optimal Cruise of an Atmospheric Vehicle [ J ]. Journal of Guidance, 1985,146 ( 8 ) : 31 -38.
  • 8杨颖,王明海.星光/惯性组合制导方案与位置误差分析[J].上海航天,2007,24(6):31-33. 被引量:2
  • 9Sungkoo B. Glas SPACECRAFT Attitude Determination U- sing CCD Star Tracker and 3-Axis Gyros [ D]. Texas :The University of Texas at Austin, 1998 : 137 - 173.
  • 10Wang Xinlong, Xie Jia, Ma Shan. Starlight Atmospheric Refraction Model for a Continuous Range of Height [ J]. Journal of Guidance Control and Dynamics, 2010, 33 (2) : 634 - 637.

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