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基于捷联式电子罗盘的舰船姿态及姿态速率估计 被引量：3

Attitude and Attitude-Rate Estimation Based on Strapdown Electronic Compass
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摘要 捷联式电子罗盘正被大量应用,根据其自身观测能力,提出了一种新的姿态及姿态速率估计方法,该优化估计方法采用加权统计线性回归技术,与经典的对非线性系统方程的线性化的方法相比具有更高的精度和稳定性。仿真结果表明,该方法可以明显提高捷联式电子罗盘的姿态测量精度,并能同步完成对姿态速率的估计,直接扩展捷联式电子罗盘的功能。 A recursive optimal attitude and attitude-rate estimation algorithm for strapdown electric compass is presented. Weighted statistical linear regression to avoid linearization of nonlinear system equation is applied in the algorithm. The simulation result show that the proposed method would improve the precision of measurement and extend the function of compass obviously.
作者 傅建国 李博 金良安 马野
机构地区 海军大连舰艇学院
出处 《中国航海》 CSCD 北大核心 2004年第2期11-14,共4页 Navigation of China
基金 军队武器装备科研资助项目(H1022003166)
关键词 捷联式电子罗盘 舰船 姿态速率估计 姿态测量 非线性估计 Ship, Navy vessel engineering Attitude determination, Research Attitude-rate Electronic Compass Strapdown, Nonlinear estimation
分类号 U666.1 [交通运输工程—船舶及航道工程]
  • 相关文献

参考文献11

  • 1[1]M Challa, G Natanson, C Wheeler. Simultaneous Determination of Spacecraft Attitude and Rates Using only a Magnetometer [A]. Proceedings of the AIAA/AAS Astrodynamics Specialist Conference [C]. San Diego,CA, 1996,7: AIAA96 - 3630.
  • 2程杨,杨涤,崔祜涛.无陀螺飞行器姿态和角速度确定[J].飞行力学,2001,19(2):34-36. 被引量：4
  • 3[3]J L Crassidis, F L Markley. Predictive Filtering for Attitude Estimation without Rata Sensors [J ]. Journal of Guidance, Control, and Dynamics, 1997, 20(3): 522- 527.
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二级参考文献4

  • 1[1]Flatley T W,Forden J K,Henretty D A,et al.Onboard attitude determination and control algorithms for SAMPEX[A].Proceedings of the Flight Mechanics/ Estimation Theory Symposium[C].Greenbelt,MD,NASA/Goddard Space Flight Center,1990.379-398.
  • 2[2]Challa M S,Natanson G A,Baker D F,et al.Advantages of estimating rate corrections during dynamic propagation of spacecraft rates——applications to real-time attitude determination of SAMPEX[A].Proceedings of the Flight Mechanics/Estimation Theory Symposium[C].Greenbelt,MD,NASA/Goddard Space Flight Center,1994.481-495.
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  • 4[4]Crassidis J L,Markley F L.Predictive filtering for attitude estimation without rate sensors[J].AIAA Journal of Guidance,Control and Dynamics,1997,20(3):522-527.

共引文献3

同被引文献14

  • 1杨勇,缪玲娟,沈军.Method of Improving the Navigation Accuracy of SINS by Continuous Rotation[J].Journal of Beijing Institute of Technology,2005,14(1):45-49. 被引量：22
  • 2周红进,许江宁,马恒,边少锋.GPS与全站仪组合测量载体航向模型研究[J].武汉大学学报（信息科学版）,2005,30(6):510-513. 被引量：6
  • 3许江宁,朱涛,卞鸿巍,徐金华.潜艇真航向测量系统[J].中国惯性技术学报,2005,13(3):76-80. 被引量：7
  • 4王磊,翟国君,黄谟涛.单历元GPS测姿中病态方程解算方法的分析[J].测绘通报,2007(2):7-10. 被引量：8
  • 5Santiago A. Design and performance of a robust GPS/INS attitude system for automobile applications[D]. Stanford, CA: Stanford University, 2004.
  • 6GAO Zhong-yu, NIU Xiao-ji, GUO Mei-feng. Quatemion-based Kalman filter for strapdown attitude heading reference system[J]. Chinese Journal of Aeronautics (S1000-9361), 2002, 15(3): 171-175.
  • 7C. E. Cohen, Attitude Determination Using GPS[D]o Ph.D. Dissertation, Stanford University, Stanford, CA, Dec. 1992.
  • 8M Challa, G Natanson, C W heeler. Simultaneous De- termination of Spacecraft Attitude and Rates Using on- ly a Magnetometer [C]. Proceedings of the AIAA/ AAS Astrodynamics Specialist Conference. San Diego, CA,1996,7.
  • 9C. E. Cohen, Attitude Determination Using GPS [ D]. Ph. D. Dissertation, Stanford Univesiity, Stanford, CA, Dec.1992.
  • 10段智勇,袁信.GPS航姿系统及多天线GPS/惯性组合技术研究[D].南京航天航空大学博士论文,2000.

引证文献3

二级引证文献5

中国航海
2004年 第2期

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