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硬件增强角速率圆锥优化算法的姿态解算精度分析及改进 被引量:5

Accuracy analysis of attitude computation and improvement for coning algorithm optimized with hardware-enhanced angular rates
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摘要 在分析传统硬件增强角速率圆锥优化算法姿态解算精度的基础上,提出了一种改进的算法,对传统算法中的周期分量进行了二次优化.首先通过分析传统算法的各轴分量相对于旋转矢量变化量的真值以及理想值的误差来确定算法的姿态解算精度,然后根据经典圆锥运动建立二次优化的误差准则并推导了相应的二次优化系数,最后在不同的经典圆锥运动环境下对传统算法以及改进算法的姿态解算精度进行仿真对比.结果表明,对传统算法的姿态解算精度的分析是正确合理的,而且只需采用改进的三子样算法就可以获得与根据理想值得到的结果几乎完全一致的姿态解算精度. Based on the accuracy analysis of attitude computation for the traditional coning algorithm optimized with hardware-enhanced angular rates,an improved coning algorithm is proposed to secondly optimize the periodic components in the traditional one.The accuracy of attitude computation is first determined by analyzing the error of any axis component in the traditional algorithm relative to the true and theoretical values of the change of rotation vector.Then an error criterion for the second optimization is established according to classical coning motion,and the corresponding coefficients are derived.Simulations are carried out in various classical coning environments to compare the accuracy of attitude computation for the traditional and improved algorithms.The results show that the accuracy analysis of attitude computation for the traditional algorithm is correct and reasonable.Furthermore,only using the improved three-subinterval algorithm the accuracy of attitude computation can be almost the same as that acquired from the theoretical value.
出处 《东南大学学报(自然科学版)》 EI CAS CSCD 北大核心 2012年第4期632-636,共5页 Journal of Southeast University:Natural Science Edition
基金 国家自然科学基金资助项目(50975049) 国家重点基础研究发展计划(973计划)资助项目(2009CB724002) 高等学校博士学科点专项科研基金资助项目(20110092110039)
关键词 圆锥优化算法 姿态解算 精度分析 周期分量 二次优化 optimal coning algorithm attitude computation accuracy analysis periodic component second optimization
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  • 1缪玲娟,林丽.减小动态误差的捷联系统姿态算法研究[J].兵工学报,2000,21(3):229-232. 被引量:4
  • 2刘危,解旭辉,李圣怡.捷联惯性导航系统的姿态算法[J].北京航空航天大学学报,2005,31(1):45-50. 被引量:10
  • 3魏小莹,林玉荣,邓正隆.光纤陀螺捷联姿态算法的改进研究[J].中国惯性技术学报,2005,13(2):70-74. 被引量:14
  • 4Jiang Y F,IEEE Transaction Aerospace Electronic Systems,1992年,28卷,2期,484页
  • 5Lee J G,J Guidance Control Dynamics,1990年,13卷,4期,738页
  • 6Jiang Y F,IEEE Trans Aerospace Electronic Systems,1992年,28卷,2期,484页
  • 7Miller R B.A new strap-down attitude algorithm[J].Journal of Guidance Control and Dynamics,1983,6(4):287~291
  • 8Jiang Y F,Lin Y P.Improved strap-down coning algorithms[J].IEEE Transaction on Arospace and Electronic System,1992,28(2):484~490
  • 9黄昊.[D].哈尔滨:哈尔滨工业大学控制工程系,2001.
  • 10Miller R B.A new strap-down attitude algorithm[J].Journal of Guidance,Control,and Dynamics,1983,6(4):287-291.

共引文献58

同被引文献24

  • 1曾庆化,刘建业,熊智,赵伟.一种角速率激光陀螺惯导系统高精度姿态算法[J].上海交通大学学报,2006,40(12):2159-2163. 被引量:12
  • 2Miller R. A new strapdown attitude algorithm. Journal of Guidance, Control, and Dynamics, 1983, 6(4): 287-291.
  • 3Ignagni M B, Optimal strapdown attitude integration algorithms, Journal of Guidance, Control, and Dynamics, 1990, 13(2): 363-369.
  • 4Savage P G. Coning algorithm design by explicit frequency shaping[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(4): 1123-1132.
  • 5Savage P G. Explicit frequency-shaped coning algorithms for pseudoconing environments[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(3): 774-782.
  • 6Park C G, Kim K J, Lee J G, et al. Formalized approach to obtaining optimal coefficients for coning algorithms[J]. Journal of Guidance, Control, and Dynamics, 1999, 22(1): 165-168.
  • 7MILLER R B. A new strapdown attitude algorithm[J]. Journal of Guidance Control and Dynamics,1983,6(4) :287-291.
  • 8SONG M, WU W Q, PAN X F. Approach to recovering maneuver accuracy in classical coning algorithms [J]. Journal of Guidance Control and Dynamics 2013,36 (6) : 1872-1880.
  • 9张荣辉,贾宏光,陈涛,张跃.基于四元数法的捷联式惯性导航系统的姿态解算[J].光学精密工程,2008,16(10):1963-1970. 被引量:172
  • 10杨胜,房建成.一种单子样旋转矢量姿态算法[J].宇航学报,2010,31(3):780-785. 被引量:14

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