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角速率输入下捷联航姿算法研究 被引量:1

Study of Strapdown Navigation Attitude Algorithms for Angular Rate Input
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摘要 文中针对工程实际中陀螺输出的角速率形式,研究了锥运动条件下捷联惯导系统姿态计算中旋转矢量双子样、三子样法和四元数法,并提出了一种改进双子样法,对各算法的漂移误差进行了仿真分析。仿真结果表明在角速率输入情况下改进双子样法的精度优于其他算法,是一种较理想的高精度捷联航姿算法。 The attitude updating algorithm is a determinant factor in strapdown inertial navigation system (SINS). According to the practical projects, this paper studies two-sample, three-sample rotation vector and quaternion under the coning base motion, and an improved two-sample rotation vector algorithm is provided. The simulation results show that the accuracy of the improved two-sample rotation vector algorithm is better than that of other algorithms.
出处 《弹箭与制导学报》 CSCD 北大核心 2005年第4期6-8,共3页 Journal of Projectiles,Rockets,Missiles and Guidance
基金 水下信息处理与控制国防科技重点实验室基金。(项目编号:51448060105HK0361)
关键词 捷联惯导系统 锥运动 四元数 旋转矢量 SINS coning motion quaternion rotation vector
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参考文献4

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二级参考文献2

  • 12, Jiang Y F. Lin Y P. Improved strapdown coning algorithms. IEEE Transactions on Aerospace and Electronic System,1992, 28(2):482~489
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共引文献3

同被引文献11

  • 1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
  • 2练军想,胡德文,胡小平,吴文启.捷联惯导姿态算法中的圆锥误差与量化误差[J].航空学报,2006,27(1):98-103. 被引量:12
  • 3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
  • 4BORTZ J E.A new mathematical formulation for strapdown inertial navigation[J].IEEE Transactions on Aerospace and Electronic Systems,1971,7(1):61-66.
  • 5KELLY M.Roscoe equivalency between strap-down inertial navigation coning and sculling integrals algorithms[J].Journal of Guidance,Control,and Dynamics,2001,24(2):2005.
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  • 8LEE J G,YOON Y J,MARK J G.Extension of strap-down attitude algorithm for high-frequency base motion[J].Journal of Guidance,Control,and Dynamics,1990,13(4):738-743.
  • 9MARK J G,TAZARTES D A.Tuning of coning algorithms to gyro date frequency response characteristics[J].Journal of Guidance,Control,and Dynamics,2001,24(4):641-647.
  • 10黄昊,邓正隆.角速率输入下的航姿算法研究[J].中国惯性技术学报,2000,8(2):21-26. 被引量:20

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