期刊文献+

一种改进的基于双矢量观测的姿态确定算法 被引量:4

Improved determination algorithm using two vector measurements
下载PDF
导出
摘要 为了提高飞行器姿态确定的精度和姿态矩阵的解算速度,提出了一种改进的双矢量定姿算法.这种算法利用测量系统的方差对两个观测矢量进行加权处理,求得一个新的矢量,以两观测矢量夹角为判断依据选取加权系数;以新矢量为基准矢量,利用双矢量定姿算法求解姿态矩阵,并对求得的姿态矩阵进行修正.仿真结果表明:这种算法所需时间为优化算法的50%,当两个传感器测量误差不同、两矢量为任意夹角时,这种算法比优化的双矢量算法精度高;当两个传感器测量误差相同时,除了两矢量夹角为90°外,这种算法均比优化的双矢量算法精度高. To improve the spacecraft attitude determination accuracy and the computational efficiency of attitude matrix, an improved TRIAD algorithm was proposed. In this algorithm, the two observation vectors was weighted utilizing the variance of the measurement system, the weighting coefficient was selected according to the angle between the two observation vectors, the attitude matrix was solved using TRIAD algorithm, and then the matrix was amended. It shows that the computation time of this algorithm is half of the optimized TRI- AD algorithm. When the measurement error of two sensors is difference, the accuracy of this algorithm is bet- ter than the optimized TRIAD algorithm for any angle of the two vectors. When the two sensors have the same measurement error, the accuracy of this algorithm is better than the optimized TRIAD algorithm except the an- gle of the two vectors is 90.
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2012年第8期992-995,共4页 Journal of Beijing University of Aeronautics and Astronautics
基金 国家自然科学基金资助项目(50805006)
关键词 双矢量定姿 观测矢量 姿态确定 TRIAD vector observation attitude determination
  • 相关文献

参考文献7

  • 1Shuster M D,Oh S D. Three-axis attitude determination from vec- tor observations [J].Journal of Guidance and Control, 1981, 4(1) :70 -77.
  • 2林玉荣,邓正隆.基于矢量观测确定飞行器姿态的算法综述[J].哈尔滨工业大学学报,2003,35(1):38-45. 被引量:24
  • 3Shuster M D. The optimization of TRIAD [ J]. The Journal of the Astronautical Sciences ,2007,55 ( 2 ) :245 - 257.
  • 4ltzhack Y B,Richard R H. Optimized TRIAD algorithm for atti- tude determination [ J]. Journal of Guidance and Control, 1997, 20(1) :208 -211.
  • 5Tanygin S, Shuster M D. The many TRIAD algorithms [ C ]// Markley L F. Advances in the Astronautical Sciences. America: Space Flight Mechanics A ,2007,127:81 -99.
  • 6陈浩,谭久彬.一种改进的TRIAD飞行器姿态确定方法[J].系统仿真学报,2008,20(8):2101-2104. 被引量:6
  • 7Freund Y. A decision-theoretic generalization of online learning and an application to boosting [J].Journal of Computer and Sys- tem Science, 1997,55 ( 1 ) : 119 - 139.

二级参考文献8

  • 1G Wahba. Problem 65.1, A Least-Squares Estimation of Satellite Attitude [J]. SIAM Review (S0036-1445), 1965, 7(3): 409.
  • 2M D Shuster, S D Oh. Three-Axis Attitude Determination from Vector Observations [J]. Journal of Guidance and Control (S0731-5090), 1981, 4(1): 70-77.
  • 3Itzhack Y. Bar-Itzhack, Richard R. Harman. Optimized TRIAD Algorithm for Attitude Determination [J]. Journal of Guidance, Control and Dynamics (S0731-5090), 1997, 20( 1): 208-211.
  • 4Christopher D. Hall. Chapter 4 Attitude Determination [EB/OL]. (03-02-24) [2007-01-08] http://www.aoe.vt.edu/-cdhall/courses/ aoe4140/.
  • 5盖尔布,胡寿松,伍立明.应用最优估计[M].北京:国防工业出版社,19895-6.
  • 6黎湧,吴宏鑫,刘良栋.融合TRIAD算法用于GPS姿态确定[J].中国空间科学技术,2000,20(2):30-37. 被引量:11
  • 7林玉荣,邓正隆.基于矢量观测确定飞行器姿态的算法综述[J].哈尔滨工业大学学报,2003,35(1):38-45. 被引量:24
  • 8刘瑞华.一种微捷联惯导系统姿态角最优估计算法研究[J].系统仿真学报,2004,16(1):142-145. 被引量:5

共引文献28

同被引文献27

引证文献4

二级引证文献10

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部