期刊文献+

方向余弦矩阵中四元数提取算法比较 被引量:12

Comparison of algorithms for extracting quaternion from DCM
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摘要 在捷联惯性导航系统姿态算法中,用四元数取代方向余弦阵来描述姿态变化具有计算量小、精度高、不存在奇异问题的优点。在实际工程应用中常常需要从方向余弦矩阵中提取对应的旋转四元数,但是经典的提取算法可能会出现平方根计算时根号内出现负值的情况,从而使四元数的提取失败。针对这一问题,总结了现有文献中提出的两种新算法,并从计算量和计算精度的角度对这几种算法进行了分析对比,通过比较发现基于特征值和特征向量的提取算法实现了计算量和精度的最佳组合,为工程应用提供了有价值的参考。 While describing the attitude changes in SINS algorithm, quaternion method is superior to direction cosine matrix because the former requires less computation, gives better accuracy and avoids singularity. Extracting the rotation quaternion from the direction cosine matrix is often needed in engineering applications, but the classical extracting algorithm has a fatal disadvantage which will result in an extraction failure when negative value appears in a square root computation. Aiming at this problem, two new algorithms from the literatures available was introduced and analyzed from the aspect of the computation complexity and the precision. The comparison of computation results shows that the algorithm based on eigenvalue and eigenvector performs the best combination of computation complexity with precision, which is valuable for the engineering application.
出处 《中国惯性技术学报》 EI CSCD 2008年第4期415-418,共4页 Journal of Chinese Inertial Technology
基金 “十一五”总装预研项目(51309060401)
关键词 四元数 姿态 方向余弦矩阵 提取 quatemion attitude direction cosine matrix extraction
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参考文献7

  • 1张士邈,刘放,秦永元.捷联惯导姿态算法若干问题的研究[J].中国惯性技术学报,2002,10(2):1-6. 被引量:11
  • 2Lee H K, Lee J G; Roh Y K, et al. Modeling quatemion errors in SDINS: computer frame approach[J]. IEEE Transactions on Aerospace and Electronic Systems, 1998, 34 (1): 289-297.
  • 3孙丽,秦永元.捷联惯导系统姿态算法比较[J].中国惯性技术学报,2006,14(3):6-10. 被引量:48
  • 4周江华,苗育红,肖刚.捷联惯导系统初始四元数提取的新算法[J].飞行力学,2003,21(3):63-66. 被引量:7
  • 5Bar-Itzhack I Y. New method for extracting the quatemion from a rotation matrix[J]. Journal of Guidance and Control, 2000, 23(6): 1085-1087.
  • 6Bar-Itzhack I Y. Iterative optimal orthogonalization of the strapdown matrix[J]. IEEE Transactions on Aerospace and Electronic Systems, 1975, AES-11(1): 30-37.
  • 7Shuster M D, Oh S D. Three-axis attitude determination from vector observations[J]. Journal of Guidance and Control, 1981, 4(1): 70-77.

二级参考文献9

  • 1以光衢.惯性导航原理[M].北京:航空工业出版社,1987..
  • 2Britting K R. Inertial navigation system analysis[M].New York :Wiley Interseienee, 1971.
  • 3Schaub H, Junkins J L. Stereographic orientation parameters for attitude dynamics: A generalization of the rodrigues parameters[J]. Journal of Astronautical Sciences, 1996, 44(1 ): 1-19.
  • 4Bortz J E. A new mathematical formulation for strapdown inertial navigation[J]. IEEE Trans. on Aerospace and ElectronicSystems, 1971, 7(1): 61-66.
  • 5Miller R B. A new strapdown attitude algorithm[J]. Journal of Guidance, Control, and Dynamics, 1983, 6(4): 287-291.
  • 6Lee J G, Yoon Y J, Mark J G, Tazartes D A. Extension of strapdown attitude algorithm for high-frequency base motion[J].Journal of Guidance, 1990, 13(4): 738-743.
  • 7周江华,苗育红,李宏,孙国基.四元数在刚体姿态仿真中的应用研究[J].飞行力学,2000,18(4):28-32. 被引量:41
  • 8柴卫华,侯芸.捷联惯导系统姿态算法研究[J].现代防御技术,2001,29(4):42-45. 被引量:16
  • 9林雪原,刘建业,刘红.一种改进的激光捷联旋转矢量姿态算法(英文)[J].Transactions of Nanjing University of Aeronautics and Astronautics,2003,20(1):47-52. 被引量:6

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