• Electronics Optics & Control
  • Vol. 27, Issue 2, 18 (2020)
MENG Chunjian, LI Kailong, and ZHANG Mengde
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2020.02.005 Cite this Article
    MENG Chunjian, LI Kailong, ZHANG Mengde. Comparison of Kalman Filters for SINS Based Integrated Navigation[J]. Electronics Optics & Control, 2020, 27(2): 18 Copy Citation Text show less
    References

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    [6] MARKLEY F L, CRASSIDIS J L.Fundamentals of space craft attitude determination and control[M].New York:Springer, 2015.

         [7]CRASSIDIS J L, MARKLEY F L, CHENG Y.Survey of nonlinear attitude estimation methods[J].Journal of Guidance, Control, and Dynamics, 2007, 30(1):12-28.

    [7] CRASSIDIS J L, MARKLEY F L.Unscented filtering for spacecraft attitude estimation[J].Journal of Guidance, Control, and Dynamics, 2003, 26(4):536-542.

    [8] SHIN E H, EL-SHEIMY N.An unscented Kalman filter for in-motion alignment of low cost IMUs[C]//Proceedings of the IEEE Position Location and Navigation Symposium, 2004:273-279.

    [9] YANG Y H, ZHOU J C, LOFFELD O.Quaternion-based Kalman filtering on INS/GPS[C]//The 15th IEEE International Conference on Information Fusion, 2012:511-518.

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    [1] QI Wenhao, LIU Ning, SU Zhong, QIAO Likang, WANG Jingxiao. Conjugate Gradient Based Method for Attitude Calculation of MARG Sensor[J]. Electronics Optics & Control, 2022, 29(8): 13

    MENG Chunjian, LI Kailong, ZHANG Mengde. Comparison of Kalman Filters for SINS Based Integrated Navigation[J]. Electronics Optics & Control, 2020, 27(2): 18
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