Volume 46 Issue 12
Dec.  2020
Turn off MathJax
Article Contents
GUO Jiangang, CHEN Peng, ZHENG Weiet al. Data fusion algorithm of multi-sensor redundant inertial navigation and its application in self-alignment[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(12): 2211-2216. doi: 10.13700/j.bh.1001-5965.2019.0604(in Chinese)
Citation: GUO Jiangang, CHEN Peng, ZHENG Weiet al. Data fusion algorithm of multi-sensor redundant inertial navigation and its application in self-alignment[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(12): 2211-2216. doi: 10.13700/j.bh.1001-5965.2019.0604(in Chinese)

Data fusion algorithm of multi-sensor redundant inertial navigation and its application in self-alignment

doi: 10.13700/j.bh.1001-5965.2019.0604
Funds:

National Natural Science Foundation of China 0901010517001

More Information
  • Corresponding author: ZHENG Wei, E-mail: zhengwei@nudt.edu.cn
  • Received Date: 26 Nov 2019
  • Accepted Date: 06 Dec 2019
  • Publish Date: 20 Dec 2020
  • For the self-alignment problem of the multi-sensor redundant inertial navigation system, the data fusion algorithm of the inertial navigation system is studied based on ten-sensor inertial navigation system which consists of three-orthogonal and two-skew sensors. The validity of the least square estimation data fusion algorithm in improving the self-alignment accuracy of the system is verified through analysis and simulation. Then, a static alignment experiment is conducted and a weighted matrix based on the bias stability is established. The results of the experiment show that, compared with using the data of orthogonal instruments only, the data fusion can effectively improve the self-alignment accuracy of the system and make full use of the data of the skew redundant instruments. The accuracy of the improved algorithm is slightly better than that of Markov estimation.

     

  • loading
  • [1]
    SABLYNSKI R, PORDON R.A report on the flight of Delta II's redundant inertial flight control assembly (RIFCA)[C]//IEEE 1998 Position Location and Navigation Symposium, 1998: 98CH36153.
    [2]
    彭蓉, 严恭敏, 秦永元.箭载捷联惯导系统水平自对准的两种实用方法[J].中国惯性技术学报, 2009, 17(4):428-435. http://www.cnki.com.cn/Article/CJFDTotal-ZGXJ200904015.htm

    PENG R, YAN G M, QIN Y Y.Two practical methods of autonomous leveling alignment for launch vehicle SINS[J].Journal of Chinese Inertial Technology, 2009, 17(4):428-435(in Chinese). http://www.cnki.com.cn/Article/CJFDTotal-ZGXJ200904015.htm
    [3]
    崔潇, 秦永元, 严恭敏, 等.基于矩阵卡尔曼滤波的捷联惯导初始对准算法[J].中国惯性技术学报, 2018, 26(5):585-590. http://www.cqvip.com/QK/83064X/201805/6100094183.html

    CUI X, QIN Y Y, YAN G M, et al.Initial alignment algorithm for SINS based on state matrix Kalman filter[J].Journal of Chinese Inertial Technology, 2018, 26(5):585-590(in Chinese). http://www.cqvip.com/QK/83064X/201805/6100094183.html
    [4]
    郭泽, 缪玲娟, 赵洪松.一种改进的强跟踪UKF算法及其在大方位失准角初始对准中的应用[J].航空学报, 2014, 35(1):203-214. http://www.cnki.com.cn/Article/CJFDTotal-HKXB201401021.htm

    GUO Z, MIAO L J, ZHAO H S.An improved strong tracking UKF algorithm and its application in SINS initial alignment under large azimuth misalignment angles[J].Acta Aeronautica et Astronautica Sinica, 2014, 35(1):203-214(in Chinese). http://www.cnki.com.cn/Article/CJFDTotal-HKXB201401021.htm
    [5]
    HE H Y, XU J N, LI J S, et al.Improved fast backtracking alignment approach for strapdown inertial navigation system[J].Journal of Chinese Inertial Technology, 2015, 23(2):179-183. http://www.researchgate.net/publication/282986198_Improved_fast_backtracking_alignment_approach_for_strapdown_inertial_navigation_system
    [6]
    郭士荦, 许江宁, 李峰.强跟踪CKF及其在惯导系统初始对准中的应用[J].中国惯性技术学报, 2017, 25(4):436-441. http://www.cnki.com.cn/Article/CJFDTotal-ZGXJ201704003.htm

    GUO S L, XU J N, LI F.Strong tracking cubature Kalman filter for initial alignment of inertial navigation system[J].Journal of Chinese Inertial Technology, 2017, 25(4):436-441(in Chinese). http://www.cnki.com.cn/Article/CJFDTotal-ZGXJ201704003.htm
    [7]
    BAR-ITZHACK I Y, HARMAN R R.In-space calibration of a skewed gyro quadruplet[J].Journal of Guidance, Control, and Dynamics, 2002, 25(5):852-859. doi: 10.2514/2.4978
    [8]
    PITTELKAU M E.Calibration and attitude determination with redundant inertial measurement units[J].Journal of Guidance, Control, and Dynamics, 2005, 28(4):743-752. doi: 10.2514/1.7040
    [9]
    PITTELKAU M E.Cascaded and decoupled RIMU calibration filters[J].The Journal of the Astronautical Sciences, 2006, 54:449-466. doi: 10.1007/BF03256500
    [10]
    YUKSEL Y, EL-SHEIMY N.An optimal fusion method for skew-redundant inertial measurement units[J].Journal of Applied Geodesy, 2011, 5(2):99-115. http://adsabs.harvard.edu/abs/2011jageo...5...99y
    [11]
    秦永元, 张洪钺, 汪叔华.卡尔曼滤波与组合导航原理[M].西安:西北工业大学出版社, 2015:63-68.

    QIN Y Y, ZHANG H Y, WANG S H.Theory of Kalman filter and integrated navigation[M].Xi'an:Northwestern Polytechnical University Press, 2015:63-68(in Chinese).
    [12]
    GILMORE J P.SIRU development final report[R].Washington, D.C.: NASA, 1973: 11-16.
    [13]
    秦永元.惯性导航[M].北京:科学出版社, 2006:240-241.

    QIN Y Y.Inertial navigation[M].Beijing:Science Press, 2006:240-241(in Chinese).
    [14]
    梅春波, 秦永元, 游金川.SINS在大失准角条件下的非线性量测初始对准算法[J].宇航学报, 2016, 37(3):1-7. http://www.cqvip.com/QK/95668X/20163/668348697.html

    MEI C B, QIN Y Y, YOU J C.Nonlinear measurement based SINS initial alignment for large misalignment angles[J].Journal of Astronautics, 2016, 37(3):1-7(in Chinese). http://www.cqvip.com/QK/95668X/20163/668348697.html
    [15]
    夏益霖, 吴家驹.航天发射的低频振动环境及其模拟[J].强度与环境, 1998(1):1-8. http://www.cnki.com.cn/Article/CJFDTotal-QDHJ199801000.htm

    XIA Y L, WU J J.Low-frequency vibration environment and its simulation for aerospace launch[J].Structure & Environment Engineering, 1998(1):1-8(in Chinese). http://www.cnki.com.cn/Article/CJFDTotal-QDHJ199801000.htm
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Figures(2)  / Tables(4)

    Article Metrics

    Article views(578) PDF downloads(110) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return