Volume 41 Issue 9
Sep.  2015
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TAN Caiming, WANG Yu, SU Yan, et al. The simplest multi-position analytic alignment for SINS[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1645-1650. doi: 10.13700/j.bh.1001-5965.2015.0033(in Chinese)
Citation: TAN Caiming, WANG Yu, SU Yan, et al. The simplest multi-position analytic alignment for SINS[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1645-1650. doi: 10.13700/j.bh.1001-5965.2015.0033(in Chinese)

The simplest multi-position analytic alignment for SINS

doi: 10.13700/j.bh.1001-5965.2015.0033
  • Received Date: 19 Jan 2015
  • Publish Date: 20 Sep 2015
  • The strapdown inertial navigation system (SINS) need to be installed on a servo platform and rotated through 90 ° or 180 ° about the up axis for traditional multi-position analytic alignment method. Thus it will bring inconvenience, and the precision of the servo platform will directly affect the precision of the multi-position analytic alignment method. To address the issue, a simplest multi-position analytic alignment method was proposed. The multi-position analytic alignment can be done by any two positions, or to say, the constant biases of the inertial measurement unit (IMU) can be ordinarily obtained through the information in any two positions. The computation procedure of this method was given and simulations proved the validity of this method. The simplest multi-position analytic alignment with any two positions can be used as a simple initial alignment method or a field calibration method. Moreover, it is proposed that the constant bias of the accelerometer or the constant drift of the gyroscope in a certain axis can be well estimated when the IMU stays in some particular attitudes. The conclusion can be used for further improvement of the multi-position alignment method.

     

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  • [1]
    Paul G S.Blazing gyros:The evolution of strapdown inertial navigation technology for aircraft[J].Journal of Guidance,Control,and Dynamics,2013,36(3):637-655.
    [2]
    Liu X X,Xu X S,Wang L H,et al.A fast compass alignment method for SINS based on saved data and repeated navigation solution[J].Measurement,2013,46(10):3836-3846.
    [3]
    Titterton D,Weston J L.Strapdown inertial navigation technology[M].2nd ed.London:Institution of Engineering and Technology,2004:277-308.
    [4]
    Cho S Y,Lee H K,Lee H K.Observability and estimation error analysis of the initial fine alignment filter for nonleveling strapdown inertial navigation system[J].Journal of Dynamic Systems,Measurement and Control,2012,135(2):44-45.
    [5]
    Wang X.Fast alignment and calibration algorithms for inertial navigation system[J].Aerospace Science and Technology,2009,13(4-5):204-209.
    [6]
    Wu Y X,Zhang H L,Wu M P,et al.Observability of strapdown INS alignment:A global perspective[J].IEEE Transactions on Aerospace and Electronic Systems,2012,48(1):78-102.
    [7]
    Xiong J,Guo H,Yang Z H.A two-position SINS initial alignment method based on gyro information[J].Advances in Space Research,2014,53(11):1657-1663.
    [8]
    王巍.光纤陀螺惯性系统[M].北京:中国宇航出版社,2013:449-464.Wang W.Inertial navigation system of the fiber optic gyroscope[M].Beijing:China Astronautic Publishing House,2013:449-464(in Chinese).
    [9]
    邓志红,付梦印,张继伟,等.惯性器件与惯性导航系统[M].北京:科学出版社,2012:261-265.Deng Z H,Fu M Y,Zhang J W,et al.Inertial device and inertial navigation system[M].Beijing:Science Press,2012:261-265(in Chinese).
    [10]
    Lee J G,Park C G,Park H W.Multiposition alignment of strapdown inertial navigation system[J].IEEE Transactions on Aerospace and Electronic Systems,1993,29(4):1323-1328.
    [11]
    Chung D,Lee J G,Park C G,et al.Strapdown INS error model for multiposition alignment[J].IEEE Transactions on Aerospace and Electronic Systems,1996,32(4):1362-1366.
    [12]
    赵长山,秦永元,周琪.参数辨识双位置对准改进算法[J].中国惯性技术学报,2009,17(6):631-635.Zhao C S,Qin Y Y,Zhou Q.Modified two-position parameter identification alignment method[J].Journal of Chinese Inertial Technology,2009,17(6):631-635(in Chinese).
    [13]
    秦永元.惯性导航[M].北京:科学出版社,2006:361-363.Qin Y Y.Inertial navigation[M].Beijing:Science Press,2006:361-363(in Chinese).
    [14]
    Zhao H,Shang H,Wang Z,et al.Comparison of initial alignment methods for SINS[C]//World Congress on Intelligent Control and Automation (WCICA).Piscataway,NJ:IEEE Press,2011:42-47.
    [15]
    Song L,Zhang C,Lu J.Self-alignment of full skewed RSINS:Observability analysis and full-observable Kalman filter[J].Journal of Systems Engineering and Electronics,2014,25(1):104-114.
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