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Volume 35 Issue 6
Jun.  2009
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Journal of Beijing University of Aeronautics and Astronautics  > 2009  >  35(6): 728-731.
Huang Jun, Wu Zhe, Zhu Rongchanget al. Optimized Collocation of Combat Aircraft Weapon Systems for Air Force[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(5): 546-549. (in Chinese)
Citation: Wang Xinlong, Shen Liangliang, Ma Shanet al. Transfer alignment of strapdown inertial navigation systems on rolling bases[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(6): 728-731. (in Chinese)
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Transfer alignment of strapdown inertial navigation systems on rolling bases

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 04 Apr 2008
  • Publish Date: 30 Jun 2009
    Abstract
  • In the process of initial alignment for rolling bases, the accuracy of a model and the observability and observability degree of states are important facts to confirm the filtering effect. A fast and precise alignment method for rolling bases was discussed. Considering time-delay between the master and slave inertial navigation system, a precise transfer alignment model of "velocity + pose" matching was established. The observability analysis of piece-wise constant system (PWCS) and singular value decomposition of observability degree were combined, the observability degree of strapdown inertial navigation system (SINS) -s states were analyzed quantificationally, and the optimal estimation of SINS can be received at the three axes rolling state. Consequently, the SINS can achieve the optimal speed and precision of initial alignment performance. The choice of optimal maneuvers trajectory for carriers and the matching mode of transfer alignment can be gained for alignment of carrier weapons. The simulation results validate the efficiency of this method.

     

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    • References(1)
  • [1] 张静.SINS空中初始对准滤波器的设计[J].上海航天, 2000(6): 34-38 Zhang Jing. Design of the filter for inertial alignment on flying plane of SINS[J]. Aerospace Shanghai, 2000(6): 34-38(in Chinese)[2] Spalding K. An efficient rapid transfer alignment filter .AIAA-92-4598-CP,1992: 1276-1286[3] LimYou-Chol, Joon Lyou. An error compensation method for transfer alignment . USA:IEEE,2001 .[4] Goshen-Meskin D, Bar-Itzhack I Y. Observability analysis of piece-wise constant system-part I: theory[J].IEEE Transactions on Aerospace and Electronics Systems, 1992, 28(4): 1056-1067[5] 程向红,万德钧,仲巡.捷联惯导系统的可观测性和可观测度研究[J].东南大学学报,1997,27(6):6-11 Cheng Xianghong,Wan Dejun,Zhong Xun.Study on observability and its degree of strapdown inertial navigation system[J].Journal of Southeast University,1997,27(6):6-11(in Chinese)
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