Volume 33 Issue 1
Jan.  2013
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Du Jiyong, Zhang Fengming, Li Jianwen, Huang Guorong, Dai Feng. Improved equivalent rotation vector based attitude updating algorithm of strapdown inertial navigation system under highly dynamic environment[J]. Chinese Journal of Space Science, 2013, 33(1): 85-91. doi: 10.11728/cjss2013.01.085
Citation: Du Jiyong, Zhang Fengming, Li Jianwen, Huang Guorong, Dai Feng. Improved equivalent rotation vector based attitude updating algorithm of strapdown inertial navigation system under highly dynamic environment[J]. Chinese Journal of Space Science, 2013, 33(1): 85-91. doi: 10.11728/cjss2013.01.085

Improved equivalent rotation vector based attitude updating algorithm of strapdown inertial navigation system under highly dynamic environment

doi: 10.11728/cjss2013.01.085 cstr: 32142.14.cjss2013.01.085
  • Received Date: 2011-11-14
  • Rev Recd Date: 2012-09-17
  • Publish Date: 2013-01-15
  • The navigation algorithm of Strapdown Inertial Navigation System (SINS) under highly dynamic environment is studied, which is the key technology to improve the accuracy of SINS. The quaternion and equivalent rotation vector algorithms of resolving the attitude matrix were analyzed, and the equivalent rotation vector algorithm was developed in view of the application problem under highly dynamic environment. Aiming at adapting the algorithm to the application in highly dynamic flight environment, an improved equivalent rotation vector algorithm was proposed on the basis of coning motion environment, and the calculation error was derived. The performance was compared to one-sample and three-sample rotation vector algorithms. Simulation results indicate the effectiveness of the improved algorithm.

     

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