A Method for Identifying Error Coefficients of Inertial Navigation Platform in Centrifuge Test
Received:October 21, 2017  Revised:January 15, 2018
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DOI:10.7643/ issn.1672-9242.2018.01.001
KeyWord:inertial navigation platform  centrifuge test  identification of error coefficients  Fourier analysis
     
AuthorInstitution
XU Yong-fei College of Aerospace Science and Engineering, National University of Defense Technology, Changsha , China
ZHANG Shi-feng College of Aerospace Science and Engineering, National University of Defense Technology, Changsha , China
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Abstract:
      In allusion to identification of error coefficients for inertial navigation platform in centrifuge test, a method based on Fourier analysis was proposed. Firstly, output equation of gyro and accelerometer in centrifuge test was derived according to the error model for inertial device. The output was composed of different order harmonics. Then, the amplitude of each order harmonic was obtained by Fourier analysis. Finally, the error coefficients were obtained based on the relationship between harmonic amplitude expressions and error coefficients. The simulation results show that the proposed method is effective.
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