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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2009, Vol. 30 ›› Issue (6): 1077-1083.

• Avionics and Autocontrol • Previous Articles     Next Articles

Realization of Parameter Identification of Inertial Platform Under Linear Vibration

Tang Jianghe1, Fu Zhenxian1, Yu Zhenyu2, Deng Zhenglong1   

  1. 1.School of Astronautics, Harbin Institute of Technology 2.Beijing Aerospace Control Device Institute
  • Received:2008-04-07 Revised:2008-07-24 Online:2009-06-25 Published:2009-06-25
  • Contact: Tang Jianghe

Abstract: This article studies the parameter identification for gyros on inertial platforms with buffered connection under linear vibration. Since the original drift model of inertial platform is unsuitable for parameter identification under such conditions, an average model is presented, and a comparison between the average model and the static model demonstrates the essential influence of linear vibration on parameter identification. Meanwhile, since the limitation of parameter redundancy exists in the average model, a new identification method is proposed which is based on two sets of data obtained from linear vibration tests with different vibration amplitudes. The new method not only ensures the convergence of high order gyro parameters for estimation, which is difficult under static conditions, but also overcomes the limitation of parameter redundancy of the average model.

Key words: linear vibration, inertial platform, gyro, identification, parameter redundancy

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