System Identification Using Impulse Response Including Initial States

Author:

YAMAGUCHI Isao1,KASAI Tokio1,IGAWA Hirotaka1,MITANI Shinji2,OHTANI Takashi2

Affiliation:

1. Japan Aerospace Exploration Agency, Airframes and Structures Group

2. Japan Aerospace Exploration Agency, Guidance and Control Group

Publisher

Japan Society of Mechanical Engineers

Reference9 articles.

1. (1) Juang, J.-N. and Pappa R.S., An Eigensystem Realization Algorithm (ERA) for Modal Parameter Identification and Model Reduction, Journal of Guidance, Control, and Dynamics, Vol. 8, No. 5(1985), pp. 620-627.

2. Experiments for Large Space Structures Identification

3. (3) Yamaguchi, I. et al., ETS-VI On-Orbit Identification Experiments (1st Report, Impulse Excitation), Transactions of the Japan Society of Mechanical Engineers, Series C,Vol. 62, No. 603(1996), pp. 4182-4189.

4. A Comparative Study of Prediction Error Method and Subspace Method Using ETS-VI On-Orbit System Identification Experimental Data

5. (5) Kasai, T. et al., A Preliminary Study of On-Orbit System Identification for ADEOS-II (2nd Report, System Identification Using Response Data during Wheel Unloading and Orbit Change), Transactions of the Japan Society of Mechanical Engineers, Series C, Vol. 69, No. 683(2003), pp. 1829-1836.

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