Shuichi Sasa scite author profile

This paper describes the application of system identification method in the time domain using accelerometer outputs that are typical measurement devices for satellite and space strucures. ERA (Eigensystem Realization Algorithm) modified by the iterative least square method is applied in the analysis. Results of numerical simulations for ETS-VI which will be launched by H-II rocket in 1994 show the validity of the method.

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Control and Guidance of Low Altitude Stationary Flight Test Vehicle

Kohno¹,

Sasa²

2005

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Shuichi Sasa

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System Identification for Large Space Structures Using Accelerometer Outputs in the Time Domain

Control and Guidance of Low Altitude Stationary Flight Test Vehicle

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