Abstract
The final goal of this study is the development of the levitation stabilization control method of "Aero-Train" which is a high-speed high-efficiency train system levitated by wing-in-ground effect on the U-shaped guide way. Toward this goal, development of a small experimental prototype and stabilization control method along Z axis and about roll and pitch axes are described in this paper. The effectiveness of developed control method is confirmed through experimental results.
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