地面効果翼機のピッチ角制御に関する研究

松本 大地; 長 保浩; 内門 茂

doi:10.11511/jacc.53.0.9.0

THE 53RD JAPAN JOINT AUTOMATIC CONTROL CONFERENCE

Session ID : 110

DOI https://doi.org/10.11511/jacc.53.0.9.0

Conference information

Host: The Japan Society of Mechanical Engineers, The Society of Instrument and Control Engineers, The Institute of Systems, Control and Information Engineers, The Society of Chemical Engineers, Japan, The Japan Society for Precision Engineering, The Japan Society for Aeronautical and Space Sciences

Co-host: Technically Cosponsored by 50 Societies and Institutes

Applications of Control Engineering 1

Study of Pitch Angle Control for WIG

*Daichi MATSUMOTO, Yasuhiro OSA, Shigeru UCHIKADO

Author information

Keywords: Wing in Ground Effect, Pitch Angle Control, PI Control

CONFERENCE PROCEEDINGS FREE ACCESS

Details

Abstract

Wing in Ground Effect (WIG) is a transport vehicle which has a possibility of filling the gap of speed and payload between ship and aircraft on marine transportation. But reports about flight control system for WIG are few. So in this study, the linear motion of WIG under the ground effect is shown, and a pitch angle control system is designed as an attempt to obtain the good maneuverability and so on.

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