국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Control System Design of a Cable-Mounted Model used for Dynamic Wind Tunnel Testing
저자	Masaaki YANAGIHARA, Masahiko NAGAYASU, Shuichi SASA, Takashi Shimomura
Keyword	cable-mounted model; dynamic wind tunnel test; control system; root locus method
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01161.pdf?id=NALTR0001161
보고서번호	NAL TR-1161
발행년도	1992.6
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	The control system of a cable-mounted aircraft model used for dynamic wind tunnel testing was disigned using the root locus method.Computer simulations were initially performed to evaluate the designed control system,which was then applied to actual wind tunnel tests. Results confirmed the system′s suitability,although the control gains required slight tunig.In addition,wind tunnel tests were conducted using the control system to identify the aerodynamic model of the cable-mounted model.