국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	H∞Control for Aircraft Take off in Windshear
저자	Lixin Wang
Keyword	Simulation research; Flight control; Robust control; H∞ control; Take off; Windshear
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr1273t.pdf?id=NALTR0001273T
보고서번호	NAL TR-1273T
발행년도	1995.6
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	Results are presented from an application of the most recently developed H∞ control design methodology to a stabilizing controller for an aircradt duting take off in a windshear.The emphasis is on the formulating of H∞ optimal control synthesis porblem in the state space.Simulation rests are performed in a six digree-of-freedom flight sumulator for different windshear histories and different take off conditions,these results demonstrate that the controlled aircraft could take