국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Position and Attitude Control of a Spacecraft by Sliding Mode Control
저자	Fuyuto Terui
Keyword	nonlinear control; attitude control; position control; spacecraft; sliding mode control
URL	http://send.nal.go.jp/send/jpn/dlfile.php3/naltr0001330.pdf?doctype=7&filetype=20&path0=naltr0001330.pdf&path1=&path2=
보고서번호	NAL TR-1330
발행년도	1997.7
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	and translational motion(six degrees of freedom motion)is a nonlinear equation.This paper applies sliding mode control that can handle a nonlinear system to the six degree of freedom control for such a vehicle.Its feasibility is investigated through a numerical simulation of proximity flight around a tumbling target object.