국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Flight Path Control for the Approach and Landing of the Quiet STOL Experimental Aircraft ASKA
저자	Flight Test Section
Keyword	Flight Test; Powered-Lift; Upper Surface Blowing; STOL; Flight Path Control; SCAS
URL	http://send.nal.go.jp/send/jpn/dlfile.php3/naltr01183?doctype=7&filetype=20&path0=naltr01183&path1=pdf&path2=naltr01183.pdf
보고서번호	NAL TR-1183
발행년도	1992.11
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	The Upper Blowing STOL experimental aircraft,ASKA,operates well on the backside of the power required curve,so flight path control is accomplished with the throttle lever(thrust)during landing approaches.To compensate for the sluggish flight path response caused by engine lag,the Flight Path Control(FPC)law puts in Stability and Control Augmentation System(SCAS).Flight tests were conducted to evaluate flight path and airspeed response characteristi