국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Basic Desing of Flight Directer System for NAL STOL Research Aircraft
저자	Keiji TANAKA
Keyword
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm00558.pdf?id=NALTM0000558
보고서번호	NAL TM-558
발행년도	1986.12
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	A basic design concept of a flight director system for the NAL STOL Research Air-craft “ASUKA” is proposed and evaluated with the help of a CAD (Computer Aided Design) tool for control system synthesis. The flight director system designed for backside operations during the approach and landing phase of ASUKA has three commands presented by one integrated symbol : pitch command for speed control, flight path command for Flight Path Control lever manipulation, and bank command for lateral control. In determining the flight-director dynamics, closed loop analysis was conducted of pilot, aircraft, control systems, and navigational sites, as well as the flight director system itself. Dialogical communications with the CAD system enabled the quick and simple determination of the dynamics. Dynamics and constants of the flight director system confirmed by the present study form a basis for future design of flight director systems for USB type aircraft.