국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Flight simulation model for Automatic Landing Flight Experiment (Part I : Free Flight and Ground Run Basic Model)
저자	NAL/NASDA ALFLEX Group
Keyword	HOPE; ALFLEX; Simulation Program
URL	http://send.nal.go.jp/send/jpn/dlfile.php3/naltr01252?doctype=7&filetype=20&path0=naltr01252&path1=pdf&path2=naltr01252.pdf
보고서번호	NAL TR-1252
발행년도	1994.10
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	The National Aerospace Laboratory (NAL) and the National Aerospace Development Agency of Japan (NASDA) have been cooperating in the research and technology development of a future unmanned re-entry space vehicle named HOPE,aance and control system.The nominal glide path is 30 degrees and the approach velocity is 80m/s.This paper discusses an ALFLEX numerical simulation model from the helicopter release to the ground run stop and the preliminary results obtained from its simulation.This numerical simulation program has been a basic tool for the ALFLEX guidance and control system design,and it appropriately presents principal characteristics of the planned re-entry space vehice for its landing/approach phase.