국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Maximum-likelihood Estimation of the NAL Spaceplane Aerodynamic Model using Dynamic Wind Tunnel Tests
저자	Dynamic Wind Tunnel Test Group
Keyword	Cable mount; dynamic wind tunnel test; parameter identification; maximum likelihood method
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01307.pdf?id=NALTR0001307
보고서번호	NAL TR-1307
발행년도	1996.9
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	As a part of a study of the estimation of aircraft aerodynamic characteristics using dynamic wind tunnel tests,cable mount dynamic wind tunnel tests were executed from 1989.Maximum likelihood estimation algorithm is applied to the test data,and low speed aerodynamic parameters are estimated.The basic performance of the algorithm is evaluated by comparing it to other estimation algorithm.