국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Navigation, Guidance, and Control Law and Planning of Flight Experiment for Scaled Supersonic Experimental Airplane (First Report)
저자	Hirokazu Suzuki
Keyword	Guidance; Control; SST; Flight Experiment
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr0001377.pdf?id=NALTR0001377
보고서번호	NAL TR-1377
발행년도	1999.01
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	As part of international joint technology development efforts for second-generation supersonic transport, two types of scaled supersonic experimental airplanes, un-powered and jet-powered ones, are under development at the National Aerospace Laboratory (NAL). The results of design of the navigation, guidance, and control law for the un-powered experimental airplane launched by a rocket booster are presented in this paper. The flight capability is assessed based on flight simulations with the designed control system. It is verified that the designed control system has the ability to perform the flight plan within first-order accuracy for flight conditions. A flight plan of higher-order accuracy is also proposed based on these results.