국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Position Error Determination for the Speedometer and Altimeter of the NAL QSTOL Experimental Aircraft ″ASKA″
저자	STOL RESEARCH AIRCRAFT GROUP FLIGHT TEST TEAM
Keyword	Position error; Speedometer; Altimeter; STOL aircraft; Flight test
URL	http://send.nal.go.jp/send/jpn/dlfile.php3/naltr01144?doctype=7&filetype=20&path0=naltr01144&path1=pdf&path2=naltr01144.pdf
보고서번호	NAL TR-1144
발행년도	1992.3
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	The position error is reported for three different pitot-static systems used in the National Aerospace Laboratory (NAL) Quiet Short Take-Off and Landing (QSTOL) experimental aircraft ″ASKA″,being determined using only the static pressure error,and assuming that the total pressure error is negligible.It was found that a continuous reference altitude and a correction for pressure prop.In addition the position error in high angle of attack cases was discussed.The resultant position error correction was used for various analyses of flight test data.Furthermore,it was incorporated into the Digital Air Data Computer to indicate the calibrated airspeed and altitude to the pilots.