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쌍발 복합재 비행기의 속도, 고도 보정 및 상승성능에 관한 연구
황명신,박윤진,이정모,김칠영,은희봉 한국항공운항학회 1997 한국항공운항학회지 Vol.5 No.1
Airspeed and altimeter calibration of "win Mee was conducted by the flight test. We have adopted system to system method. Flight test data is corrected for instrumented error and position error, and the resultin data was satisfied. Climb Performance flight test also was conducted. But we could not have all data because of limited flight time. The resulted data was satisfied compare with calculated dab.
황명신 한국 항공대학교 항공산업기술연구소 1993 航空宇宙産業技術硏究所 硏究誌 Vol.3 No.-
The Instrumentation system is the most important aspect of a flight test program. It is the means by which the objective of a flight test, the production of accurate, useful data are achived. An instrumentation system consists of everything required to sence, condition, and record all parameters of interest. The task of a flight test engineer is to select-a-system that is adequte to obtain all needed data, but not complex, expensive, and heavy than the situation demands. In this paper, the primary factors that determine the design of an instrumentation system are discussed.