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Development of Transient Simulation Program for Smart UAV Propulsion System  

Lee, Chang-Ho (한국항공우주연구원 스마트무인기 사업단)
Ki, Ja-Young ((주)이지가스터빈)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.15, no.6, 2011 , pp. 63-69 More about this Journal
Abstract
The Smart UAV must have the control characteristics of propulsion system necessary for both rotary aircraft and fixed wing aircraft though it equips turbo-shaft engine. To develop an electronic engine controller in the future, it is necessary to accumulate the experience of engine operation and data of tilt rotor aircraft. For this purpose, the computer programs which predict engine performance in the steady state and transient state can be utilized for the supplementation of flight test data. In this work, we developed a dynamic analysis program using engine performance data gathered during the flight tests. In addition the accuracy of the program was verified through comparison with flight test data and the results of steady-state performance analysis program.
Keywords
Smart UAV; PW206C Engine; Transient Performance Analysis; Flight Test Performance;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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