Development of Software for Fidelity Test of Flight Dynamic Model on Fixed Wing Aircraft

  • Baek, Seung-Jae; 
  • Kang, Mun-Hye; 
  • Choi, Seong-Hwan; 
  • Kim, Byoung Soo; 
  • Moon, Yong Ho
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초록

Currently, aircraft simulator has drawn a great attention because it has significant advantages of economic, temporal, and spatial costs compared with pilot training with real aircraft. Among the components of the aircraft simulator, flight dynamic model plays a key role in simulating the flight of an actual aircraft. Hence, it is important to verify the fidelity of flight dynamic model with an automated tool. In this paper, we develop a software to automatically verify the fidelity of the flight mechanics model for the efficient development of the aircraft simulator. After designing the software structure and GUI based on the requirements derived from the fidelity verification process, the software is implemented with C # language in Window-based environment. Experimental results on CTSW models show that the developed software is effective in terms of function, performance and user convenience.

키워드

Flight Dynamic Model; Fidelity; Validation Test; Qualification Test Guide; Software
제목
Development of Software for Fidelity Test of Flight Dynamic Model on Fixed Wing Aircraft
저자
Baek, Seung-Jae; Kang, Mun-Hye; Choi, Seong-Hwan; Kim, Byoung Soo; Moon, Yong Ho
DOI
10.5139/JKSAS.2020.48.8.631
발행일
2020-08
유형
Article
저널명
한국항공우주학회지
권
48
호
8
페이지
631 ~ 640