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

被引:0
|
作者
Baek, Seung-Jae [1 ]
Kang, Mun-Hye [3 ]
Choi, Seong-Hwan [2 ]
Kim, Byoung Soo [3 ]
Moon, Yong Ho [3 ]
机构
[1] Gyeongsang Natl Univ, Sch Mech & Aerosp Engn, Jinju Si, Gyeongsangnam D, South Korea
[2] BrainsLab Co Ltd, Beijing, Peoples R China
[3] Gyeongsang Natl Univ, Dept Aerosp & Software Engn, Jinju Si, Gyeongsangnam D, South Korea
关键词
Flight Dynamic Model; Fidelity; Validation Test; Qualification Test Guide; Software;
D O I
10.5139/JKSAS.2020.48.8.631
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
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.
引用
收藏
页码:631 / 640
页数:10
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