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http://dx.doi.org/10.5139/JKSAS.2020.48.8.631

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

Baek, Seung-Jae (School of Mechanical and Aerospace Eng. Gyeongsang National University)
Kang, Mun-Hye (Dept. of Aerospace and Software Eng. Gyeongsang National University)
Choi, Seong-Hwan (BrainsLab Co.,Ltd)
Kim, Byoung Soo (Dept. of Aerospace and Software Eng. Gyeongsang National University)
Moon, Yong Ho (Dept. of Aerospace and Software Eng. Gyeongsang National University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.48, no.8, 2020 , pp. 631-640 More about this Journal
Abstract
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.
Keywords
Flight Dynamic Model; Fidelity; Validation Test; Qualification Test Guide; Software;
Citations & Related Records
Times Cited By KSCI : 3  (Citation Analysis)
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