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http://dx.doi.org/10.12985/ksaa.2022.30.1.038

Flight Scenario Trajectory Design of Fixed Wing and Rotary Wing UAV for Integrated Navigation Performance Analysis  

Won, Daehan (한서대학교 항공시스템공학과)
Oh, Jeonghwan (한서대학교 항공시스템공학과)
Kang, Woosung (한서대학교 항공시스템공학과)
Eom, Songgeun (한서대학교 항공시스템공학과)
Lee, Dongjin (한서대학교 무인항공기학과)
Kim, Doyoon (한국항공우주연구원)
Han, Sanghyuck (한국항공우주연구원)
Publication Information
Journal of the Korean Society for Aviation and Aeronautics / v.30, no.1, 2022 , pp. 38-43 More about this Journal
Abstract
As the use of unmanned aerial vehicles increases, in order to expand the operability of the unmanned aerial vehicle, it is essential to develop an unmanned aerial vehicle traffic management system, and to establish the system, it is necessary to analyze the integrated navigation performance of the unmanned aerial vehicle to be operated. Integrated navigation performance is affected by various factors such as the type of unmanned aerial vehicle, flight environment, and guidance law algorithm. In addition, since a large amount of flight data is required to obtain high-reliability analysis results, efficient and consistent flight scenarios are required. In this paper, a flight scenario that satisfies the requirements for integrated navigation performance analysis of rotary and fixed-wing unmanned aerial vehicles was designed and verified through flight experiments.
Keywords
Flight Scenario; Integrated Navigation Performance Analysis; Trajectory Design; Unmanned Aerial Vehicle; Unmanned Aircraft System Traffic Management;
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  • Reference
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