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Assessment of Flight Control Performance based on the Ground Test Results of Smart UAV  

Kang, Young-Shin (스마트무인기 사업단 무인체계팀)
Park, Bum-Jin (스마트무인기 사업단 무인체계팀)
Yoo, Chang-Sun (스마트무인기 사업단 무인체계팀)
Kim, Yu-Shin (스마트무인기 사업단 무인체계팀)
Koo, Sam-Ok (스마트무인기 사업단 무인체계팀)
Publication Information
Aerospace Engineering and Technology / v.9, no.1, 2010 , pp. 1-8 More about this Journal
Abstract
The tilt-rotor Smart UAV(Unmanned Air Vehicle) has been developed by KARI(Korea Aerospace Research Institute) for civil purposes. In order to prove the reliabilities of total system of Smart UAV, the series of ground tests were performed including system interface test, aircraft HILS(Hardware In the Loop Simulation) Test, ground power test, 4-DOF (Degrees of Freedom)rig test, and tethered hover test. Many unexpected problems occurred at each ground test. With clearing these problems, the total Smart UAV systems were matured and the airworthiness was proven enough. After complete of additional ground test proposed by FRRB(Flight Readiness Review Board), the first flight test will be performed in this year. This paper presents the procedures and the analysis results of the ground tests for the tilt-rotor Smart UAV.
Keywords
tiltrotor; ground test; test result; flight control; Smart UAV;
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