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http://dx.doi.org/10.5302/J.ICROS.2008.14.12.1244

Analysis on Flight Test Results of Reconfiguration Flight Control System  

Min, Byoung-Mun (한국과학기술원 항공우주공학과)
Kim, Seong-Pil (한국항공우주연구원)
Kim, Bong-Ju (한국항공우주산업)
Kim, Eung-Tai (한국항공우주연구원)
Tahk, Min-Jea (한국과학기술원 항공우주공학과)
Publication Information
Journal of Institute of Control, Robotics and Systems / v.14, no.12, 2008 , pp. 1244-1252 More about this Journal
Abstract
This paper presents the analysis results obtained by the flight test of reconfiguration flight control system for an aircraft. The reconfiguration flight control system was designed by using control allocation scheme that automatically distributes the demanded control moments determined by control law to each actual control surface. In this paper, some control allocation algorithms for reconfiguration control of general aircraft with redundant control surfaces are summarized and their performance evaluation results through nonlinear simulation and Hardware-In-the-Loop-Simulation (HILS) test are shown. Also, Unmanned Aerial Vehicle (UAV) system adopted as a platform for the flight test of reconfiguration flight controller and the implementation procedure of reconfiguration flight controller into real-time UAV system were introduced. Finally, flight test results were analyzed.
Keywords
control allocation; flight test; HILS test; implementation procedure; nonlinear simulation; real-time UAV system; reconfiguration flight control system;
Citations & Related Records
Times Cited By KSCI : 3  (Citation Analysis)
연도 인용수 순위
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