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http://dx.doi.org/10.5139/JKSAS.2010.38.1.035

Reconfiguration Control Using LMI-based Constrained MPC  

Oh, Hyon-Dong (한국과학기술원 항공우주공학과 대학원)
Min, Byoung-Mun (한국과학기술원 항공우주공학과)
Kim, Tae-Hun (한국과학기술원 항공우주공학과)
Tahk, Min-Jea (한국과학기술원 항공우주공학과)
Lee, Jang-Ho (한국항공우주연구원)
Kim, Eung-Tai (한국항공우주연구원)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.38, no.1, 2010 , pp. 35-41 More about this Journal
Abstract
In developing modern aircraft, the reconfiguration control that can improve the safety and the survivability against the unexpected failure by partitioning control surfaces into several parts has been actively studied. This paper deals with the reconfiguration control using model predictive control method considering the saturation of control surfaces under the control surface failure. Linearized aircraft model at trim condition is used as the internal model of model predictive control. We propose the controller that performs optimization using LMI (linear matrix inequalities) based semi-definite programming in case that control surface saturation occurs, otherwise, uses analytic solution of the model predictive control. The performance of the proposed control method is evaluated by nonlinear simulation under the flight scenario of control surface failure.
Keywords
Reconfiguration Control; Model Predictive Control; Linear Matrix Inequalities;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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