06.1 - Flight Dynamics and Control (Control & Modelling)
DESIGN OF STABILITY AUGMENTATION SYSTEMS FOR A FLEXIBLE AIRCRAFT USING LQ OUTPUT-FEEDBACK CONTROL VIA LMI
R.L. Pereira, ITA, Brazil; P.J. González¹, F.J. Silvestre¹; ¹TU Berlin, Germany
This paper presents novel linear quadratic (LQ) output-feedback synthesis conditions for stability augmentationrnsystems in a flexible aircraft. The proposed conditions have been formulated using the linear matrix inequalitiesrn(LMIs) theory to provide two different approaches: centralized and decentralized LQ with output-feedbackrnframework.