Damping of the limited perturbations in the system of the aircraft control when landing

• Date: 2020
• Author Affiliations: О.Г. Мазко — Iнститут математики НАН України; С.І. Кусій — Iнститут математики НАН України
• Keywords: keywords
• Main Authors: Mazko, Відділ 04, Kusiy, S.I., Мазко, А.Г., Кусий, С.И., Мазко, О.Г., Кусій, С.І.
• Format: Article
• Language: Ukrainian
• Published: Інститут математики НАН України 2020
• Online Access: https://trim.imath.kiev.ua/index.php/trim/article/view/427
• Journal Title: Transactions of Institute of Mathematics of NAS of Ukraine

A linear model of the aircraft control system in the landing mode is consid- ered in the presence of limited external perturbations. The method of lin- ear matrix inequalities is implemented in the generalized H∞-optimization problem in order to evaluate and reduce the influence of external and i...