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

• Дата: 2020
• Автори: Mazko, Відділ 04, Kusiy, S.I., Мазко, А.Г., Кусий, С.И., Мазко, О.Г., Кусій, С.І.
• Формат: Стаття
• Мова: Українська
• Опубліковано: Інститут математики НАН України 2020
• Онлайн доступ: https://trim.imath.kiev.ua/index.php/trim/article/view/427
• Назва журналу: 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...