Damping of the limited perturbations in the system of the aircraft control when landing
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...
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| Datum: | 2020 |
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| Hauptverfasser: | , , , , , |
| Format: | Artikel |
| Sprache: | Ukrainisch |
| Veröffentlicht: |
Інститут математики НАН України
2020
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| Online Zugang: | https://trim.imath.kiev.ua/index.php/trim/article/view/427 |
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| Назва журналу: | Transactions of Institute of Mathematics of NAS of Ukraine |
| Завантажити файл: |  |