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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| Date: | 2020 |
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| Author Affiliations: |
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| Keywords: | keywords |
| Main Authors: | , , , , , |
| Format: | Article |
| Language: | Ukrainian |
| Published: |
Інститут математики НАН України
2020
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| Online Access: | https://trim.imath.kiev.ua/index.php/trim/article/view/427 |
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| Journal Title: | Transactions of Institute of Mathematics of NAS of Ukraine |
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Transactions of Institute of Mathematics of NAS of Ukraine| Summary: | 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 ini- tial disturbances on qualitative characteristics of the system. In particular, influence of weight coefficients of the generalized quality criteria on the sta- bility factor and the transient process time of a closed system have been investigated.
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