Please use this identifier to cite or link to this item:
https://er.nau.edu.ua/handle/NAU/28252Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Komnatska, M. M. | - |
| dc.date.accessioned | 2017-05-25T11:28:38Z | - |
| dc.date.available | 2017-05-25T11:28:38Z | - |
| dc.date.issued | 2015 | - |
| dc.identifier.issn | 1990-5548 | - |
| dc.identifier.uri | http://er.nau.edu.ua/handle/NAU/28252 | - |
| dc.description.abstract | The problem of optimal state feedback controller design in terms of quadratic performance index is considered. The problem is formulated in the form of linear matrix inequalities (LMIs). The obtained solution guarantees stabilization of the aircraft during flight mission. During flight envelope the aircraft is subjected to the external stochastic disturbances. The efficiency of the proposed approach is illustrated by a case study of airplane longitudinal motion. | uk_UA |
| dc.language.iso | en | uk_UA |
| dc.publisher | Kyiv, “Osvita Ukrainy” | uk_UA |
| dc.subject | aircraft motion control | uk_UA |
| dc.title | OPTIMAL GUARANTEED COST CONTROL OF AIRCRAFT MOTION | uk_UA |
| dc.type | Article | uk_UA |
| Appears in Collections: | Наукові статті кафедри аерокосмічних систем управління | |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| Komnatska_EACS 2_2015___.pdf | Статья | 217.51 kB | Adobe PDF | View/Open |
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