| DC Field | Value | Language |
|---|
| dc.contributor.author | Amirzhanova, Z. B. | - |
| dc.contributor.author | Mashtaeva, A. A. | - |
| dc.contributor.author | Satybaldina, D. K. | - |
| dc.date.accessioned | 2019-11-27T08:45:42Z | - |
| dc.date.available | 2019-11-27T08:45:42Z | - |
| dc.date.issued | 2019 | - |
| dc.identifier.citation | Amirzhanova, Z. B. Development of a robust aircraft control system in conditions of disturbances / Amirzhanova Z. B., Mashtaeva A. A., Satybaldina D. K. // Информационные технологии и системы 2019 (ИТС 2019) = Information Teсhnologies and Systems 2019 (ITS 2019) : материалы международной научной конференции, Минск, 30 октября 2019 г. / Белорусский государственный университет информатики и радиоэлектроники; редкол. : Л. Ю. Шилин [и др.]. – Минск, 2019. – С. 30 – 31. | ru_RU |
| dc.identifier.uri | https://libeldoc.bsuir.by/handle/123456789/37528 | - |
| dc.description.abstract | In this paper a mathematical model of the dynamics of an airplane in a vertical plane is developed. The features
of the robust structural synthesis procedure as applied to the system of the type under study are presented. The
optimization problem for the system under study was solved using the mixed sensitivity method. The modern
approach to solving the problem of robust structural optimization is based on the formation of the desired frequency
characteristics of the system by expanding the object by introducing weighted transfer functions. | ru_RU |
| dc.language.iso | ru | ru_RU |
| dc.publisher | БГУИР | ru_RU |
| dc.subject | материалы конференций | ru_RU |
| dc.subject | mathematical description | ru_RU |
| dc.subject | introducing weighted transfer functions | ru_RU |
| dc.title | Development of a robust aircraft control system in conditions of disturbances | ru_RU |
| dc.type | Статья | ru_RU |
| Appears in Collections: | ИТС 2019
|
