Zobrazeno 1 - 10
of 26
pro vyhledávání: '"control actuation system"'
Publikováno v:
Bulletin of the Polish Academy of Sciences: Technical Sciences, Vol 72, Iss 2 (2023)
The aim of the study described herein was to design, construct and test a demonstrator of a system to control the direction of the resultant thrust vector of a rocket motor to be used in short range anti-tank missiles with a mass of up to 15 kg. The
Externí odkaz:
https://doaj.org/article/dce09bcd928c466c9aad2e30b3775a58
Autor:
Ercan, Hamdi, Akın, Mustafa
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2022, Vol. 94, Issue 10, pp. 1671-1683.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-11-2021-0326
Autor:
Bülent Özkan
Publikováno v:
Uludağ University Journal of The Faculty of Engineering, Vol 27, Iss 3, Pp 1163-1176 (2022)
In this study, the design of an electro-mechanical fin loading system which is utilized to simulate the effects of the aerodynamic moment occurring in an atmospheric flight on a missile system is dealt with. In this extent, the dynamic modeling of th
Externí odkaz:
https://doaj.org/article/c564102c72bf4058b76a2a9e991bfca0
Publikováno v:
Applied Sciences, Vol 14, Iss 3, p 1206 (2024)
Many different types of aircraft designs have flight control systems (FCS) powered by hydraulic systems. With respect to the torques, moments, surface areas, and opposing forces to be acted upon, components introduce faults into the hydraulic system
Externí odkaz:
https://doaj.org/article/30715f2b611f444bb5e3867766a93b6e
Akademický článek
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Publikováno v:
Energies, Vol 15, Iss 1, p 356 (2022)
This article approaches the issue of the optimal control of a hypothetical anti-tank guided missile (ATGM) with an innovative rocket engine thrust vectorization system. This is a highly non-linear dynamic system; therefore, the linearization of such
Externí odkaz:
https://doaj.org/article/5e4e97e87e9b41bf9e709df30a1584a3
Akademický článek
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Autor:
Bülent ÖZKAN
In this study, the design of an electro-mechanical fin loading system which is utilized to simulate the effects of the aerodynamic moment occurring in an atmospheric flight on a missile system is dealt with. In this extent, the dynamic modeling of th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::671ba1bc2a8cea2044f89400c7b27994
http://hdl.handle.net/11452/31614
http://hdl.handle.net/11452/31614
Autor:
ÖZKAN, Bülent
Publikováno v:
Volume: 27, Issue: 3 1163-1176
Uludağ University Journal of The Faculty of Engineering
Uludağ Üniversitesi Mühendislik Fakültesi Dergisi
Uludağ University Journal of The Faculty of Engineering
Uludağ Üniversitesi Mühendislik Fakültesi Dergisi
Bu çalışmada, atmosfer içerisinde uçan bir füzeye etkiyen aerodinamik moment etkisinin yerde benzetimini yapmak amacıyla tasarlanan elektromekanik eyletimli bir kanat yükleme cihazının tasarımı ele alınmaktadır. Bu kapsamda, göz önün
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=tubitakulakb::723a41c8ab5ba83d40f9336f02208c11
https://dergipark.org.tr/tr/pub/uumfd/issue/73731/1121360
https://dergipark.org.tr/tr/pub/uumfd/issue/73731/1121360
Akademický článek
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