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https://hdl.handle.net/20.500.11851/2833
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DC Field | Value | Language |
---|---|---|
dc.contributor.author | Akyürek, Şeyma | - |
dc.contributor.author | Ozden, Gizem Sezin | - |
dc.contributor.author | Kürkcü, Burak | - |
dc.contributor.author | Kaynak, Ünver | - |
dc.contributor.author | Kasnakoğlu, Coşku | - |
dc.date.accessioned | 2019-12-25T14:03:41Z | - |
dc.date.available | 2019-12-25T14:03:41Z | - |
dc.date.issued | 2015 | |
dc.identifier.citation | Akyurek, S., Ozden, G. S., Kurkcu, B., Kaynak, U., and Kasnakoglu, C. (2015, November). Design of a flight stabilizer for fixed-wing aircrafts using H? loop shaping method. In 2015 9th International Conference on Electrical and Electronics Engineering (ELECO) (pp. 790-795). IEEE. | en_US |
dc.identifier.uri | https://hdl.handle.net/20.500.11851/2833 | - |
dc.identifier.uri | https://ieeexplore.ieee.org/abstract/document/7394579 | - |
dc.description.abstract | Autopilot systems for unmanned aerial vehicles (UAVs) and aircrafts provide flight missions without need of human input and make them more reliable and efficient. The first step of designing an autopilot is a stabilizer mode. Conventional autopilot systems have inner and outer loops. Stabilizer is the inner loop for an autopilot. In this paper designing an aircraft control system ensures good performance and robustness that allows control of roll, pitch and yaw angles will be declared. Aircraft dynamics are used to design the model of the control system in the MATLAB Simulink environment. Using loop shaping method to achieve stable and robust control system will be the strategy. Generated controllers to find the most effective one are embedded in the X-plane which is one of the realistic simulations. | en_US |
dc.language.iso | en | en_US |
dc.publisher | IEEE | en_US |
dc.rights | info:eu-repo/semantics/closedAccess | en_US |
dc.subject | UAV | en_US |
dc.subject | aircraft | en_US |
dc.subject | drone | en_US |
dc.subject | stabilizer | en_US |
dc.subject | autopilot | en_US |
dc.subject | control | en_US |
dc.subject | loop shaping | en_US |
dc.subject | H-infinity | en_US |
dc.title | Design of a Flight Stabilizer for Fixed-Wing Aircrafts Using H-Infinity Loop Shaping Method | en_US |
dc.type | Conference Object | en_US |
dc.department | Faculties, Faculty of Engineering, Department of Electrical and Electronics Engineering | en_US |
dc.department | Fakülteler, Mühendislik Fakültesi, Elektrik ve Elektronik Mühendisliği Bölümü | tr_TR |
dc.identifier.startpage | 790 | |
dc.identifier.endpage | 795 | |
dc.authorid | 0000-0002-9928-727X | - |
dc.identifier.wos | WOS:000380410800143 | en_US |
dc.identifier.scopus | 2-s2.0-84963828234 | en_US |
dc.institutionauthor | Kasnakoğlu, Coşku | - |
dc.identifier.doi | 10.1109/ELECO.2015.7394579 | - |
dc.relation.publicationcategory | Konferans Öğesi - Uluslararası - Kurum Öğretim Elemanı | en_US |
item.openairetype | Conference Object | - |
item.languageiso639-1 | en | - |
item.grantfulltext | none | - |
item.fulltext | No Fulltext | - |
item.openairecristype | http://purl.org/coar/resource_type/c_18cf | - |
item.cerifentitytype | Publications | - |
crisitem.author.dept | 02.7. Department of Mechanical Engineering | - |
crisitem.author.dept | 02.5. Department of Electrical and Electronics Engineering | - |
Appears in Collections: | Elektrik ve Elektronik Mühendisliği Bölümü / Department of Electrical & Electronics Engineering Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collection |
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