| dc.contributor.author | Işık, Yasemin | |
| dc.date.accessioned | 2019-10-22T20:07:10Z | |
| dc.date.available | 2019-10-22T20:07:10Z | |
| dc.date.issued | 2010 | |
| dc.identifier.isbn | 9789604741854 | |
| dc.identifier.uri | https://hdl.handle.net/11421/22237 | |
| dc.description | University of Sfax | en_US |
| dc.description | 6th WSEAS International Conference on Dynamical Systems and Control, CONTROL '10 -- 3 May 2010 through 6 May 2010 -- Sousse -- 84086 | en_US |
| dc.description.abstract | Aircraft dynamics are in general nonlinear, time varying, and uncertain. A control system (classical control systems) designed for a flight condition, may not provide the desired stability and performance characteristics in case of deviation from the equilibrium point. There are numerous studies regarding flight control in the literature. One of them is fuzzy flight control system. In this study an aircraft pitch rate damping is evaluated by using a fuzzy PD controller. | en_US |
| dc.language.iso | eng | en_US |
| dc.rights | info:eu-repo/semantics/closedAccess | en_US |
| dc.subject | Aircraft | en_US |
| dc.subject | Flight Control | en_US |
| dc.subject | Fuzzy And Fuzzy Pd Control | en_US |
| dc.subject | Pitch Rate | en_US |
| dc.title | Pitch rate damping of an aircraft by a fuzzy PD controller | en_US |
| dc.type | conferenceObject | en_US |
| dc.relation.journal | 6th WSEAS International Conference on Dynamical Systems and Control, CONTROL '10 | en_US |
| dc.contributor.department | Anadolu Üniversitesi, Sivil Havacılık Yüksekokulu | en_US |
| dc.identifier.startpage | 118 | en_US |
| dc.identifier.endpage | 122 | en_US |
| dc.relation.publicationcategory | Konferans Öğesi - Uluslararası - Kurum Öğretim Elemanı | en_US] |
