Design and Analysis of a High Power Density Brushless DC Motor for a Multi-Rotor Unmanned Aircraft
13th International Conference on Electrical and Electronics Engineering (ELECO 2021), Bursa/TÜRKİYE, 25 Kasım 2021
OZER KEVSER, YILMAZ MURAT
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Switching Control Architecture with Parametric Optimization for Aircraft Upset Recovery
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, Vol. 42, No. 9, Eylül 2019, s. 2055-2068, ISSN: 0731-5090
YILDIZ ANIL,AKÇAL MEHMET UĞUR,HOŞTAŞ BATUHAN,ÜRE NAZIM KEMAL
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Rate envelope based time efficient strategy for upset recovery of a fighter aircraft
2018 IEEE Aerospace Conference, 3 Mart 2018
AKÇAL MEHMET UĞUR,HOŞTAŞ BATUHAN,ÜRE NAZIM KEMAL
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Finite State Automata Based Approach to Autonomous Stall and Upset Recovery for Agile Aircraft
2018 AIAA Guidance, Navigation, and Control Conference, 8 Ocak 2018
YILDIZ ANIL,AKÇAL MEHMET UĞUR,HOŞTAŞ BATUHAN,ÜRE NAZIM KEMAL,İNALHAN GÖKHAN
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Recoverability Envelope Analysis of Nonlinear Control Laws for Agile Maneuvering Aircraft
2018 AIAA Guidance, Navigation, and Control Conference, 8 Ocak 2018
AKÇAL MEHMET UĞUR,HOŞTAŞ BATUHAN,ÜRE NAZIM KEMAL,İNALHAN GÖKHAN
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Optimization of the PD coefficient in a flight simulator control via genetic algorithms
Aircraft Engineering and Aerospace Technology, Vol. 74, No. 2, Nisan 2002, s. 147-153, ISSN: 0002-2667
YURT SAİT,OZKOL İBRAHİM,KAYA METİN ORHAN,HACIZADE CENGİZ
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Vibrational genetic algorithm as a new concept in airfoil design
Aircraft Engineering and Aerospace Technology, Vol. 74, No. 3, Haziran 2002, s. 228-236, ISSN: 0002-2667
HACIOĞLU ABDURRAHMAN,OZKOL İBRAHİM
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The stability dependence on the different pressure gradients in a channel flow
Aircraft Engineering and Aerospace Technology, Vol. 75, No. 5, Ekim 2003, s. 485-490, ISSN: 0002-2667
SÖYLEMEZ HARUN TAYFUN,OZKOL İBRAHİM
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Error analysis and motion determination of a flight simulator
Aircraft Engineering and Aerospace Technology, Vol. 76, No. 2, Nisan 2004, s. 185-192, ISSN: 0002-2667
YURT SAİT,OZKOL İBRAHİM,HACIZADE CENGİZ
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Evaluation of critical parameters in the design of a trainer aircraft landing gear
2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE), 22 Temmuz 2017
ÇETİNKAYA BURHAN,OZKOL İBRAHİM
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The effects of the use of single task-oriented maintenance concept and more accurate letter check alternatives on the reduction of scheduled maintenance downtime of aircraft
2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE), 22 Temmuz 2017
SENTURK CANER,OZKOL İBRAHİM
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Sugeno and Mamdani based Fuzzy Inference Approaches for Aircraft Pitch Control
International Conference on Mathematics and Mathematics Education (ICMME), URFA/TÜRKİYE, 11 Mayıs 2017
ÖZTÜRK MUHAMMET,BAYEZİT İSMAİL,OKUDAN MEHMET EMİN,OZKOL İBRAHİM
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Implementation of Propulsion System Integration Losses to a Supersonic Military Aircraft Conceptual Design
AIAA Propulsion and Energy 2021 Forum, Virtual/AMERİKA BİRLEŞİK DEVLETLERİ, 9 Ağustos 2021
KARASELVİ EMRE, NİKBAY MELİKE
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Multifidelity Sonic Boom Minimization of A Supersonic Aircraft by Parametric Wing Shape Design
AIAA Scitech Forum, Tennessee (Virtual)/AMERİKA BİRLEŞİK DEVLETLERİ, 11 Ocak 2021
YUSUF DEMİROĞLU, YILDIZ ŞIHMEHMET, NİKBAY MELİKE
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Free vibration analysis of a rotating double tapered beam with flexible root via differential quadrature method
Aircraft Engineering and Aerospace Technology, Vol. 93, Ocak 2021, ISSN: 1748-8842
OZKOL İBRAHİM, YAVUZ MUSTAFA TOLGA
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Comparison of modified Karnik-Mendel algorithm-based interval type-2 ANFIS and type-1 ANFIS
Aircraft Engineering and Aerospace Technology, Vol. 93, Ocak 2021, ISSN: 1748-8842
OZKOL İBRAHİM, ÖZTÜRK MUHAMMET
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Sonic boom mitigation via shape optimization using an adjoint method and application to a supersonic fighter aircraft
European Journal of Computational Mechanics, Vol. 17, No. 1, Ocak 2008, s. 217-243, ISSN: 1779-7179
MAUTE KURT, FARHAT CHARBEL, ARGROW BRİAN, NİKBAY MELİKE
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Electrical System Design for Very Light Aircraft
ISUDEF 2021 (International Symposium on Unmanned Systems and the Defense Industry) Program, Washington/AMERİKA BİRLEŞİK DEVLETLERİ, 25 Ekim 2021
ALUÇ MERVE, KÖMÜRGÖZ KIRIŞ GÜVEN
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Atomistic simulation of micro scale adiabatic piston problem
Aircraft Engineering and Aerospace Technology, Vol. 81, No. 6, Ocak 2009, s. 499-507, ISSN: 0002-2667
SENGİL NEVSAN, EDİS FİRAT OGUZ
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Micro scale synthetic jet actuator flow simulation with characteristic based split method
Aircraft Engineering and Aerospace Technology, Vol. 81, No. 3, Ocak 2009, s. 239-246, ISSN: 0002-2667
CELİK BAYRAM, EDİS FİRAT OGUZ
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