Effects of Various Baffle Designs on Center Of Gravity Deviation in a Training Aircraft Wing Fuel Tank Using 1D Simulations
Proceedings of the ASME 2023 International Mechanical Engineering Congress and Exposition (IMECE2023), New Orleans/AMERİKA BİRLEŞİK DEVLETLERİ, 29 Ekim 2023
KARAHAN KEREM, ÇADIRCI SERTAÇ
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Vibration response analysis of an aircraft structure in terms of crashworthiness by using differential transformation method
Gazi University Journal of Science, Vol. 37, Aralık 2024, ISSN: 2147-1762
SOYSAL AYSUN,ÖZKOL İBRAHİM,UZAL EROL
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Design of a large-scale model for wind tunnel test of a multiadaptive flap concept
CHINESE JOURNAL OF AERONAUTICS, Vol. 37, No. 2, Şubat 2024, s. 58-80, ISSN: 1000-9361
SİCİM MÜRÜVET SİNEM,ROSARİO PECORA,KAYA METİN ORHAN
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Advanced Autopilot Design with Extremum-Seeking Control for Aircraft Control
Open Engineering, Vol. 14, No. 1, Ocak 2024, s. 1-38, ISSN: 2391-5439
BARAN HACİ,BAYEZİT İSMAİL
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Exploration of Optimal Propulsion System Airframe Integration Design Concepts for a Low Boom Supersonic Aircraft
AIAA Aviation 2021 FORUM, 2 Ağustos 2021
IMRAK RUMED, KARASELVİ EMRE, TUTKUN BÜLENT, NİKBAY MELİKE
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Aircraft Detection in Very High Resolution Satellite Images using YOLO-based Deep Learning Methods
4th Intercontinental Geoinformation Days, TABRİZ/İRAN, 20 Haziran 2022, s. 270-273
YABAN BERKAY, ALGANCI UĞUR, SERTEL ELİF
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Decentralized learning-based planning for multiagent missions in the presence of actuator failures
2013 International Conference on Unmanned Aircraft Systems (ICUAS), 28 Mayıs 2013
ÜRE NAZIM KEMAL,CHOWDHARY GİRİSH,CHEN YU FAN,CUTLER MARK,HOW JONATHAN P,VİAN JOHN
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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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Localization and tracking of RF emitting targets with multiple unmanned aerial vehicles in large scale environments with uncertain transmitter power
2017 International Conference on Unmanned Aircraft Systems (ICUAS), 13 Haziran 2017
HASANZADE MEHMET,HEREKOGLU ÖMER,ÜRE NAZIM KEMAL,KOYUNCU EMRE,YENİÇERİ RAMAZAN,İNALHAN GÖKHAN
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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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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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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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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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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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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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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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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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