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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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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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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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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UAV-based evaluation of morphological changes induced by extreme rainfall events in meandering rivers
PLOS ONE, Vol. 15, No. 11, Ocak 2020, ISSN: 1932-6203
AKAY SEMİH SAMİ,ÖZCAN ORKAN,BALIK ŞANLI FUSUN,GÖRÜM TOLGA,ŞEN ÖMER LÜTFİ,BAYRAM BÜLENT
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Conceptual Design of a Nonconstant Swept Flying Wing Unmanned Combat Aerial Vehicle
American Institute of Aeronautics and Astronautics (AIAA) Journal of Aircraft, Vol. 60, No. 6, Kasım 2023, ISSN: 0021-8669
ALEİSA HASSAN, KONTİS KONSTANTİNOS, PİRLEPELİ BERKAY, NİKBAY MELİKE
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Free vibration analysis of composite aircraft wings modeled as thin-walled beams with NACA airfoil sections
Thin-Walled Structures, Vol. 139, Haziran 2019, s. 362-371, ISSN: 0263-8231
EKEN SEHER
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Exergetic Sustainability Indicators as a Tool in Commercial Aircraft A Case Study for a Turbofan Engine
International Journal of Green Energy, Vol. 12, No. 1, Eylül 2015, s. 28-40, ISSN: 1543-5075
AYDIN HAKAN,TURAN ÖNDER,KARAKOÇ TAHİR HİKMET,MİDİLLİ ADNAN
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Approximate Analytical Solutions Of Nonlinear Flutter Of Aircraft Wings
IFASD 2011, 15th International Forum on Aeroelasticity and Structural Dynamics, Paris/FRANSA, 26 Haziran 2011
EKEN SEHER, KERKİ TİLBE, KAYA METİN ORHAN
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Active Vibration Control Applications for Adaptive Aircraft Wings Modelled as Thin-Walled Composite Beams
AIAA-57th Structures, Structural Dynamics, and Materials Conference, San Diego-California/AMERİKA BİRLEŞİK DEVLETLERİ, 4 Ocak 2016
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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Aeroleastic analysis of a thin-walled composite aircraft wing with an external store subjected to a follower force
ASME-IMECE2014, International Mechanical Engineering Congress & Exposition, Montreal/KANADA, 14 Kasım 2014
KAÇAR AKSONGUR ALEV, EKEN SEHER, KAYA METİN ORHAN
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Multi-Fidelity and Multi-Disciplinary Design Optimization of A Low-Boom Supersonic Transport Aircraft
AIAA Scitech 2023, 23 Ocak 2023
NİKBAY MELİKE, KILIÇ DİLAN, ÇAKMAK ENES, TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROĞLU YUSUF
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Exergo sustainability indicators of a turboprop aircraft for the phases of a flight
Energy, Vol. 58, Eylül 2013, s. 550-560, ISSN: 03605442
AYDIN HAKAN,TURAN ÖNDER,KARAKOÇ TAHİR HİKMET,MİDİLLİ ADNAN
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