TOPOLOGY OPTIMIZATION AND STRUCTURAL ANALYSIS AN AIRCRAFT WING
10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara/TÜRKİYE, 18 Eylül 2019
İNCİ HARUN, ÇAMUR ZELİHA, EKEN SEHER
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Aeroelastic instability of aircraft wings modeled as thin-walled composite beams
7th Ankara International Aerospace Conference, Ankara/TÜRKİYE, 11 Eylül 2013
EKEN SEHER, KAYA METİN ORHAN
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Aircraft Icing Detection Identification and Reconfigurable control Kalman Filtering and Neural Networks Approaches
Saarbrücken/ALMANYA, 2011, Lambert Academic Publishing
HAJİYEV CHİNGİZ, AYKAN RAHMİ, CALİSKAN FİKRET
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Multi-Fidelity Low-Rank Approximations for Uncertainty Quantification of a Supersonic Aircraft Design
Algorithms, Temmuz 2022, ISSN: 1999-4893
YILDIZ ŞIHMEHMET, PEHLİVAN SOLAK HAYRİYE, NİKBAY MELİKE
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Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction
Journal of Aircraft, Aralık 2022, ISSN: 1533-3868
TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROĞLU YUSUF, NİKBAY MELİKE
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Aircraft detection in very high-resolution satellite images using YOLO-based deep learning methods
4th Intercontinental Geoinformation Days, 20 Haziran 2022
YABAN BERKAY, ALGANCI UĞUR, SERTEL ELİF
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Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design
AIAA Scitech 2021 Forum, 11 Ocak 2021
DEMİROĞLU YUSUF, YILDIZ ŞIHMEHMET, NİKBAY MELİKE
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Aeroelastic Analysis of a Tapered Aircraft Wing
4th Ankara International Aerospace Conference, Ankara/TÜRKİYE, 10 Eylül 2007
EKEN SEHER, ÖZDEMİR ÖZGE, KAYA METİN ORHAN
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Autonomous Execution of Aircraft Supermaneuvers with Switching Nonlinear Backstepping Control
2018 AIAA Guidance, Navigation, and Control Conference, 8 Ocak 2018
MOGHADAM MAJİD,ÜRE NAZIM KEMAL,İNALHAN GÖKHAN
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Aircraft sensor fault diagnosis based on Kalman filter innovation sequence
IEEE Conference on Decision and Control, 16 Aralık 1998
ÇALIŞKAN FİKRET,HACIZADE CENGİZ
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Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin Walled Composite Beams
Applied Mechanics and Materials, Ekim 2015
KAAN YILDIZ,SEHER EKEN,KAYA METİN ORHAN
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Vibration Analysis of a Hingeless helicopter blade in hover Part I
Aircraft Engineering and Aerospace Technology: An International Journal, 2007
ÖZGE ÖZDEMİR ÖZGÜMÜŞ,KAYA METİN ORHAN
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Free Vibration Analysis of Rotating Timoshenko Beam by Differential Transform Metho
Aircraft Engineering and Aerospace Technology: An International Journal, 2006
KAYA METİN ORHAN
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Using the Dynamic Mesh Method for Genetically Obtained Wing Structures
Aircraft Engineering and Aerospace Technology: An International Journal, 2004
ERGÜVEN VATANDAS,İBRAHİM ÖZKOL,KAYA METİN ORHAN
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Three Axes Predictive Control of Autopilot for Missile
Aircraft Engineering and Aerospace Technology, Vol. 88, No. 4
ADA CELAL,KURAL AYHAN
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Model Predictive Control Of An Unmanned Aerial Vehicle
Aircraft Engineering and Aerospace Technology
HALİT FIRAT ERDOĞAN,KURAL AYHAN,ÖZSOY İSMAİL CAN
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Dynamic Finite Element Analysis of an Aircraft Seat
7th Ankara International Aerospace Conference, 11 Eylül 2013
DOĞAN VEDAT ZİYA,SİMİTCİOĞLU GÖKAY
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Random Vibration of A Rectangular FGM Strip
3rd Aircraft Structural Design Conference, 9 Ekim 2012
DOĞAN VEDAT ZİYA
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Aircraft Sensor and Actuator Fault Detection Isolation and Accommodation
JOURNAL OF AEROSPACE ENGINEERING, Ocak 2011, ISSN: 0893-1321
KIYAK EMRE,KAHVECİOĞLU AYŞE,ÇALIŞKAN FİKRET
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Aircraft icing detection identification and reconfigurable control based on Kalman filtering and neural networks
JOURNAL OF AEROSPACE ENGINEERING, Nisan 2008
ÇALIŞKAN FİKRET,AYKAN RAHMİ,HACIZADE CENGİZ
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