Image Based and Hybrid Visual Servo Control of an Unmanned Aerial Vehicle Recent Developments in Unmanned Aircraft Systems
2012, Springer
ZEHRA CEREN,ALTUĞ ERDİNÇ
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Intelligent Based Aircraft Engine Health Monitoring Improving Aircraft Engine Maintenance Effectiveness and Reliability
Saarbrücken/ALMANYA, 2011, LAP LAMBERT Academic Publishing GmbH&Co.KG
DEMİRCİ ŞEREF, HAJİYEV CHİNGİZ
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The effect of sweep angle on the limit cycle oscillations of aircraft wings
ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, Nisan 2015
SEHER EKEN,KAYA METİN ORHAN
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Kalman filter and neural network based icing a identification applied to A340 aircraft dynamics
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, Ocak 2005, ISSN: 0002-2667
AYKAN RAHMİ,HACIZADE CENGİZ,ÇALIŞKAN FİKRET
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Multiple fault-based FDI and reconfiguration for aircraft engine sensors
Aircraft Engineering and Aerospace Technology, Vol. 89, No. 3, Mayıs 2017, s. 397-405, ISSN: 0002-2667
YAZAR IŞIL,ÇALIŞKAN FİKRET,KIYAK EMRE
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Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: Part I
Aircraft Engineering and Aerospace Technology, Vol. 79, No. 2, Şubat 2007, s. 177-183, ISSN: 0002-2667
ÖZDEMİR ÖZGÜMÜŞ ÖZGE, KAYA METİN ORHAN
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The effect of sweep angle on the limit cycle oscillations of aircraft wings
ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, Vol. 2, No. 2, Ocak 2015, s. 199-215, ISSN: 2287-528X
EKEN SEHER, KAYA METİN ORHAN
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A Comparative Study on Multi-Fidelity Sonic Boom Prediction for a Supersonic Aircraft
AeroBest 2021, An Eccomas Thematic Conference on Multidisciplinary Design Optimization of Aerospace Systems, Lisbon (Virtual)/PORTEKİZ, 21 Temmuz 2021
YUSUF DEMİROĞLU, NİKBAY MELİKE
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Investigation of Nacelle Design Parameters for a Supersonic Aircraft with Low Fidelity Approaches
11th Ankara International Aerospace Conference (AIAC), Ankara (Virtual)/TÜRKİYE, 8 Eylül 2021
OMER OZYILMAZ, NİKBAY MELİKE
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Exploration of Optimal Propulsion System Airframe Integration Design Concepts for a Low Boom Supersonic Aircraft
AIAA Aviation Forum and Exposition, Washington, Washington (Virtual)/AMERİKA BİRLEŞİK DEVLETLERİ, 2 Ağustos 2021
IMRAK RUMED, KARASELVİ EMRE, TUTKUN BÜLENT, NİKBAY MELİKE
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The Vital Link: Using LabVIEW to Develop the Ground Processing Interface System (GPIS) Software for the C-5 Galaxy Aircraft
National Instruments (NI) Week 1998 [Poster Presentation & Proceedings recorded in a CD], Austin/AMERİKA BİRLEŞİK DEVLETLERİ, Vol. 1998, No. 246, 24 Ağustos 1998, s. 1-9
ÇİÇEK İSMAİL
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Local thermal non-equilibrium conjugate forced convection and entropy generation in an aircraft cabin with air channel partially filled porous insulation
Aircraft Engineering and Aerospace Technology, Kasım 2021, ISSN: 1748-8842
ÇİÇEK OKTAY, BAYTAŞ AHMET CİHAT
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CERTIFICATION OF AIRCRAFT GALLEYS BY FINITE ELEMENT METHOD AND STATIC TEST
10th Ankara International Aerospace Conference, 18 Eylül 2019
ÖNÜT ABDULLAH ERDİ,TÜRKMEN HALİT SÜLEYMAN
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Modeling and Control of a Novel Tilt Roll Rotor Quadrotor UAV
International Conference on Unmanned Aircraft Systems (ICUAS'13)
FATİH ŞENKUL, ERDİNÇ ALTUĞ
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Adaptive control of a tilt roll rotor quadrotor UAV
2014 International Conference on Unmanned Aircraft Systems (ICUAS), 27 Mayıs 2014
FATİH ŞENKUL,ALTUĞ ERDİNÇ
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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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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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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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Random Vibration of A Rectangular FGM Strip
3rd Aircraft Structural Design Conference, 9 Ekim 2012
DOĞAN VEDAT ZİYA
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