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Özel Aralık Girişi

Image Based and Hybrid Visual Servo Control of an Unmanned Aerial Vehicle Recent Developments in Unmanned Aircraft Systems
2012, Springer
ZEHRA CEREN,ALTUĞ ERDİNÇ
Erdinç Altuğ Bilimsel KitapKitap Bölümü
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
Cengiz Hacızade Bilimsel Kitap
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
Metin Orhan Kaya Özgün Makale
Kalman filter and neural network based icing a identification applied to A340 aircraft dynamics
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, Ocak 2005
AYKAN RAHMİ,HACIZADE CENGİZ,ÇALIŞKAN FİKRET
Fikret Çalışkan Özgün Makale
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
Fikret Çalışkan Özgün Makale
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
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
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
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
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
Prediction of Aircraft Failure Times Using Artificial Neural Networks and Genetic Algorithms
Journal of Aircraft, Vol. 51, No. 1, Ocak 2014, s. 47-53, ISSN: 0021-8669
KAYAKUTLU GÜLGÜN,ÖZKAN ÖMER,ALTAY AYÇA
Automated troubleshooting tools for minimizing downtime and reducing the labor and materialcosts of C-5 aircraft
AUTOTESTCON 2004, PROCEEDINGS, Eylül 2004, s. 504-510, ISSN: 1088-7725
ÇİÇEK İSMAİL,VİLLAREAL CARLOS
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, 24 Ağustos 1998
ÇİÇEK İSMAİL
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
Oktay Çiçek Özgün Makale
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
Halit Süleyman Türkmen Tam metin bildiri
Modeling and Control of a Novel Tilt Roll Rotor Quadrotor UAV
International Conference on Unmanned Aircraft Systems (ICUAS'13)
FATİH ŞENKUL, ERDİNÇ ALTUĞ
Erdinç Altuğ Tam metin bildiri
Adaptive control of a tilt roll rotor quadrotor UAV
2014 International Conference on Unmanned Aircraft Systems (ICUAS), 27 Mayıs 2014
FATİH ŞENKUL,ALTUĞ ERDİNÇ
Erdinç Altuğ Tam metin bildiri
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
Nazım Kemal Üre Tam metin bildiri
Model Predictive Control Of An Unmanned Aerial Vehicle
Aircraft Engineering and Aerospace Technology
HALİT FIRAT ERDOĞAN,KURAL AYHAN,ÖZSOY İSMAİL CAN
Ayhan Kural Özgün Makale
Three Axes Predictive Control of Autopilot for Missile
Aircraft Engineering and Aerospace Technology, Vol. 88, No. 4
ADA CELAL,KURAL AYHAN
Ayhan Kural Özgün Makale

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