• An integrated navigation system design for Quadrotors 

  Gümüşboğa, İlkay; Kıyak, Emre (Institute of Electrical and Electronics Engineers Inc., 2015)

  In this work, a particle filter based integrated navigation system is designed and tested with real quadrotor systems. Conventionally, Kalman filter based algorithms is used for navigation systems which is highly non-linear. ...

• The modeling and simulation of a quadrocopter 

  Kıyak, Emre; Ermeydan, Ahmet (EUROSIS, 2016)

  Mini-flying vehicles with four rotors which are called quadcopters have attracted many researchers in recent years. Quadrotor is the one of the most popular rotary wing aircraft in control problems. Vertical take off and ...

• Modelling and pid controller design for a quadrotor 

  Ünal, G.; Kıyak, Emre (EUROSIS, 2016)

  This paper presents the modelling of a four rotor vertical take-off and landing unmanned air vehicle known as the quadrotor aircraft, Vertical take off and landing, high maneuverability capabilities and indoor/outdoor ...

• Zaman Serilerinde NARX Sinir Ağları Modeliyle Uçuşa Elverişlilik Süresinin Kestirimi 

  Tatli, A.; Kahvecioğlu, Seray (Institute of Electrical and Electronics Engineers Inc., 2017)

  Havacılık planlamalara yo˘gun bir ¸sekilde ba¸svurulan ciddi bir sektördür. Yüksek maliyetlere sebep olabilecek plansızlı˘gın giderilmesi ve vahim sonuçlar do˘gurabilecek kazaların önüne geçilebilmesi için öngörülere ...

• The importance of preventive maintenance in terms of reliability in aviation sector 

  Kıyak, Emre (2011)

  Aircraft is a system that requires high reliability levels throughout flights. Preventive maintenance procedures are applied to maintain this reliability at an optimum level. The higher frequency of preventive maintenance ...

• Aircraft engine sensor fault detection, isolaton and reconfiguration using fuzzy logic control based unknown input observer 

  Yazar, Işıl; Kıyak, Emre (Lappeenranta University of Technology, 2014)

  In this paper, a model-based robust fault diagnosis approach 'Unknown Input Observer (UIO)', 'Generalized Observer Scheme (GOS)' and 'a Fuzzy Logic Control Mechanism' will be studied respectively for fault detection, ...

• A fault tolerant flight control system for sensor and actuator faults 

  Kıyak, Emre; Çalışkan, Fikret (2010)

  The purpose of the paper is to present an approach to detect, isolate and accommodate the sensor or actuator faults using bank of unknown input observers (UIO). Full order observers, reduced order observers, unknown input ...

• ARINC 629 data bus standard on aircrafts 

  Işık, Yasemin (2010)

  In earlier analogue avionic systems the number of cables used to transfer information between the various system components was considerable. With these systems, at least one pair of wires has been required for each signal ...

• NARX Neural Networks Based Time Series Prediction for Amount of Airworthiness Time 

  Tatli, Ali; Kahvecioğlu, Sinem (IEEE, 2016)

  Aviation, a serious sector, is required to recourse planning intensively. There is a need for foresight in order to eliminate the planless that can lead to high costs and prevent accidents that could cause to fatal ...

• Pitch rate damping of an aircraft by a fuzzy PD controller 

  Işık, Yasemin (2010)

  Aircraft dynamics are in general nonlinear, time varying, and uncertain. A control system (classical control systems) designed for a flight condition, may not provide the desired stability and performance characteristics ...

• Open and closed loop control of a transport aircraft after component failure 

  Daşkiran, O.; Kavsaoğlu, Mehmet Şerif (2011)

  Aircraft dynamics are severely affected by the damages and failures of components. If corrective commands are not supplied immediately, force and moment imbalances lead into catastrophic consequences. In this study, flight ...

• FDI & reconfiguration on aircraft engine by hamming-NN&UIO 

  Yazar, Işıl; Kıyak, Emre (2013)

  Fault detection, isolation and reconfiguration process has a vital importance especially in aviation sector. In this sector, health fault diagnosis can avoid systems abnormal situations and provides operational continuity ...

• The use of information technologies and systems in airlines 

  Oktal, Hakan; Oktal, Ö. (2009)

  All over the world, air passengers would like to determine their destination, prefer an airline company among the many in the world, buy their tickets without any difficulty and make any changes when necessary. Then they ...

• Performance figures of merit for turbojet/fan transport aircraft performance comparison and conceptual design 

  Cavcar, Mustafa; Cavcar, Aydan (2003)

  A set of aircraft performance figures of merit for different phases of flight mission is derived from aircraft performance equations. In addition, an overall performance figure of merit combining the derived performance ...

• Aero-propulsive modeling of transport aircraft for air traffic management applications 

  Cavcar, Mustafa; Cavcar, Aydan (2004)

  Aerodynamic and propulsive modeling of current aircraft fleet is vital for Air Traffic Management applications, especially for use in decision support tools to predict aircraft trajectories and simulation tools. There are ...

• Testing and characterization of ceramic thermal barrier coatings 

  Bartsch, Marion; Baufeld, Bernd; Dalkilic, S; Mircea, I (Trans Tech Publications LTD, 2005)

  This paper gives a short overview of tests applied for the investigation of long term behaviour of thermal barrier coating systems. A variety of tests has been conducted on an exemplary material system with the coatings ...

• Defect evolution in thermal barrier coating systems under multi-axial thermomechanical loading 

  Baufeld, B; Bartsch, M; Dalkilic, S; Heinzelmann, M (Elsevier Science Sa, 2005)

  In service, gas turbine components with thermal barrier coatings experience high cyclic mechanical and thermal loading. Important, but not yet considered sufficiently, are the multi-axial stresses arising from thermal ...

• The role of cyclic mechanical loading and thermal gradients in damage behavior of thermal barrier coating systems 

  Bartsch, Marion; Baufeld, Bernd; Dalkilic, S.; Heinzelmann, M. (2005)

  Ceramic thermal barrier coatings (TBC) can exhibit premature in-service failure due to spallation as a consequence of exposure to elevated temperatures, aggressive environments, and cyclic thermal and mechanical loading. ...

• Parallel solution of low aspect ratio rectangular flat wings in compressible flow 

  Durmuş, Gökhan; Kavsaoğlu, Mehmet Şerif; Kaynak, Ünver (2005)

  Two block parallel Navier Stokes solutions of an aspect ratio 1.0 flat plate with sharp edges are obtained at different Mach numbers and angles of attack. Reynolds numbers are of the order of 200,000-300,000. The flow field ...

• Failure analysis of an aircraft piston engine components 

  Turan, Dilek; Karcı, Adem (Pergamon-Elsevier Science LTD, 2009)

  In this study, failed parts from the piston engine of TB-20 Trinidad aircraft which declared an emergency landing to Anadolu University Airport, Eskisehir, Turkey due to the over-speed of propeller during a training flight ...

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