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SCI, SSCI ve AHCI İndekslerine Giren Dergilerde Yayınlanan Makaleler

Full envelope nonlinear flight controller design for a novel electric VTOL (eVTOL) air taxi

Suiçmez E., Kutay A. T.
AERONAUTICAL JOURNAL , cilt.1, ss.1-28, 2023 (SCI-Expanded) Creative Commons License identifier identifier
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  • Citations
    • Citation Indexes: 13
  • Captures
    • Readers: 31
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Optimization of reward shaping function based on genetic algorithm applied to a cross validated deep deterministic policy gradient in a powered landing guidance problem

Nugroho L., Andiarti R., Akmeliawati R., KUTAY A. T., Larasati D. K., Wijaya S. K.
Engineering Applications of Artificial Intelligence , cilt.120, 2023 (SCI-Expanded) identifier identifier
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  • Citations
    • Citation Indexes: 10
  • Captures
    • Readers: 21
  • Mentions
    • News Mentions: 1
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Single channel digital controller design for a high spinning rate rolling airframe missile

Suicmez E. C., KUTAY A. T.
AERONAUTICAL JOURNAL , cilt.126, sa.1305, ss.1815-1833, 2022 (SCI-Expanded) identifier identifier
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  • Citations
    • Citation Indexes: 1
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    • Readers: 2
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Identification of Physical Helicopter Models Using Subspace Identification

Avcioglu S., KUTAY A. T., Leblebicioglu K.
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY , cilt.65, sa.2, 2020 (SCI-Expanded) identifier identifier
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  • Citations
    • Citation Indexes: 4
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    • Readers: 4
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Command governor-based adaptive control for dynamical systems with matched and unmatched uncertainties

YAYLA M., Arabi E., KUTAY A. T., Yucelen T.
INTERNATIONAL JOURNAL OF ADAPTIVE CONTROL AND SIGNAL PROCESSING , cilt.32, sa.8, ss.1124-1144, 2018 (SCI-Expanded) identifier identifier
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  • Citations
    • Citation Indexes: 13
  • Usage
    • Downloads: 10
  • Captures
    • Readers: 10
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Simulation of Rapidly Maneuvering Airfoils with Synthetic Jet Actuators

Jee S., Lopez Mejia O. D., Moser R. D., Muse J. A., KUTAY A. T., Calise A. J.
AIAA JOURNAL , cilt.51, sa.8, ss.1883-1897, 2013 (SCI-Expanded) identifier identifier
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  • Citations
    • Citation Indexes: 11
  • Captures
    • Readers: 16
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Experimental results on adaptive output feedback control using a laboratory model helicopter

Kutay A. T., Calise A., Idan M., Hovakimyan N.
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY , cilt.13, sa.2, ss.196-202, 2005 (SCI-Expanded) identifier identifier
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  • Citations
    • Citation Indexes: 111
  • Captures
    • Readers: 31
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Diğer Dergilerde Yayınlanan Makaleler

Hibrit hedef kestirim algoritması tasarımı

Kale S., KUTAY A. T.
Havacılık ve Uzay Teknolojileri Dergisi , cilt.7, sa.2, ss.103-110, 2014 (Hakemli Dergi)

Dört rotorlu bir insansız hava aracının geri adımlama yöntemi ile yol takibi kontrolü

Emrecan S., KUTAY A. T.
Havacılık ve Uzay Teknolojileri Dergisi , cilt.7, sa.2, ss.1-13, 2014 (Hakemli Dergi)

Flow simulation of a controlled airfoil with synthetic jet actuators

Jee S. K., Lopez O., Moser R. D., Kutay A. T., Muse J. A., Calise A. J.
19th AIAA Computational Fluid Dynamics Conference , 2009 (Scopus) identifier
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  • Citations
    • Citation Indexes: 13
  • Captures
    • Readers: 16
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Vortex model based adaptive flight control using synthetic jets

Muse J. A., Tchieu A. A., Kutay A. T., Chandramohan R., Calise A. J., Leonard A.
AIAA Guidance, Navigation, and Control Conference and Exhibit , 2009 (Scopus) identifier

A novel force control traverse for simulating UAV flight in a wind tunnel

Muse J. A., Kutay A. T., Calise A. J.
AIAA Atmospheric Flight Mechanics Conference and Exhibit , 2008 (Scopus) identifier

Experimental trapped vorticity flight control using an augmenting error minimization adaptive law

Muse J. A., Kutay A. T., Calise A. J.
AIAA Guidance, Navigation and Control Conference and Exhibit , 2008 (Scopus) identifier
Hakemli Bilimsel Toplantılarda Yayımlanmış Bildiriler

Experimental Study on Active Vibration Control of a Piezo-Beam Structure with Finite Series Based Adaptive Controller

Gezer R. B., Alan A. B., Kutay A. T., ŞAHİN M.
AIAA SciTech Forum and Exposition, 2024, Florida, Amerika Birleşik Devletleri, 8 - 12 Ocak 2024 identifier

Quadcopter Guidance Law Design using Deep Reinforcement Learning

Aydinli S. U., KUTAY A. T.
10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023, İstanbul, Türkiye, 7 - 09 Haziran 2023 identifier identifier

Comparison of Deep Reinforcement Learning-Based Guidance Strategies under Non-Ideal Conditions

Aydinli S. U., KUTAY A. T.
9th International Conference on Control, Decision and Information Technologies, CoDIT 2023, Rome, İtalya, 3 - 06 Temmuz 2023, ss.1524-1529 identifier

A Modification to Adaptive Control with Time-varying Learning Rate for Improved Transient Performance

YAYLA M., KUTAY A. T.
AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022, California, Amerika Birleşik Devletleri, 3 - 07 Ocak 2022 identifier
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  • Citations
    • Citation Indexes: 1
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    • Readers: 1
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Energy-based adaptive flight controller for improved coordinated longitudinal control

YAYLA M., KUTAY A. T., Kutlu A.
AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021, Virtual, Online, 11 - 15 Ocak 2021, ss.1-18 identifier

An adaptive flight controller design for a tilt-prop fixed wing uav for all flight modes

YAYLA M., KUTAY A. T., Senipek M., Gungor O.
AIAA Scitech Forum, 2020, Florida, Amerika Birleşik Devletleri, 6 - 10 Ocak 2020, ss.1-20 identifier
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  • Citations
    • Citation Indexes: 13
  • Captures
    • Readers: 18
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Single hidden layer neural network based model reference adaptive controller for estimation of periodic disturbances

Gezer R. B., KUTAY A. T.
AIAA Scitech Forum, 2019, California, Amerika Birleşik Devletleri, 7 - 11 Ocak 2019 identifier

Multidisciplinary optimization and performance analysis tool for ballistic missiles

Adsız M. A., KUTAY A. T.
AIAA Scitech Forum, 2019, California, Amerika Birleşik Devletleri, 7 - 11 Ocak 2019 identifier

Implementation of physical subspace identification on a realistic helicopter

Avcıoğlu S., KUTAY A. T., Leblebicioğlu K.
AIAA Scitech Forum, 2019, California, Amerika Birleşik Devletleri, 7 - 11 Ocak 2019 identifier

Helicopter parameters estimation from subspace identification by constrained nonlinear optimization

Avcıoğlu S., KUTAY A. T., LEBLEBİCİOĞLU M. K., Özkazanç Y., YAVRUCUK İ.
45th European Rotorcraft Forum 2019, ERF 2019, Warszawa, Polonya, 17 - 20 Eylül 2019, cilt.2, ss.1001-1012 identifier

A Model Based Approach for Sensor Fault Detection in Civil Aircraft Control Surface

Sercekman O., KUTAY A. T.
IEEE/ION Position, Location and Navigation Symposium (PLANS), Monterrey, Meksika, 23 - 26 Nisan 2018, ss.715-729 identifier identifier

Experimental design and statistical modeling methodology for wind tunnel aerodynamics of an agile missile to improve the simulation accuracy and performance

Savas O., Topbas E., Unal K., Karaca H. D., KUTAY A. T.
AIAA Modeling and Simulation Technologies Conference, 2018, Florida, Amerika Birleşik Devletleri, 8 - 12 Ocak 2018 identifier

Nonlinear optimal adaptive transition control of a tolt-prop VTOL UAV

Senipek M., YAYLA M., Gungor O., Cevher L., KUTAY A. T., TEKİNALP O.
44th European Rotorcraft Forum 2018, ERF 2018, Delft, Hollanda, 18 - 21 Eylül 2018, cilt.2, ss.952-964 identifier

Reinforcement learning control for helicopter landing in autorotation

Kopsa K., KUTAY A. T.
44th European Rotorcraft Forum 2018, ERF 2018, Delft, Hollanda, 18 - 21 Eylül 2018, cilt.2, ss.917-924 identifier

ON ROBUSTNESS OF CONCURRENT LEARNING ADAPTIVE CONTROL TO TIME-VARYING DISTURBANCES AND SYSTEM UNCERTAINTIES

Sarsilmaz S. B., KUTAY A. T., Yucelen T.
ASME International Mechanical Engineering Congress and Exposition, Tama, Japonya, 3 - 09 Kasım 2017 identifier identifier

A Control System Architecture for Control of Non-Affine in Control, Open-Loop Unstable Underactuated Systems

Marangoz A., KUTAY A. T.
8th International Conference on Mechanical and Aerospace Engineering (ICMAE), Prague, Çek Cumhuriyeti, 22 - 25 Temmuz 2017, ss.780-785 identifier identifier

Attitude and Altitude Tracking of Hexacopter via LQR with Integral Action

Suicmez E. C., KUTAY A. T.
International Conference on Unmanned Aircraft Systems (ICUAS), Florida, Amerika Birleşik Devletleri, 13 - 16 Haziran 2017, ss.150-159 identifier identifier

Experimental Investigation of Optimal Gap Distance between Rotors of a Quadrotor UAV

KAYA D. D., KUTAY A. T., TEKİNALP O.
AIAA Aviation Forum 2017, Atmospheric Flight Mechanics Conference, 5 - 09 Haziran 2017

Estimation of Target Velocity under Scarce Range Information for IR Guided Missiles

Babaoglu B. C., KUTAY A. T.
IEEE Aerospace Conference, Montana, Amerika Birleşik Devletleri, 4 - 11 Mart 2017 identifier identifier

Adaptive roll control of guided munitions with state independent uncertainty parameterization

Ovec N. T., KUTAY A. T.
AIAA Guidance, Navigation, and Control Conference, 2017, Texas, Amerika Birleşik Devletleri, 9 - 13 Ocak 2017 identifier
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  • Citations
    • Citation Indexes: 1
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    • Readers: 3
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Adaptive model predictive control of uncertain systems with input constraints

YAYLA M., KUTAY A. T.
AIAA Guidance, Navigation, and Control Conference, 2017, Texas, Amerika Birleşik Devletleri, 9 - 13 Ocak 2017 identifier

Adaptive Control Algorithm for Linear Systems with Matched and Unmatched Uncertainties

YAYLA M., KUTAY A. T.
55th IEEE Conference on Decision and Control (CDC), Nevada, Amerika Birleşik Devletleri, 12 - 14 Aralık 2016, ss.2975-2980 identifier identifier

Guaranteed Exponential Convergence without Persistent Excitation in Adaptive Control

YAYLA M., KUTAY A. T.
11th UKACC International Conference on Control (UKACC Control), Belfast, Birleşik Krallık, 31 Ağustos - 02 Eylül 2016 identifier identifier

Automatic Landing Flare Control Design by Model-Following Control and Flight Test on X-Plane Flight Simulator

Cetin E., KUTAY A. T.
7th International Conference on Mechanical and Aerospace Engineering (ICMAE), London, Kanada, 18 - 20 Temmuz 2016, ss.416-420 identifier identifier

Particle Filter Studies on Terrain Referenced Navigation

Turan B., KUTAY A. T.
IEEE/ION Position, Location and Navigation Symposium (PLANS), Savannakhet, Laos, 11 - 14 Nisan 2016, ss.949-954 Sürdürülebilir Kalkınma identifier identifier

Propulsion System Selection and Modeling for a Quadrotor with Search and Rescue Mission

KAYA D., KUTAY A. T., KURTULUŞ D. F., TEKİNALP O., ŞİMŞEK İ., SOYSAL S., et al.
54th AIAA Aerospace Sciences Meeting, San Diego, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016 identifier

Design and control of a micro UAV

Kaya D., Büyükkoçak A. T., KUTAY A. T., TEKİNALP O.
AIAA Atmospheric Flight Mechanics Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016 identifier
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  • Citations
    • Citation Indexes: 1
  • Captures
    • Readers: 4
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Aerodynamic parameter estimation of a supersonic air to air missile with rapid speed variation

Bayoglu T., Nalci M. O., KUTAY A. T.
AIAA Atmospheric Flight Mechanics Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016 identifier
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  • Citations
    • Citation Indexes: 5
  • Captures
    • Readers: 7
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An analysis of stochastic disturbances on nonlinear missile-target engagements based on the adjoint method

Sezer E., Nalcı M. O., KUTAY A. T.
AIAA Modeling and Simulation Technologies Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016 identifier
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    • Readers: 1
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Extended kalman filter based robust altitude controller for sea skimming missiles

Dülgar Ö., Gezer R. B., KUTAY A. T.
AIAA Guidance, Navigation, and Control Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016 identifier

Capturability of Combined Augmented Proportional Navigation against a Pull-Up Maneuvering Target

Nugroho L., KUTAY A. T.
IEEE International Conference on Aerospace Electronics and Remote Sensing Technology (ICARES), Balvi, Letonya, 3 - 05 Aralık 2015 identifier identifier identifier

Uncertainty Parametrization on Inverted Pendulum with Model Reference Adaptive Control

SARSILMAZ S. B., YAYLA M., KUTAY A. T.
Ankara International Aerospace Conference (AIAC), 10 - 12 Eylül 2015

Modeling and Simulation of a Quadrotor using Curve Fitting Method

KAYA D. D., KUTAY A. T.
AIAA Atmospheric Flight Mechanics Conference, Dallas, TX, Amerika Birleşik Devletleri, 22 - 26 Haziran 2015

Calibration of Five Hole Probe with Redundant Coefficients

Karahan S., KUTAY A. T.
31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Dallas, TX, Amerika Birleşik Devletleri, 22 - 26 Haziran 2015
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    • Readers: 8
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A Comparative Study of a Pseudo Five Degree of Freedom and an Adjoint Model Against a Six Degree of Freedom Model for Fidelity Assessment

Sezer E., Nalci M. O., KUTAY A. T.
AIAA Modeling and Simulation Technologies Conference, Dallas, TX, Amerika Birleşik Devletleri, 22 - 26 Haziran 2015

Finite Series Based Model Reference Adaptive Control

Rustu Berk G., KUTAY A. T.
AIAA Atmospheric Flight Mechanics Conference, Dallas, TX, Amerika Birleşik Devletleri, 22 - 26 Haziran 2015
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  • Citations
    • Citation Indexes: 1
  • Captures
    • Readers: 3
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Linear Analysis of Zero-Lift Pitching Moment Coefficient and Gravity Effects on Missile Autopilots

Ovec N. T., Erer K. S., KUTAY A. T.
IEEE Aerospace Conference, Montana, Amerika Birleşik Devletleri, 7 - 14 Mart 2015 identifier identifier

Analysis of five-hole probe calibration parameters

Karahan S., KUTAY A. T.
31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2015, Texas, Amerika Birleşik Devletleri, 22 - 26 Haziran 2015 identifier

Robust Model Following Control Design for Missile Roll Autopilot

Gezer R. B., KUTAY A. T.
United-Kingdom-Automatic-Control-Council (UKACC) 10th International Conference on Control (CONTROL), Loughborough, Birleşik Krallık, 9 - 11 Temmuz 2014, ss.7-12 identifier identifier

Optimal Path Tracking Control of a Quadrotor UAV

Suicmez E. C., KUTAY A. T.
International Conference on Unmanned Aircraft Systems (ICUAS), Florida, Amerika Birleşik Devletleri, 27 - 30 Mayıs 2014, ss.115-125 Sürdürülebilir Kalkınma identifier identifier

Adaptive robust attitude controller design for a quadrotor platform

Yilmaz E., KUTAY A. T.
AIAA AVIATION 2014 -AIAA Atmospheric Flight Mechanics Conference 2014, Atlanta, GA, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014 identifier
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  • Citations
    • Citation Indexes: 3
  • Captures
    • Readers: 12
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Aerodynamic modeling and parameter estimation of a quadrotor helicopter

Kaya D., KUTAY A. T.
AIAA AVIATION 2014 -AIAA Atmospheric Flight Mechanics Conference 2014, Atlanta, GA, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014 identifier

SYSTEM IDENTIFICATION AND CONTROLLER DEVELOPMENTFOR A SMALL TURBOJET ENGINE

Ekinci S., KUTAY A. T., UZOL O., Yiğittürk M.
6th Ankara International Aerospace Conference, Türkiye, 14 - 16 Eylül 2011

A comparison of two novel direct adaptive control methods under actuator failure accommodation

Kutay A. T., Chowdhary G., Calise A. J., Johnson E. N.
AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, HI, Amerika Birleşik Devletleri, 18 - 21 Ağustos 2008 identifier

Closed-loop aerodynamic flow control of a free airfoil

Brzozowski D. P., Culp J. R., Kutay A. T., Muse J. A., Glezer A.
4th AIAA Flow Control Conference, Seattle, WA, Amerika Birleşik Devletleri, 23 - 26 Haziran 2008 identifier

Validation of a low-order model for closed-loop flow control enable flight

Tchieu A. A., Kutay A. T., Muse J. A., Calise A. J., Leonard A.
4th AIAA Flow Control Conference, Seattle, WA, Amerika Birleşik Devletleri, 23 - 26 Haziran 2008 identifier

Dynamic flight maneuvering using trapped vorticity flow control

Muse J. A., Kutay A. T., Brzozowski D. P., Culp J. R., Calise A. J., Glezer A.
46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Amerika Birleşik Devletleri, 7 - 10 Ocak 2008 identifier

A Comparison of Select Direct Adaptive Control Methods Under Actuator Failure Accommodation

KUTAY A. T., Chowdhary G., Calise A. J., Johnson E. N.
AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, Hawaii, Amerika Birleşik Devletleri, 18 - 21 Ağustos 2008

Validation of A Low Order Model for Closed Loop Flow Control Enabled Flight

Tchieu A., KUTAY A. T., Muse J., Calise A. J., Leonard A.
4th Flow Control Conference, Seattle, Washington, Amerika Birleşik Devletleri, 23 - 26 Haziran 2008

A closed-loop flight control experiment using active flow control actuators

Kutay A. T., Culp J. R., Muse J. A., Brzozowski D. P., Glezer A., Calise A. J.
45th AIAA Aerospace Sciences Meeting 2007, Reno, NV, Amerika Birleşik Devletleri, 8 - 11 Ocak 2007, cilt.2, ss.1289-1304 identifier

Adaptive longitudinal control of aircraft using synthetic jets

Muse J. A., Kutay A. T., Calise A. J.
AIAA Guidance, Navigation, and Control Conference 2007, Hilton Head, SC, Amerika Birleşik Devletleri, 20 - 23 Ağustos 2007, cilt.3, ss.2594-2615 identifier

A 1-DOF wind tunnel experiment in adaptive flow control

Kutay A. T., Calise A. J., Muse J. A.
AIAA Guidance, Navigation, and Control Conference 2006, Keystone, CO, Amerika Birleşik Devletleri, 21 - 24 Ağustos 2006, cilt.5, ss.3017-3028 identifier

“Adaptive Neural Network Based Control System Applications for Autonomous UAV

YAVRUCUK İ., KUTAY A. T.
AIAC 2005, 10 - 12 Eylül 2005

Distributed adaptive output feedback control design and application to a formation flight experiment

Kutay A. T., Fowler J. M., Calise A. J., D'Andrea R.
AIAA Guidance, Navigation, and Control Conference 2005, San Francisco, CA, Amerika Birleşik Devletleri, 15 - 18 Ağustos 2005, cilt.7, ss.4953-4965 identifier
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  • Citations
    • Citation Indexes: 13
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    • Readers: 7
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An adaptive guidance approach for spinning projectiles

Calise A. J., El-Shirbiny H. A., Kim N., Kutay A. T.
Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference, Providence, RI, Amerika Birleşik Devletleri, 16 - 19 Ağustos 2004, cilt.5, ss.3226-3238 identifier
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  • Citations
    • Citation Indexes: 15
  • Captures
    • Readers: 9
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Adaptive output feedback control with reduced sensitivity to sensor noise

Kutay A. T., Calise A., Hovakimyan N.
Annual American Control Conference (ACC 2003), Colorado, Amerika Birleşik Devletleri, 04 Haziran 2003 - 06 Haziran 2006, ss.5141-5146 Sürdürülebilir Kalkınma identifier identifier

Experimental results on adaptive output feedback control using a laboratory model helicopter

Kutay A. T., Calise A. J., Idan M., Hovakimyan N.
AIAA Guidance, Navigation, and Control Conference and Exhibit 2002, Monterey, CA, Amerika Birleşik Devletleri, 5 - 08 Ağustos 2002 identifier
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  • Citations
    • Citation Indexes: 7
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    • Readers: 4
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NEURAL NETWORK BASED ORBIT PREDICTION FOR A GEOSTATIONARY SATELLITE

KUTAY A. T., Yurdanur T., Tulunay E., TEKİNALP O.
Automatic Systems for Building the Infrastructure in Developing Countries 2001. Knowledge and Technology Transfer, Ohrid, Makedonya, 21 - 23 Mayıs 2001, ss.3-14
Kitaplar

Adaptive Neural Network Based Approach for Active Flow Control

Idan M., Calise A. J., KUTAY A. T., David E P.
Manipulation and Control of Jets in Crossflow, Karagozian Ann R., Cortelezzi Luca, Soldati Alfredo, Editör, Springer-Verlag Wien, Viyana, ss.287-297, 2003
Metrikler

Yayın

72

Atıf (WoS)

157

H-İndeks (WoS)

7

Atıf (Scopus)

444

H-İndeks (Scopus)

11

Atıf (Scholar)

463

H-İndeks (Scholar)

12

Atıf (Diğer Toplam)

225

Proje

10

Tez Danışmanlığı

50

Açık Erişim

40
BM Sürdürülebilir Kalkınma Amaçları