Yayınlar & Eserler

Makaleler 14
Tümü (14)
SCI-E, SSCI, AHCI (8)
SCI-E, SSCI, AHCI, ESCI (8)
Scopus (12)
TRDizin (2)
Hakemli Bilimsel Toplantılarda Yayımlanmış Bildiriler 58

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

AIAA SciTech Forum and Exposition, 2024, Florida, Amerika Birleşik Devletleri, 8 - 12 Ocak 2024, (Tam Metin Bildiri)

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

9th International Conference on Control, Decision and Information Technologies, CoDIT 2023, Rome, İtalya, 3 - 06 Temmuz 2023, ss.1524-1529, (Tam Metin Bildiri)

3. Quadcopter Guidance Law Design using Deep Reinforcement Learning

10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023, İstanbul, Türkiye, 7 - 09 Haziran 2023, (Tam Metin Bildiri)

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

AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022, California, Amerika Birleşik Devletleri, 3 - 07 Ocak 2022, (Tam Metin Bildiri)

5. Energy-based adaptive flight controller for improved coordinated longitudinal control

AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021, Virtual, Online, 11 - 15 Ocak 2021, ss.1-18, (Tam Metin Bildiri)

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

AIAA Scitech Forum, 2020, Florida, Amerika Birleşik Devletleri, 6 - 10 Ocak 2020, ss.1-20, (Tam Metin Bildiri)

7. Single hidden layer neural network based model reference adaptive controller for estimation of periodic disturbances

AIAA Scitech Forum, 2019, California, Amerika Birleşik Devletleri, 7 - 11 Ocak 2019, (Tam Metin Bildiri)

8. Implementation of physical subspace identification on a realistic helicopter

AIAA Scitech Forum, 2019, California, Amerika Birleşik Devletleri, 7 - 11 Ocak 2019, (Tam Metin Bildiri)

9. Helicopter parameters estimation from subspace identification by constrained nonlinear optimization

45th European Rotorcraft Forum 2019, ERF 2019, Warszawa, Polonya, 17 - 20 Eylül 2019, cilt.2, ss.1001-1012, (Tam Metin Bildiri)

10. Multidisciplinary optimization and performance analysis tool for ballistic missiles

AIAA Scitech Forum, 2019, California, Amerika Birleşik Devletleri, 7 - 11 Ocak 2019, (Tam Metin Bildiri)

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

IEEE/ION Position, Location and Navigation Symposium (PLANS), Monterrey, Meksika, 23 - 26 Nisan 2018, ss.715-729, (Tam Metin Bildiri)

13. Reinforcement learning control for helicopter landing in autorotation

44th European Rotorcraft Forum 2018, ERF 2018, Delft, Hollanda, 18 - 21 Eylül 2018, cilt.2, ss.917-924, (Tam Metin Bildiri)

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

44th European Rotorcraft Forum 2018, ERF 2018, Delft, Hollanda, 18 - 21 Eylül 2018, cilt.2, ss.952-964, (Tam Metin Bildiri)

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

ASME International Mechanical Engineering Congress and Exposition, Tama, Japonya, 3 - 09 Kasım 2017, (Tam Metin Bildiri)

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

8th International Conference on Mechanical and Aerospace Engineering (ICMAE), Prague, Çek Cumhuriyeti, 22 - 25 Temmuz 2017, ss.780-785, (Tam Metin Bildiri)

17. Attitude and Altitude Tracking of Hexacopter via LQR with Integral Action

International Conference on Unmanned Aircraft Systems (ICUAS), Florida, Amerika Birleşik Devletleri, 13 - 16 Haziran 2017, ss.150-159, (Tam Metin Bildiri)

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

AIAA Aviation Forum 2017, Atmospheric Flight Mechanics Conference, 5 - 09 Haziran 2017, (Tam Metin Bildiri)

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

IEEE Aerospace Conference, Montana, Amerika Birleşik Devletleri, 4 - 11 Mart 2017, (Tam Metin Bildiri)

20. Adaptive model predictive control of uncertain systems with input constraints

AIAA Guidance, Navigation, and Control Conference, 2017, Texas, Amerika Birleşik Devletleri, 9 - 13 Ocak 2017, (Tam Metin Bildiri)

21. Adaptive roll control of guided munitions with state independent uncertainty parameterization

AIAA Guidance, Navigation, and Control Conference, 2017, Texas, Amerika Birleşik Devletleri, 9 - 13 Ocak 2017, (Tam Metin Bildiri)

22. Adaptive Control Algorithm for Linear Systems with Matched and Unmatched Uncertainties

55th IEEE Conference on Decision and Control (CDC), Nevada, Amerika Birleşik Devletleri, 12 - 14 Aralık 2016, ss.2975-2980, (Tam Metin Bildiri)

23. Guaranteed Exponential Convergence without Persistent Excitation in Adaptive Control

11th UKACC International Conference on Control (UKACC Control), Belfast, Birleşik Krallık, 31 Ağustos - 02 Eylül 2016, (Tam Metin Bildiri)

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

7th International Conference on Mechanical and Aerospace Engineering (ICMAE), London, Kanada, 18 - 20 Temmuz 2016, ss.416-420, (Tam Metin Bildiri)

25. Particle Filter Studies on Terrain Referenced Navigation

IEEE/ION Position, Location and Navigation Symposium (PLANS), Savannakhet, Laos, 11 - 14 Nisan 2016, ss.949-954, (Tam Metin Bildiri) Sürdürülebilir Kalkınma

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

54th AIAA Aerospace Sciences Meeting, San Diego, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016, (Tam Metin Bildiri)

27. Aerodynamic parameter estimation of a supersonic air to air missile with rapid speed variation

AIAA Atmospheric Flight Mechanics Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016, (Tam Metin Bildiri)

28. Extended kalman filter based robust altitude controller for sea skimming missiles

AIAA Guidance, Navigation, and Control Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016, (Tam Metin Bildiri)

29. Design and control of a micro UAV

AIAA Atmospheric Flight Mechanics Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016, (Tam Metin Bildiri)

30. An analysis of stochastic disturbances on nonlinear missile-target engagements based on the adjoint method

AIAA Modeling and Simulation Technologies Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016, (Tam Metin Bildiri)

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

IEEE International Conference on Aerospace Electronics and Remote Sensing Technology (ICARES), Balvi, Letonya, 3 - 05 Aralık 2015, (Tam Metin Bildiri)

32. Uncertainty Parametrization on Inverted Pendulum with Model Reference Adaptive Control

Ankara International Aerospace Conference (AIAC), 10 - 12 Eylül 2015, (Tam Metin Bildiri)

33. Modeling and Simulation of a Quadrotor using Curve Fitting Method

AIAA Atmospheric Flight Mechanics Conference, Dallas, TX, Amerika Birleşik Devletleri, 22 - 26 Haziran 2015, (Tam Metin Bildiri)

34. Calibration of Five Hole Probe with Redundant Coefficients

31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Dallas, TX, Amerika Birleşik Devletleri, 22 - 26 Haziran 2015, (Tam Metin Bildiri)

35. A Comparative Study of a Pseudo Five Degree of Freedom and an Adjoint Model Against a Six Degree of Freedom Model for Fidelity Assessment

AIAA Modeling and Simulation Technologies Conference, Dallas, TX, Amerika Birleşik Devletleri, 22 - 26 Haziran 2015, (Tam Metin Bildiri)

36. Finite Series Based Model Reference Adaptive Control

AIAA Atmospheric Flight Mechanics Conference, Dallas, TX, Amerika Birleşik Devletleri, 22 - 26 Haziran 2015, (Tam Metin Bildiri)

37. Linear Analysis of Zero-Lift Pitching Moment Coefficient and Gravity Effects on Missile Autopilots

IEEE Aerospace Conference, Montana, Amerika Birleşik Devletleri, 7 - 14 Mart 2015, (Tam Metin Bildiri)

38. Analysis of five-hole probe calibration parameters

31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2015, Texas, Amerika Birleşik Devletleri, 22 - 26 Haziran 2015, (Tam Metin Bildiri)

39. Robust Model Following Control Design for Missile Roll Autopilot

United-Kingdom-Automatic-Control-Council (UKACC) 10th International Conference on Control (CONTROL), Loughborough, Birleşik Krallık, 9 - 11 Temmuz 2014, ss.7-12, (Tam Metin Bildiri)

40. Optimal Path Tracking Control of a Quadrotor UAV

International Conference on Unmanned Aircraft Systems (ICUAS), Florida, Amerika Birleşik Devletleri, 27 - 30 Mayıs 2014, ss.115-125, (Tam Metin Bildiri) Sürdürülebilir Kalkınma

41. Adaptive robust attitude controller design for a quadrotor platform

AIAA AVIATION 2014 -AIAA Atmospheric Flight Mechanics Conference 2014, Atlanta, GA, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014, (Tam Metin Bildiri)

42. Aerodynamic modeling and parameter estimation of a quadrotor helicopter

AIAA AVIATION 2014 -AIAA Atmospheric Flight Mechanics Conference 2014, Atlanta, GA, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014, (Tam Metin Bildiri)

43. SYSTEM IDENTIFICATION AND CONTROLLER DEVELOPMENTFOR A SMALL TURBOJET ENGINE

6th Ankara International Aerospace Conference, Türkiye, 14 - 16 Eylül 2011, (Tam Metin Bildiri)

44. Closed-loop aerodynamic flow control of a free airfoil

4th AIAA Flow Control Conference, Seattle, WA, Amerika Birleşik Devletleri, 23 - 26 Haziran 2008, (Tam Metin Bildiri)

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

AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, HI, Amerika Birleşik Devletleri, 18 - 21 Ağustos 2008, (Tam Metin Bildiri)

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

4th AIAA Flow Control Conference, Seattle, WA, Amerika Birleşik Devletleri, 23 - 26 Haziran 2008, (Tam Metin Bildiri)

47. Dynamic flight maneuvering using trapped vorticity flow control

46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Amerika Birleşik Devletleri, 7 - 10 Ocak 2008, (Tam Metin Bildiri)

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

AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, Hawaii, Amerika Birleşik Devletleri, 18 - 21 Ağustos 2008, (Tam Metin Bildiri)

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

4th Flow Control Conference, Seattle, Washington, Amerika Birleşik Devletleri, 23 - 26 Haziran 2008, (Tam Metin Bildiri)

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

45th AIAA Aerospace Sciences Meeting 2007, Reno, NV, Amerika Birleşik Devletleri, 8 - 11 Ocak 2007, cilt.2, ss.1289-1304, (Tam Metin Bildiri)

51. Adaptive longitudinal control of aircraft using synthetic jets

AIAA Guidance, Navigation, and Control Conference 2007, Hilton Head, SC, Amerika Birleşik Devletleri, 20 - 23 Ağustos 2007, cilt.3, ss.2594-2615, (Tam Metin Bildiri)

52. A 1-DOF wind tunnel experiment in adaptive flow control

AIAA Guidance, Navigation, and Control Conference 2006, Keystone, CO, Amerika Birleşik Devletleri, 21 - 24 Ağustos 2006, cilt.5, ss.3017-3028, (Tam Metin Bildiri)

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

AIAA Guidance, Navigation, and Control Conference 2005, San Francisco, CA, Amerika Birleşik Devletleri, 15 - 18 Ağustos 2005, cilt.7, ss.4953-4965, (Tam Metin Bildiri)

55. An adaptive guidance approach for spinning projectiles

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference, Providence, RI, Amerika Birleşik Devletleri, 16 - 19 Ağustos 2004, cilt.5, ss.3226-3238, (Tam Metin Bildiri)

56. Adaptive output feedback control with reduced sensitivity to sensor noise

Annual American Control Conference (ACC 2003), Colorado, Amerika Birleşik Devletleri, 04 Haziran 2003 - 06 Haziran 2006, ss.5141-5146, (Tam Metin Bildiri) Sürdürülebilir Kalkınma

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

AIAA Guidance, Navigation, and Control Conference and Exhibit 2002, Monterey, CA, Amerika Birleşik Devletleri, 5 - 08 Ağustos 2002, (Tam Metin Bildiri)

58. NEURAL NETWORK BASED ORBIT PREDICTION FOR A GEOSTATIONARY SATELLITE

Automatic Systems for Building the Infrastructure in Developing Countries 2001. Knowledge and Technology Transfer, Ohrid, Makedonya, 21 - 23 Mayıs 2001, ss.3-14, (Tam Metin Bildiri)
Kitaplar 1

1. Adaptive Neural Network Based Approach for Active Flow Control

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

73

Yayın (WoS)

23

Yayın (Scopus)

59

Atıf (WoS)

242

H-İndeks (WoS)

7

Atıf (Scopus)

508

H-İndeks (Scopus)

13

Atıf (Scholar)

463

H-İndeks (Scholar)

12

Atıf (Diğer Toplam)

225

Proje

10

Tez Danışmanlığı

52

Açık Erişim

48
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