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) identifier

2. 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) identifier identifier

3. 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) identifier

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) identifier

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) identifier

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) identifier

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) identifier

8. Multidisciplinary optimization and performance analysis tool for ballistic missiles

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

9. Implementation of physical subspace identification on a realistic helicopter

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

10. 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) identifier

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) identifier identifier

13. 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) identifier

14. 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) identifier

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) identifier identifier

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) identifier identifier

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) identifier identifier

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) identifier identifier

20. 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) identifier

21. 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) identifier

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) identifier identifier

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) identifier identifier

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) identifier identifier

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 identifier identifier

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) identifier

27. Design and control of a micro UAV

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

28. 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) identifier

29. 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) identifier

30. 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) identifier

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) identifier identifier identifier

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) identifier identifier

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) identifier

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) identifier identifier

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 identifier identifier

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) identifier

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) identifier

43. SYSTEM IDENTIFICATION AND CONTROLLER DEVELOPMENTFOR A SMALL TURBOJET ENGINE

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

44. 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) identifier

45. 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) identifier

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) identifier

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) identifier

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) identifier

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) identifier

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) identifier

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) identifier

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) identifier

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 identifier identifier

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) identifier

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)

218

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