Publications & Works

Articles Published in Journals That Entered SCI, SSCI and AHCI Indexes

Long term and safe relative orbit design for heterogeneous spacecraft clusters

Advances in Space Research, vol.67, no.11, pp.3546-3558, 2021 (Journal Indexed in SCI) identifier identifier

A new multiobjective simulated annealing algorithm

JOURNAL OF GLOBAL OPTIMIZATION, vol.39, no.1, pp.49-77, 2007 (Journal Indexed in SCI) identifier identifier identifier

A new steering law for redundant control moment gyroscope clusters

AEROSPACE SCIENCE AND TECHNOLOGY, vol.9, no.7, pp.626-634, 2005 (Journal Indexed in SCI) identifier identifier

Simulated annealing for missile optimization: Developing method and formulation techniques

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, vol.27, no.4, pp.616-626, 2004 (Journal Indexed in SCI) identifier identifier

Turkish Small Satellite Program: Goals and policies

ACTA ASTRONAUTICA, vol.46, pp.375-378, 2000 (Journal Indexed in SCI) identifier identifier

Free bending vibrations of adhesively bonded orthotropic plates with a single lap joint

JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, vol.118, no.1, pp.122-134, 1996 (Journal Indexed in SCI) identifier identifier

Refereed Congress / Symposium Publications in Proceedings

Maneuver planning strategy for rapid response solar sail satellite concept

AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021, Virtual, Online, 11 - 15 January 2021, pp.1-17 identifier

Oscillating Control Moment Gyroscope Mathematical Model Development, Verification and Results

International Symposium on Space Technology and Science, Fukui, Japan, 15 - 21 June 2019

A MISSION ANALYSIS SOFTWARE FOR SMALL SATELLITES

10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 18 - 20 September 2019

INCORPORATING REAL LIFE DESIGN PROBLEMS INTO THE AEROSPACE CURRICULUM

10TH ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 18 - 20 September 2019

SCATTER AND SENSITIVITY ANALYSIS OF A PROJECTILE MODELED UNDER MAGNUS EFFECT

10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 18 - 20 September 2019

Long Term and Safe Relative Orbit Design for Heterogenously Distributed Spacecraft Clusters

International Workshop on Satellite Constellations and Formation Flying, Glasgow, England, 16 - 19 July 2019

Slew Maneuver Control of Flexible Spacecraft

8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS), Madrid, Spain, 1 - 04 July 2019

Passively Safe Relative Orbit Configurations over LongTime Intervals for Heterogeneously Distributed SpacecraftClusters

8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS), Madrid, Spain, 1 - 04 July 2019

Control of a Quadrotor Formation Carrying a Slung Load Using Flexible Bars

AIAA Aviation 2019 Forum, Dallas, Texas, United States Of America, 17 - 21 June 2019 identifier

Oscillating Control Moment Gyroscope Experimental Results

AIAA Scitech 2019 Forum, San Diego, California, United States Of America, 7 - 11 January 2019 identifier

SAFE SPACECRAFT RENDEZVOUS WITH CONSTRAINED MODEL PREDICTIVE CONTROL

AAS/AIAA Astrodynamics Specialist Conference, Utah, United States Of America, 19 - 23 August 2018, vol.167, pp.883-895 identifier

Solar Sail Application with a Proposed Low Earth Orbit Mission Concept

9th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Turkey, 11 - 14 June 2019, pp.285-291 identifier identifier

TRACKING CONTROL OF SPACECRAFT ATTITUDE AND POSITION ON TIME DEPENDENT TRAJECTORIES USING DUAL QUATERNIONS

AAS/AIAA Astrodynamics Specialist Conference, Utah, United States Of America, 19 - 23 August 2018, vol.167, pp.1411-1422 identifier

A Multi-National Multi-Institutional Educaiton Framework: APSCO SSS-2B CubeSat Project

9th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Turkey, 11 - 14 June 2019, pp.553-557 identifier identifier

Formation Flight Design near Sun-Earth Collinear Libration Points under the Effect of Disturbances

9th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Turkey, 11 - 14 June 2019, pp.137-144 identifier identifier

Safe Spacecraft Rendezvous with Constraint Model Predictive Control

AIAA/ Amerıcan Astronautıcal Socıety Astrodynamics Specialst Conference, Snowbird, Utah, United States Of America, 19 - 23 August 2018

Orbit Estimation Strategy for Low Earth Orbit and Geostationary Satellites

AIAA/Amerıcan Astronautıcal Society, 2018 Astrodynamics Specialst Conference, Snowbird, Utah, United States Of America, 19 - 23 August 2018 identifier

A Hypothetical Mechanical Design for Vibrating Mass Control Moment Gyroscopes

2018 Space Flight Mechanics Meeting, Kissimmee, Florida, United States Of America, 8 - 12 January 2018 identifier

Modeling and Control of Quadrotor Formations Carrying a Slung Load

2018 AIAA Information Systems-AIAA Infotech @ Aerospace, Kissimmee, Florida, United States Of America, 8 - 12 January 2018 identifier

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

44th European Rotorcraft Forum 2018, ERF 2018, Delft, Netherlands, 18 - 21 September 2018, vol.2, pp.952-964 identifier

Angle Only Orbit Determination Using a Telescope System

9th Ankara International Aerospace Conference, 20 - 22 September 2017

Constrained Model Predictive Control for Spacecraft Rendezvous

9th Ankara International Aerospace Conference, 20 - 22 September 2017

Experimental Characterization and Validation of Vibrating Rotor Control Moment Gyroscope

AIAA SPACE and Astronautics Forum and Exposition, Orlando, FL, United States Of America, 12 - 14 September 2017 identifier

Effects of Rotor Geometry on the Performance of Vibrating Mass Control Moment Gyroscopes

AAS/AIAA Astrodynamics Specialist Conference, Columbia River George, Stevenson, WA, United States Of America, 20 - 24 August 2017

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

AIAA Aviation Forum 2017, Atmospheric Flight Mechanics Conference, 5 - 09 June 2017

A SIMPLIFIED MODEL FOR VIBRATING MASS CONTROL MOMENT GYROSCOPE

27th AAS/AIAA Space Flight Mechanics Meeting, San-Antonio, Northern Mariana Islands, 5 - 09 February 2017, vol.160, pp.2961-2974 identifier

ORBIT TRANSFER OF AN EARTH ORBITING SOLAR SAIL CUBESAT

27th AAS/AIAA Space Flight Mechanics Meeting, San-Antonio, Northern Mariana Islands, 5 - 09 February 2017, vol.160, pp.2201-2212 identifier

Main Rotor Downwash Effect on Seperation Characteristics of External Stores

AIAA SciTech 2017, Atmospheric Flight Mechanics Conference, 9 - 13 January 2017

A Novel Flight Control Algorithm for Multicopters

30th Congress of International Council of Aeronautical Sciences, 26 - 29 September 2016

Tracking Control of Spacecraft Attitude on Time Dependent Trajectories

Space 2016, AIAA/AAS Astrodynamics Specialist Conference, Long Beach, CA, United States Of America, 13 - 16 September 2016

Vibrating Mass Control Moment Gyroscope Dynamic Model Validation

AIAA/AAS Astrodynamics Specialist Conference, Long Beach, California, United States Of America, 13 - 16 September 2016 identifier

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

54th AIAA Aerospace Sciences Meeting, San Diego, United States Of America, 4 - 08 January 2016 identifier

Comparison of Time and Frequency Domain Identification of Fixed Wing UAV

AIAA, SCITECH 2016, SAN DIEGO, CA, United States Of America, 4 - 08 January 2016

Nonlinear Aircraft Flight Control Using Forward Propagating Riccati Equation

AIAA SCITECH 2016, SAN DIEGO, CA, United States Of America, 4 - 08 January 2016

Design and control of a micro UAV

AIAA Atmospheric Flight Mechanics Conference, 2016, California, United States Of America, 4 - 08 January 2016 identifier

NONLINEAR TRACKING ATTITUDE CONTROL OF SPACECRAFT ON TIME DEPENDENT TRAJECTORIES

AAS/AIAA Astrodynamics Specialist Conference, Colorado, United States Of America, 11 - 13 August 2015, vol.156, pp.1585-1597 identifier

SOLAR SAIL SPACECRAFT BOOM VIBRATION DURING DEPLOYMENT AND DAMPING MECHANISMS

AAS/AIAA Astrodynamics Specialist Conference, Colorado, United States Of America, 11 - 13 August 2015, vol.156, pp.2189-2202 identifier

Solar Sail Spacecraft Boom Vibration During Deployment and Damping Analysis

AAS/AIAA ASTRODYNAMICS SPECIALIST CONFERENCE, Vail, Colorado, United States Of America, 9 - 13 August 2015

Nonlinear Tracking Attitude Control on Time Dependent Trajectories

AAS/AIAA Astrodynamics Specialist Conference, Vail, Colorado, United States Of America, 9 - 13 August 2015

Vibrationally Excited Satellite Attitude Actuator: a Feasibility Study

7th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Turkey, 16 - 19 June 2015, pp.183-186 identifier

Two ASRE Approaches with Application to Spacecraft Coulomb Formations

AstroNet-II International Final Conference, Tossa de Mar, Spain, 15 - 19 June 2015, vol.44, pp.109-120 identifier identifier

Vibrationally Excited Satellite Atttiude Actuator A Feasibity Study

RAST 2015, Recent Advances on Space Technologies, İstanbul, Turkey, 16 - 19 June 2015

Fuzzy Logic Guidance of Formation Flight

International Conference on Unmanned Aircraft Systems (ICUAS), Colorado, United States Of America, 9 - 12 June 2015, pp.167-175 identifier

Modeling and Controller Design of a VTOL UAV

International Conference on Unmanned Aircraft Systems (ICUAS), Colorado, United States Of America, 9 - 12 June 2015, pp.329-337 identifier identifier

STATE DEPENDENT RICCATI EQUATION CONTROL OF COLLINEAR SPINNING THREE-CRAFT COULOMB FORMATIONS

25th American-Astronautical-Society/American Institute of Aeronautics and Astronautics Space Flight Mechanics Meeting, Virginia, United States Of America, 11 - 15 January 2015, vol.155, pp.643-657 identifier

ARCHITECTURES FOR VIBRATING MASS ATTITUDE CONTROL ACTUATORS

25th American-Astronautical-Society/American Institute of Aeronautics and Astronautics Space Flight Mechanics Meeting, Virginia, United States Of America, 11 - 15 January 2015, vol.155, pp.3509-3528 identifier

ATTITUDE CONTROL OF AN EARTH ORBITING SOLAR SAIL SATELLITE TO PROGRESSIVELY CHANGE THE SELECTED ORBITAL ELEMENT

25th American-Astronautical-Society (AAS)/American-Institute-of-Aeronautics-and-Astronautics (AIAA) Space Flight Mechanics Meeting, Virginia, United States Of America, 11 - 15 January 2015, vol.155, pp.3529-3546 identifier

Architecturesfor Vibrating Mass Atttitude Control Actuators

AIAA/AAS Space Flight Mechanics Meeting, Williamsburg, Virginia, United States Of America, 12 - 15 January 2015

Attitude Control of an Earth Orbiting Solar Sail Satellite to Progressively Change the Selected Orbital Elements

AAS/AIAA Space Flıght Mechanıcs Meetıng, Williamsburg, Virginia, United States Of America, 12 - 15 January 2015

State Dependent Riccati Equation Control of Spinning Three Craft Coulomb Formations

AIAA/AAS space Flight Mechanics Meeting, Williamsburg, Virginia, United States Of America, 12 - 15 January 2015

System Identification and Handling Quality Analysis of a UAV from Flight Test Data

AIAA Atmospheric Flight Mechanics Conference, Kissimmee, Florida, United States Of America, 5 - 09 January 2015

SDRE Based Guidance and Flight Control of Aircraft Formations

AIAA ScitTech 2015 Konferansı, Orlando, Florida, United States Of America, 5 - 09 January 2015

Nonlinear Guidance of Aircraft Formations

AIAA SciTech 2015 Konferansi, Orlando, Florida, United States Of America, 5 - 09 January 2015

Nonlinear Control to Maneuver Two Craft Coulomb Formation at Libration Poınts

AIAA ScitTech 2015 Konferansı, Orlando, Florida, United States Of America, 5 - 09 January 2015

Faux-Riccati Synthesis of Nonlinear Observer-Based Compensators for Discrete-Time Nonlinear Systems

53rd IEEE Annual Conference on Decision and Control (CDC), Los-Angeles, Chile, 15 - 17 December 2014, pp.854-859 identifier

Response Surface Based Performance Analysis of an Air-Defense Missile System

IEEE Aerospace Conference, Montana, United States Of America, 1 - 08 March 2014 identifier

Spacecraft Attitude and Rate Estimation Using the SDRE Method

5the European Conference on Aeronautical and Space Sciences, 1 - 05 July 2013

Attitude Control of Satellites with De-Orbiting Solar Sails

6th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Turkey, 12 - 14 June 2013, pp.347-351 identifier

Multiobjective Conceptual Design of an Unmanned Combat Air Vehicle

12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Indianapolis, Indiana, United States Of America, 17 - 19 September 2012

Fault Tolerant Control of an Over Actuated UAV

AIAAGuidance, Navigation, and Control Conference, 8 - 11 July 2011

Gain scheduled inverse optimal control for fine pointing of a spacecraft camera

Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011, Istanbul, Turkey, 9 - 11 June 2011

COMBINED USE OF CONTROL MOMENT GYROS AND MAGNETIC TORQUE RODS FOR SATELLITE ATTITUDE CONTROL

ASME Dynamic Systems and Control Conference, Cambridge, Canada, 12 - 15 September 2010, pp.189-196 identifier

Quaternion Based State Dependent Ricatti Equation Control of a Satellite Camera on Piezoelectric Actuators

AIAA/AAS Astrodynamics Specialist Conference, Toronto, Ontario, Canada, 2 - 05 August 2010

POINTING PERFORMANCE CONTROL OF A SPACECRAFT CAMERA USING PIEZOELECTRIC ACTUATORS

20th AAS/AIAA Spaceflight Mechanics Meeting, California, United States Of America, 14 - 18 February 2010, vol.136, pp.661-663 identifier

ATTITUDE CONTROL OF MULTIPLE RIGID BODY SPACECRAFT WITH FLEXIBLE HINGE JOINTS

20th AAS/AIAA Spaceflight Mechanics Meeting, California, United States Of America, 14 - 18 February 2010, vol.136, pp.2477-2478 identifier

Simulation and Flight Control of a Tilt Duct UAV

Modeling and Simulation Technologies Conference, Chicago, United States Of America, 10 - 12 August 2009 identifier

Gimbal Angle Restricted Control Moment Gyroscope Clusters

4th International Conference on Recent Advances in Space Technologies, İstanbul, Turkey, 11 - 13 June 2009, pp.585-590 identifier identifier

SATELLITE ATTITUDE CONTROL USING DISSIMILAR REDUNDANT ACTUATORS

AAS/AIAA 19th Space Flight Mechanics Meeting, Savannakhet, Laos, 8 - 12 February 2009, vol.134, pp.2303-2315 identifier

POINTING PERFORMANCE INVESTIGATION OF A MULTIPLE RIGID BODY SPACECRAFT

AAS/AIAA 19th Space Flight Mechanics Meeting, Savannakhet, Laos, 8 - 12 February 2009, vol.134, pp.1029-1030 identifier

KALMAN FILTER BASED MULTIMODE ATTITUDE DETERMINATION ALGORITHMS FOR A LEO SATELLITE

AAS/AIAA 19th Space Flight Mechanics Meeting, Savannakhet, Laos, 8 - 12 February 2009, vol.134, pp.1551-1566 identifier

Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data

3rd International Conference on Recent Advances in Space Technologies, İstanbul, Turkey, 14 - 16 June 2007, pp.458-459 identifier identifier

Spacecraft energy storage and attitude control

2nd International Conference on Recent Advances in Space Technologies, İstanbul, Turkey, 9 - 11 June 2005, pp.201-206 identifier identifier

Trajectory optimization of advanced launch system

2nd International Conference on Recent Advances in Space Technologies, İstanbul, Turkey, 9 - 11 June 2005, pp.374-378 identifier identifier

Flight Control of a Tilt-Duct UAV

1st UAV Conference, Portsmouth, Virginia, United States Of America, 20 - 23 May 2002

Artificial neural networks for transfer aligment and calibration of inertial navigation systems

AIAA Guidance, Navigation, and Control Conference and Exhibit, Montreal,Canada, 6 - 09 August 2001

NEURAL NETWORK BASED ORBIT PREDICTION FOR A GEOSTATIONARY SATELLITE

Automatic Systems for Building the Infrastructure in Developing Countries 2001. Knowledge and Technology Transfer, Ohrid, Macedonia, 21 - 23 May 2001, pp.3-14

Minimum fuel station keeping maneuver strategy for Turksat geostationary satellites

3rd International Symposium on Reducing the Cost of Spacecraft Ground Systems and Operations, Tainan, Taiwan, 22 - 24 March 1999, vol.3, pp.33-40 identifier

An attitude control sysytem design based on the TURKSAT-1B geostationary satellite

COSPAR Colloquium on Microsatellites as Research Tools, Tainan, Taiwan, 14 - 17 December 1997, vol.10, pp.143-151 identifier

Interacting fuzzy multimodel intelligent tracking system for swift target manoeuvres

1997 IEEE/RSJ International Conference on Intelligent Robot and Systems - Innovative Robotics for Real-World Applications (IROS 97), Grenoble, France, 7 - 11 September 1997, pp.766-771 identifier identifier

Tracking a swift target using the interacting fuzzy multi-model algorithm

1997 IEEE International Symposium on Intelligent Control, İstanbul, Turkey, 16 - 18 July 1997, pp.331-336 identifier identifier

NATURAL VIBRATION CHARACTERISTICS OF ROTATING, COMPOSITE MULTI-LAYER BEAMS AND BLADES

5th International Conference on Recent Advances in Structural Dynamics, Southampton, United Kingdom, 18 - 21 July 1994, pp.504-514 identifier