Yayınlar & Eserler

SCI, SSCI ve AHCI İndekslerine Giren Dergilerde Yayınlanan Makaleler

Quaternion-based nonlinear attitude control of quadrotor formations carrying a slung load

AEROSPACE SCIENCE AND TECHNOLOGY, cilt.105, 2020 (SCI İndekslerine Giren Dergi) identifier identifier

A new multiobjective simulated annealing algorithm

JOURNAL OF GLOBAL OPTIMIZATION, cilt.39, ss.49-77, 2007 (SCI İndekslerine Giren Dergi) identifier identifier identifier

A new steering law for redundant control moment gyroscope clusters

AEROSPACE SCIENCE AND TECHNOLOGY, cilt.9, ss.626-634, 2005 (SCI İndekslerine Giren Dergi) identifier identifier

Simulated annealing for missile optimization: Developing method and formulation techniques

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, cilt.27, ss.616-626, 2004 (SCI İndekslerine Giren Dergi) identifier identifier

Turkish Small Satellite Program: Goals and policies

ACTA ASTRONAUTICA, cilt.46, ss.375-378, 2000 (SCI İndekslerine Giren Dergi) identifier identifier

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

JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, cilt.118, ss.122-134, 1996 (SCI İndekslerine Giren Dergi) identifier identifier

Hakemli Kongre / Sempozyum Bildiri Kitaplarında Yer Alan Yayınlar

Oscillating Control Moment Gyroscope Mathematical Model Development, Verification and Results

International Symposium on Space Technology and Science, Fukui, Japonya, 15 - 21 Haziran 2019

INCORPORATING REAL LIFE DESIGN PROBLEMS INTO THE AEROSPACE CURRICULUM

10TH ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 18 - 20 Eylül 2019

A MISSION ANALYSIS SOFTWARE FOR SMALL SATELLITES

10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 18 - 20 Eylül 2019

SCATTER AND SENSITIVITY ANALYSIS OF A PROJECTILE MODELED UNDER MAGNUS EFFECT

10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 18 - 20 Eylül 2019

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

International Workshop on Satellite Constellations and Formation Flying, Glasgow, İngiltere, 16 - 19 Temmuz 2019

Slew Maneuver Control of Flexible Spacecraft

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

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

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

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

AIAA Aviation 2019 Forum, Dallas, Texas, Amerika Birleşik Devletleri, 17 - 21 Haziran 2019

Oscillating Control Moment Gyroscope Experimental Results

AIAA Scitech 2019 Forum, San Diego, California, Amerika Birleşik Devletleri, 7 - 11 Ocak 2019 identifier

SAFE SPACECRAFT RENDEZVOUS WITH CONSTRAINED MODEL PREDICTIVE CONTROL

AAS/AIAA Astrodynamics Specialist Conference, Utah, Amerika Birleşik Devletleri, 19 - 23 Ağustos 2018, cilt.167, ss.883-895 identifier

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

9th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Türkiye, 11 - 14 Haziran 2019, ss.553-557 identifier identifier

Solar Sail Application with a Proposed Low Earth Orbit Mission Concept

9th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Türkiye, 11 - 14 Haziran 2019, ss.285-291 identifier identifier

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

AAS/AIAA Astrodynamics Specialist Conference, Utah, Amerika Birleşik Devletleri, 19 - 23 Ağustos 2018, cilt.167, ss.1411-1422 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, Türkiye, 11 - 14 Haziran 2019, ss.137-144 identifier identifier

Orbit Estimation Strategy for Low Earth Orbit and Geostationary Satellites

AIAA/Amerıcan Astronautıcal Society, 2018 Astrodynamics Specialst Conference, Snowbird, Utah, Amerika Birleşik Devletleri, 19 - 23 Ağustos 2018 identifier

A Hypothetical Mechanical Design for Vibrating Mass Control Moment Gyroscopes

2018 Space Flight Mechanics Meeting, Kissimmee, Florida, Amerika Birleşik Devletleri, 8 - 12 Ocak 2018 identifier

Modeling and Control of Quadrotor Formations Carrying a Slung Load

2018 AIAA Information Systems-AIAA Infotech @ Aerospace, Kissimmee, Florida, Amerika Birleşik Devletleri, 8 - 12 Ocak 2018 identifier

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 identifier

Angle Only Orbit Determination Using a Telescope System

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

Experimental Characterization and Validation of Vibrating Rotor Control Moment Gyroscope

AIAA SPACE and Astronautics Forum and Exposition, Orlando, FL, Amerika Birleşik Devletleri, 12 - 14 Eylül 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, Amerika Birleşik Devletleri, 20 - 24 Ağustos 2017

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

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

ORBIT TRANSFER OF AN EARTH ORBITING SOLAR SAIL CUBESAT

27th AAS/AIAA Space Flight Mechanics Meeting, San-Antonio, Kuzey Mariana Adaları, 5 - 09 Şubat 2017, cilt.160, ss.2201-2212 identifier

A SIMPLIFIED MODEL FOR VIBRATING MASS CONTROL MOMENT GYROSCOPE

27th AAS/AIAA Space Flight Mechanics Meeting, San-Antonio, Kuzey Mariana Adaları, 5 - 09 Şubat 2017, cilt.160, ss.2961-2974 identifier

Main Rotor Downwash Effect on Seperation Characteristics of External Stores

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

A Novel Flight Control Algorithm for Multicopters

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

Vibrating Mass Control Moment Gyroscope Dynamic Model Validation

AIAA/AAS Astrodynamics Specialist Conference, Long Beach, California, Amerika Birleşik Devletleri, 13 - 16 Eylül 2016 identifier

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 identifier

Design and control of a micro UAV

AIAA Atmospheric Flight Mechanics Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016 identifier

SOLAR SAIL SPACECRAFT BOOM VIBRATION DURING DEPLOYMENT AND DAMPING MECHANISMS

AAS/AIAA Astrodynamics Specialist Conference, Colorado, Amerika Birleşik Devletleri, 11 - 13 Ağustos 2015, cilt.156, ss.2189-2202 identifier

NONLINEAR TRACKING ATTITUDE CONTROL OF SPACECRAFT ON TIME DEPENDENT TRAJECTORIES

AAS/AIAA Astrodynamics Specialist Conference, Colorado, Amerika Birleşik Devletleri, 11 - 13 Ağustos 2015, cilt.156, ss.1585-1597 identifier

Two ASRE Approaches with Application to Spacecraft Coulomb Formations

AstroNet-II International Final Conference, Tossa de Mar, İspanya, 15 - 19 Haziran 2015, cilt.44, ss.109-120 identifier identifier

Vibrationally Excited Satellite Attitude Actuator: a Feasibility Study

7th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Türkiye, 16 - 19 Haziran 2015, ss.183-186 identifier

Fuzzy Logic Guidance of Formation Flight

International Conference on Unmanned Aircraft Systems (ICUAS), Colorado, Amerika Birleşik Devletleri, 9 - 12 Haziran 2015, ss.167-175 identifier

Modeling and Controller Design of a VTOL UAV

International Conference on Unmanned Aircraft Systems (ICUAS), Colorado, Amerika Birleşik Devletleri, 9 - 12 Haziran 2015, ss.329-337 identifier 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, Amerika Birleşik Devletleri, 11 - 15 Ocak 2015, cilt.155, ss.3529-3546 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, Amerika Birleşik Devletleri, 11 - 15 Ocak 2015, cilt.155, ss.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, Amerika Birleşik Devletleri, 11 - 15 Ocak 2015, cilt.155, ss.3509-3528 identifier

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

53rd IEEE Annual Conference on Decision and Control (CDC), Los-Angeles, Şili, 15 - 17 Aralık 2014, ss.854-859 identifier

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

IEEE Aerospace Conference, Montana, Amerika Birleşik Devletleri, 1 - 08 Mart 2014 identifier

Attitude Control of Satellites with De-Orbiting Solar Sails

6th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Türkiye, 12 - 14 Haziran 2013, ss.347-351 identifier

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

ASME Dynamic Systems and Control Conference, Cambridge, Kanada, 12 - 15 Eylül 2010, ss.189-196 identifier

POINTING PERFORMANCE CONTROL OF A SPACECRAFT CAMERA USING PIEZOELECTRIC ACTUATORS

20th AAS/AIAA Spaceflight Mechanics Meeting, California, Amerika Birleşik Devletleri, 14 - 18 Şubat 2010, cilt.136, ss.661-663 identifier

ATTITUDE CONTROL OF MULTIPLE RIGID BODY SPACECRAFT WITH FLEXIBLE HINGE JOINTS

20th AAS/AIAA Spaceflight Mechanics Meeting, California, Amerika Birleşik Devletleri, 14 - 18 Şubat 2010, cilt.136, ss.2477-2478 identifier

Simulation and Flight Control of a Tilt Duct UAV

Modeling and Simulation Technologies Conference, Chicago, Amerika Birleşik Devletleri, 10 - 12 Ağustos 2009 identifier

Gimbal Angle Restricted Control Moment Gyroscope Clusters

4th International Conference on Recent Advances in Space Technologies, İstanbul, Türkiye, 11 - 13 Haziran 2009, ss.585-590 identifier identifier

POINTING PERFORMANCE INVESTIGATION OF A MULTIPLE RIGID BODY SPACECRAFT

AAS/AIAA 19th Space Flight Mechanics Meeting, Savannakhet, Laos, 8 - 12 Şubat 2009, cilt.134, ss.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 Şubat 2009, cilt.134, ss.1551-1566 identifier

SATELLITE ATTITUDE CONTROL USING DISSIMILAR REDUNDANT ACTUATORS

AAS/AIAA 19th Space Flight Mechanics Meeting, Savannakhet, Laos, 8 - 12 Şubat 2009, cilt.134, ss.2303-2315 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, Türkiye, 14 - 16 Haziran 2007, ss.458-459 identifier identifier

Spacecraft energy storage and attitude control

2nd International Conference on Recent Advances in Space Technologies, İstanbul, Türkiye, 9 - 11 Haziran 2005, ss.201-206 identifier identifier

Trajectory optimization of advanced launch system

2nd International Conference on Recent Advances in Space Technologies, İstanbul, Türkiye, 9 - 11 Haziran 2005, ss.374-378 identifier identifier

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

Minimum fuel station keeping maneuver strategy for Turksat geostationary satellites

3rd International Symposium on Reducing the Cost of Spacecraft Ground Systems and Operations, Tainan, Tayvan, 22 - 24 Mart 1999, cilt.3, ss.33-40 identifier

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

COSPAR Colloquium on Microsatellites as Research Tools, Tainan, Tayvan, 14 - 17 Aralık 1997, cilt.10, ss.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, Fransa, 7 - 11 Eylül 1997, ss.766-771 identifier identifier

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

1997 IEEE International Symposium on Intelligent Control, İstanbul, Türkiye, 16 - 18 Temmuz 1997, ss.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, İngiltere, 18 - 21 Temmuz 1994, ss.504-514 identifier