Yayınlar & Eserler

Yayın Ağı

SCI, SSCI ve AHCI İndekslerine Giren Dergilerde Yayınlanan Makaleler

Orbit Control of an Earth Orbiting Solar Sail Satellite

Polat H. C., Tekinalp O.
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , cilt.24, sa.1, ss.274-283, 2023 (SCI-Expanded) identifier identifier

Long term and safe relative orbit design for heterogeneous spacecraft clusters

Yaglioglu B., TEKİNALP O.
Advances in Space Research , cilt.67, sa.11, ss.3546-3558, 2021 (SCI-Expanded) identifier identifier

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

Ariyibi S. O., TEKİNALP O.
AEROSPACE SCIENCE AND TECHNOLOGY , cilt.105, 2020 (SCI-Expanded) identifier identifier

Output-feedback control of linear time-varying and nonlinear systems using the forward propagating Riccati equation

Prach A., TEKİNALP O., Bernstein D. S.
JOURNAL OF VIBRATION AND CONTROL , cilt.24, sa.7, ss.1239-1263, 2018 (SCI-Expanded) identifier identifier

Solving Constrained Optimal Control Problems Using State-Dependent Factorization and Chebyshev Polynomials

Gomroki M. M., Topputo F., Bernelli-Zazzera F., TEKİNALP O.
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS , cilt.41, sa.3, ss.618-631, 2018 (SCI-Expanded) identifier identifier

Infinite-Horizon Linear-Quadratic Control by Forward Propagation of the Differential Riccati Equation

Prach A., TEKİNALP O., Bernstein D. S.
IEEE CONTROL SYSTEMS MAGAZINE , cilt.35, sa.2, ss.78-93, 2015 (SCI-Expanded) identifier identifier

A new multiobjective simulated annealing algorithm

Tekinalp O., Karsli G.
JOURNAL OF GLOBAL OPTIMIZATION , cilt.39, sa.1, ss.49-77, 2007 (SCI-Expanded) identifier identifier identifier

A new steering law for redundant control moment gyroscope clusters

Tekinalp O., Yavuzoglu E.
AEROSPACE SCIENCE AND TECHNOLOGY , cilt.9, sa.7, ss.626-634, 2005 (SCI-Expanded) identifier identifier

A layerwise approach to piezo-electric plates accounting for adhesive flexibility and delaminated regions

Erturk C., Tekinalp O.
COMPUTERS & STRUCTURES , cilt.83, ss.279-296, 2005 (SCI-Expanded) identifier identifier

Simulated annealing for missile optimization: Developing method and formulation techniques

Tekinalp O., Bingol M.
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS , cilt.27, sa.4, ss.616-626, 2004 (SCI-Expanded) Sürdürülebilir Kalkınma identifier identifier

Tilt duct vertical takeoff and landing uninhabited aerial vehicle concept design study

Armutcuoglu O., Kavsaoglu M., Tekinalp O.
JOURNAL OF AIRCRAFT , cilt.41, sa.2, ss.215-223, 2004 (SCI-Expanded) identifier identifier

Turkish Small Satellite Program: Goals and policies

Askar M., Tekinalp O.
ACTA ASTRONAUTICA , cilt.46, ss.375-378, 2000 (SCI-Expanded) identifier identifier

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

Yuceoglu U., Toghi F., Tekinalp O.
JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME , cilt.118, sa.1, ss.122-134, 1996 (SCI-Expanded) identifier identifier

Diğer Dergilerde Yayınlanan Makaleler

Sequential Orbit Determination Verification for Geostationary Satellites

KÖKER A., TEKİNALP O., YILMAZ Ü. C., ŞAKACI C.
Advances in Astronautical Sciences , cilt.175, ss.3227-3244, 2021 (Hakemli Dergi)

Mission Analysis of a New Solar Sail Satellite Concept at Low Earth Orbit

POLAT H. C., TEKİNALP O.
Advances in Astronautical Sciences , cilt.175, ss.2387-2406, 2021 (Hakemli Dergi)

Effects of geometric and process parameters on drill transverse vibrations

Tekinalp O., Galip Ulsoy A.
Journal of Manufacturing Science and Engineering, Transactions of the ASME , cilt.112, sa.2, ss.189-194, 1990 (Scopus) identifier

Modeling and finite element analysis of drill bit vibrations

Tekinalp O., Ulsoy A.
Journal of Vibration and Acoustics, Transactions of the ASME , cilt.111, sa.2, ss.148-155, 1989 (Scopus) identifier

Modeling of drill bit transverse vibrations

Tekinalp O., Ulsoy A. G.
Proceedings of SPIE - The International Society for Optical Engineering , cilt.955, ss.129-134, 1988 (Scopus) identifier

Dynamic Modeling of Transverse Drill Bit Vibrations

Ulsoy A. G., Tekinalp O., Lenz E.
CIRP Annals - Manufacturing Technology , cilt.33, sa.1, ss.253-258, 1984 (Scopus) identifier identifier

Hakemli Kongre / Sempozyum Bildiri Kitaplarında Yer Alan Yayınlar

Development and Validation of a Fast Mid-Fidelity Comprehensive Analysis Tool for Generic E-VTOL Configurations

Şenipek M., Güngör O., TEKİNALP O.
48th European Rotorcraft Forum, Wintherthur, İsviçre, 6 - 08 Eylül 2022 identifier

Trajectory Tracking Controller Design and Simulation of a Tethered Aircraft,

Önen A. S., TEKİNALP O.
Airborne Wind Energy Conference (AWEC 2021), Milan, İtalya, 22 Haziran 2022

Aiding Coarse Attitude with Image-Based Three-Axis Attitude Measurements Using Multiplicative Extended Kalman Filter for Small Satellites

GÜZEL M. B., SÖKEN H. E., TEKİNALP O.
2021 AAS/AIAA Astrodynamics Specialists Conference, Amerika Birleşik Devletleri, 9 - 11 Ağustos 2021

BATCH ORBIT DETERMINATION COMPARISON FOR GEOSTATIONARY SATELLITES

KÖKER A., AYDIN S., DAĞ E., YILMAZ Ü. C., TEKİNALP O.
2021 ESA Guidance Navigation and Control Conference, Amerika Birleşik Devletleri, 22 - 25 Haziran 2021

Airborne Wind Energy: Trajectory Tracking Controller Design of a Tethered Aircraft

Önen A. S., Tekinalp O.
Wind Energy Science Conference, Hannover, Almanya, 25 - 28 Mayıs 2021, cilt.10, ss.119-120 Sürdürülebilir Kalkınma

Maneuver Planning Strategy for Rapid Response Solar Sail Satellite Concept

Polat H. C., Tekinalp O.
SciTech 2021, Science and Technology Forum and Exposition 2021, Virginia, Amerika Birleşik Devletleri, 11 - 21 Ocak 2021, cilt.1, sa.2, ss.1-17 Creative Commons License

SEQUENTIAL ORBIT DETERMINATION VERIFICATION FOR GEOSTATIONARY SATELLITES

Köker A., TEKİNALP O., Yılmaz Ü. C., Şakacı C.
AAS/AIAA Astrodynamics Specialist Conference, 2020, Virtual, Online, 9 - 12 Ağustos 2020, cilt.175, ss.3227-3244 identifier

MISSION ANALYSIS OF A NEW SOLAR SAIL SATELLITE CONCEPT AT LOW EARTH ORBIT

POLAT H., TEKİNALP O.
AAS/AIAA Astrodynamics Specialist Conference, 2020, Virtual, Online, 9 - 12 Ağustos 2020, cilt.175, ss.2387-2406 identifier

Maneuver planning strategy for rapid response solar sail satellite concept

POLAT H., TEKİNALP O.
AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021, Virtual, Online, 11 - 15 Ocak 2021, ss.1-17 identifier

Image Based Attitude Determination Algorithm for Small Satellites: Design and Preliminary Results

SÖKEN H. E., GÜZEL M. B., TEKİNALP O.
International Astronautical Federation, 2020 International Astronatucial Congress, Dubai, Sanal Yapıldı, Birleşik Arap Emirlikleri, 12 - 14 Ekim 2020

STATION-KEEPING STRATEGY FOR A SOLAR SAIL SATELLITE AT LOW EARTH ELLIPTICAL ORBIT

POLAT H. C., TEKİNALP O.
South East Europe Space Conference 2020, SEE UNIVERSE 2020, Belgrade, Sırbistan, 30 Eylül 2020

KÜÇÜK UYDULARDA YÖNELİM BELİRLEME FİLTRESİNİN KAMERA TABANLI ÖLÇÜMLER İLE DESTEKLENMESİ

Söken H. E., Güzel M. B., Tekinalp O.
8. ULUSAL HAVACILIK VE UZAY KONFERANSI, Ankara, Türkiye, 9 - 11 Eylül 2020, ss.1-13

FIRDÖNDÜ UYDULAR İÇİN SÖZLE ÖLÇÜMLER KULLANARAK YÖNELİM BAĞIMSIZ GERÇEK ZAMANLI MANYETOMETRE KALİBRASYONU

Çetin M. E., Söken H. E., Tekinalp O.
8. Ulusal Havacılık ve Uzay Konferansı, Ankara, Türkiye, 9 - 11 Eylül 2020, ss.1-8

Oscillating Control Moment Gyroscope Mathematical Model Development, Verification and Results

AKBULUT B., ARBERKLİ F., AZGIN K., TEKİNALP O.
International Symposium on Space Technology and Science, Fukui, Japonya, 15 - 21 Haziran 2019

Imaging-based attitude determination algorithm for small satellites: Design and the preliminary results

Güzel M. B., Söken H. E., Tekinalp O.
71st International Astronautical Congress, IAC 2020, Virtual, Online, 12 - 14 Ekim 2020, cilt.2020-October identifier

LATERAL-DIRECTIONAL CONTROL OF A HIGHLY MANEUVERABLE JET AIRCRAFT BASED ON COMBINATION OF MODAL AND OPTIMAL CONTROL THEORY

MESCE V., TEKİNALP O.
10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 18 - 20 Eylül 2019

A MISSION ANALYSIS SOFTWARE FOR SMALL SATELLITES

KOPRÜCÜ S. U., ÖZÇELİK S. A., ALTUNAY Ş., YAĞLIOĞLU B., TEKİNALP O.
10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 18 - 20 Eylül 2019

SCATTER AND SENSITIVITY ANALYSIS OF A PROJECTILE MODELED UNDER MAGNUS EFFECT

MUHİDDİNOĞLU A., YAYLA K., TEKİNALP O.
10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 18 - 20 Eylül 2019

INCORPORATING REAL LIFE DESIGN PROBLEMS INTO THE AEROSPACE CURRICULUM

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

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

YAĞLIOĞLU B., TEKİNALP O.
International Workshop on Satellite Constellations and Formation Flying, Glasgow, Birleşik Krallık, 16 - 19 Temmuz 2019

Slew Maneuver Control of Flexible Spacecraft

ALTINIŞIK S., TEKİNALP O.
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

YAĞLIOĞLU B., TEKİNALP O.
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

TEKİNALP O., ARIYIBI S.
AIAA Aviation 2019 Forum, Dallas, Texas, Amerika Birleşik Devletleri, 17 - 21 Haziran 2019 identifier

Oscillating Control Moment Gyroscope Experimental Results

AKBULUT B., ARBERKLİ F., AZGIN K., TEKİNALP O.
AIAA Scitech 2019 Forum, San Diego, California, Amerika Birleşik Devletleri, 7 - 11 Ocak 2019 identifier

Safe Spacecraft Rendezvous Using Dual Quaternions on Time-Dependent Trajectories Generated by Model Predictive Control

TEKİNALP O., BÜYÜKKOÇAK A. T.
AIAA Scitech 2019 Forum, San Diego, California, Amerika Birleşik Devletleri, 7 - 11 Ocak 2019 identifier

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

Kutlu A., TEKİNALP O.
9th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Türkiye, 11 - 14 Haziran 2019, ss.137-144 identifier identifier

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

Yaglioglu B., Atas O., Kahraman D., Kose S., TEKİNALP O., Suer M.
9th International Conference on Recent Advances in Space Technologies (RAST), İstanbul, Türkiye, 11 - 14 Haziran 2019, ss.553-557 Sürdürülebilir Kalkınma identifier identifier

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

BÜYÜKKOÇAK A. T., TEKİNALP O.
AAS/AIAA Astrodynamics Specialist Conference, Utah, Amerika Birleşik Devletleri, 19 - 23 Ağustos 2018, cilt.167, ss.1411-1422 identifier identifier

Solar Sail Application with a Proposed Low Earth Orbit Mission Concept

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

SAFE SPACECRAFT RENDEZVOUS WITH CONSTRAINED MODEL PREDICTIVE CONTROL

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

Safe Spacecraft Rendezvous with Constraint Model Predictive Control

TEKİNALP O., BÜYÜKKOÇAK A. T.
AIAA/ Amerıcan Astronautıcal Socıety Astrodynamics Specialst Conference, Snowbird, Utah, Amerika Birleşik Devletleri, 19 - 23 Ağustos 2018

Orbit Estimation Strategy for Low Earth Orbit and Geostationary Satellites

TEKİNALP O., KÖKER A.
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

BURAK A., ARBERKLİ F., TEKİNALP O., AZGIN K.
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

ARIYIBI S., TEKİNALP O.
2018 AIAA Information Systems-AIAA Infotech @ Aerospace, Kissimmee, Florida, Amerika Birleşik Devletleri, 8 - 12 Ocak 2018 identifier

EFFECTS OF ROTOR GEOMERY ON THE PERFORMANCE OF VIBRATING MASS CONTROL MOMENT GYRPOSCOPES

Arberkli F., Akbulut B., AZGIN K., TEKİNALP O.
AAS/AIAA Astrodynamics Specialist Conference, Washington, Amerika Birleşik Devletleri, 20 - 24 Ağustos 2017, cilt.162, ss.247-258 identifier identifier

A multi-national multi-institutional education framework: APSCO SSS-2B CubeSat Project

Yaglioglu B., AtaÅŸ Ã., Kahraman D., Köse S., Koru A., TEKİNALP O., et al.
69th International Astronautical Congress: #InvolvingEveryone, IAC 2018, Bremen, Almanya, 1 - 05 Ekim 2018, cilt.2018-October 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

Constrained Model Predictive Control for Spacecraft Rendezvous

BÜYÜKKOÇAK A. T., ALTINIŞIK S., TEKİNALP O.
9th Ankara International Aerospace Conference, 20 - 22 Eylül 2017

Angle Only Orbit Determination Using a Telescope System

KÖKER A., TEKİNALP O.
9th Ankara International Aerospace Conference, 20 - 22 Eylül 2017

Experimental Characterization and Validation of Vibrating Rotor Control Moment Gyroscope

AKBULUT B., ARBERKLİ F., AZGIN K., TEKİNALP O.
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

ARBERKLİ F., AKBULUT B., AZGIN K., TEKİNALP O.
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

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

ORBIT TRANSFER OF AN EARTH ORBITING SOLAR SAIL CUBESAT

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

A SIMPLIFIED MODEL FOR VIBRATING MASS CONTROL MOMENT GYROSCOPE

Akbulut B., Arberkli F., AZGIN K., TEKİNALP O.
27th AAS/AIAA Space Flight Mechanics Meeting, San-Antonio, Kuzey Mariana Adaları, 5 - 09 Şubat 2017, cilt.160, ss.2961-2974 identifier identifier

Main Rotor Downwash Effect on Seperation Characteristics of External Stores

Kapulu Ö., TEKİNALP O.
AIAA SciTech 2017, Atmospheric Flight Mechanics Conference, 9 - 13 Ocak 2017

Main rotor downwash effect on separation characteristics of external stores

Kapulu O., TEKİNALP O.
AIAA Atmospheric Flight Mechanics Conference, 2017, Colorado, Amerika Birleşik Devletleri, 5 - 09 Haziran 2017 identifier

A Novel Flight Control Algorithm for Multicopters

TEKİNALP O., Kumbasar S.
30th Congress of International Council of Aeronautical Sciences, 26 - 29 Eylül 2016

Tracking Control of Spacecraft Attitude on Time Dependent Trajectories

TEKİNALP O., TEKİNALP A.
Space 2016, AIAA/AAS Astrodynamics Specialist Conference, Long Beach, CA, Amerika Birleşik Devletleri, 13 - 16 Eylül 2016 identifier

Vibrating Mass Control Moment Gyroscope Dynamic Model Validation

AKBULUT B., ARBERKLİ F., AZGIN K., TEKİNALP O.
AIAA/AAS Astrodynamics Specialist Conference, Long Beach, California, Amerika Birleşik Devletleri, 13 - 16 Eylül 2016 identifier

Nonlinear Aircraft Flight Control Using Forward Propagating Riccati Equation

PRACH A., TEKİNALP O., BERNSTEIN D.
AIAA SCITECH 2016, SAN DIEGO, CA, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016

Comparison of Time and Frequency Domain Identification of Fixed Wing UAV

ŞİMSEK O., AS H., ORHAN E., TEKİNALP O.
AIAA, SCITECH 2016, SAN DIEGO, CA, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016

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

Comparison of time and frequency domain identification of a fixed-wing UAV

Simsek O., Haser S. A., Orhan E. H., TEKİNALP O.
AIAA Atmospheric Flight Mechanics Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016 identifier

Nonlinear aircraft flight control using the forward propagating riccati equation

PRACH A., TEKİNALP O., Bernstein D. S.
AIAA Guidance, Navigation, and Control Conference, 2016, California, 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

A novel flight contorl algorithm for multicopters

TEKİNALP O., Kumbasar S.
30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016, Daejeon, Güney Kore, 25 - 30 Eylül 2016 identifier

NONLINEAR TRACKING ATTITUDE CONTROL OF SPACECRAFT ON TIME DEPENDENT TRAJECTORIES

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

SOLAR SAIL SPACECRAFT BOOM VIBRATION DURING DEPLOYMENT AND DAMPING MECHANISMS

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

Nonlinear Tracking Attitude Control on Time Dependent Trajectories

TEKİNALP O., GOMROKI M. M., ATAŞ Ö.
AAS/AIAA Astrodynamics Specialist Conference, Vail, Colorado, Amerika Birleşik Devletleri, 9 - 13 Ağustos 2015

Solar Sail Spacecraft Boom Vibration During Deployment and Damping Analysis

TEKİNALP O., DEMİREL E., ATAŞ Ö.
AAS/AIAA ASTRODYNAMICS SPECIALIST CONFERENCE, Vail, Colorado, Amerika Birleşik Devletleri, 9 - 13 Ağustos 2015

Two ASRE Approaches with Application to Spacecraft Coulomb Formations

Gomroki M. M., Topputo F., TEKİNALP O., Bernelli-Zazzera F.
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

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

Vibrationally Excited Satellite Atttiude Actuator A Feasibity Study

TEKİNALP O., AKBULUT B., AZGIN K.
RAST 2015, Recent Advances on Space Technologies, İstanbul, Türkiye, 16 - 19 Haziran 2015

Fuzzy Logic Guidance of Formation Flight

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

Modeling and Controller Design of a VTOL UAV

Onen A. S., Cevher L., Şenipek M., Mutlu T., Gungor O., Uzunlar I. O., et al.
International Conference on Unmanned Aircraft Systems (ICUAS), Colorado, Amerika Birleşik Devletleri, 9 - 12 Haziran 2015, ss.329-337 identifier identifier

ARCHITECTURES FOR VIBRATING MASS ATTITUDE CONTROL ACTUATORS

Akbulut B., TEKİNALP O.
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

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

Gomroki M. M., TEKİNALP O.
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

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

Atas O., TEKİNALP O.
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

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

TEKİNALP O., ATAS Ö.
AAS/AIAA Space Flıght Mechanıcs Meetıng, Williamsburg, Virginia, Amerika Birleşik Devletleri, 12 - 15 Ocak 2015

State Dependent Riccati Equation Control of Spinning Three Craft Coulomb Formations

TEKİNALP O., MOHAMMAD MEHDI G.
AIAA/AAS space Flight Mechanics Meeting, Williamsburg, Virginia, Amerika Birleşik Devletleri, 12 - 15 Ocak 2015

Architecturesfor Vibrating Mass Atttitude Control Actuators

TEKİNALP O., BURAK A.
AIAA/AAS Space Flight Mechanics Meeting, Williamsburg, Virginia, Amerika Birleşik Devletleri, 12 - 15 Ocak 2015

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

TEKİNALP O., ŞİMŞEK O.
AIAA Atmospheric Flight Mechanics Conference, Kissimmee, Florida, Amerika Birleşik Devletleri, 5 - 09 Ocak 2015

Nonlinear Control to Maneuver Two Craft Coulomb Formation at Libration Poınts

TEKİNALP O., MOHAMMAD MEHDI G.
AIAA ScitTech 2015 Konferansı, Orlando, Florida, Amerika Birleşik Devletleri, 5 - 09 Ocak 2015

Nonlinear Guidance of Aircraft Formations

TEKİNALP O., Segun A.
AIAA SciTech 2015 Konferansi, Orlando, Florida, Amerika Birleşik Devletleri, 5 - 09 Ocak 2015

SDRE Based Guidance and Flight Control of Aircraft Formations

TEKİNALP O., SARPER K.
AIAA ScitTech 2015 Konferansı, Orlando, Florida, Amerika Birleşik Devletleri, 5 - 09 Ocak 2015 identifier

Nonlinear guidance of unmanned aircraft formations

Ariyib S., TEKİNALP O.
AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015, Florida, Amerika Birleşik Devletleri, 5 - 09 Ocak 2015 identifier

Nonlinear control to maneuver a two-craft coulomb formation at libration points

Gomroki M. M., TEKİNALP O.
AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015, Florida, Amerika Birleşik Devletleri, 5 - 09 Ocak 2015 identifier

Attitude control mechanization to de-orbit satellites using solar sails

TEKİNALP O., Atas O.
2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014, Rome, İtalya, 24 - 26 Mart 2014, cilt.153, ss.673-684 identifier

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

Prach A., TEKİNALP O., Bernstein D. S.
53rd IEEE Annual Conference on Decision and Control (CDC), Los-Angeles, Şili, 15 - 17 Aralık 2014, ss.854-859 identifier identifier

A Numerical Comparison of Frozen-Time and Forward-Propagating Riccati Equations for Stabilization of Periodically Time-Varying Systems

Prach A., TEKİNALP O., Bernstein D. S.
American Control Conference, Oregon, Amerika Birleşik Devletleri, 4 - 06 Aralık 2014, ss.5633-5638 identifier identifier

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

Gunaydin K., Cimen T., TEKİNALP O.
IEEE Aerospace Conference, Montana, Amerika Birleşik Devletleri, 1 - 08 Mart 2014 identifier identifier

Design of a full state SDRE tracking controller for an unmanned aircraft

PRACH A., TEKİNALP O.
AIAA Guidance, Navigation, and Control Conference 2014 - SciTech Forum and Exposition 2014, National Harbor, MD, Amerika Birleşik Devletleri, 13 - 17 Ocak 2014 identifier

Performance evaluation of sdre-based spacecraft attitude estimation and control

Choukroun D., TEKİNALP O.
54th Israel Annual Conference on Aerospace Sciences, IACAS 2014, Tel-Aviv and Haifa, İsrail, 19 - 20 Şubat 2014, cilt.1, ss.609-634 identifier

Relative position control of a two-satellite formation using the SDRE control method

Gomroki M. M., TEKİNALP O.
24th AAS/AIAA Space Flight Mechanics Meeting, 2014, Mexico, Amerika Birleşik Devletleri, 26 - 30 Ocak 2014, cilt.152, ss.235-254 identifier

Maneuvering of two-craft coulomb formation using ASRE method

Gomroki M. M., TEKİNALP O.
AIAA/AAS Astrodynamics Specialist Conference 2014, San Diego, CA, Amerika Birleşik Devletleri, 4 - 07 Ağustos 2014 identifier

Development of a state dependent ricatti equation based tracking flight controller for an unmanned aircraft

PRACH A., TEKİNALP O.
AIAA Guidance, Navigation, and Control (GNC) Conference, Boston, MA, Amerika Birleşik Devletleri, 19 - 22 Ağustos 2013 identifier

DYNAMIC STABILITY FLIGHT TESTS OF REMOTE SENSING MEASUREMENT CAPABLE AMPHIBIOUS UNMANNED AERIAL VEHICLE (A-UAV)

Yayla M., Sarsılmaz S. B., Mutlu T., Coşgun V., Kurtuluş B., Kurtuluş D. F., et al.
7. ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 11 - 13 Eylül 2013

Development of a State Dependent Riccati Equation Based Tracking Flight Controller for an Unmanned Aircraft

TEKİNALP O., PRACH A.
2013 AIAA Guidance Navigation and Control Conference, 19 - 22 Ağustos 2013

Spacecraft Attitude and Rate Estimation Using the SDRE Method

CHOUKROUN D., TEKİNALP O.
5the European Conference on Aeronautical and Space Sciences, 1 - 05 Temmuz 2013

Attitude Control of Satellites with De-Orbiting Solar Sails

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

Momentum envelopes and steering of control moment gyroscope clusters

TEKİNALP O.
AIAA/AAS Astrodynamics Specialist Conference 2012, Minneapolis, MN, Amerika Birleşik Devletleri, 13 - 16 Ağustos 2012 identifier

Multiobjective Conceptual Design of an Unmanned Combat Air Vehicle

TEKİNALP O., ÇAVUŞ N.
12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Indianapolis, Indiana, Amerika Birleşik Devletleri, 17 - 19 Eylül 2012 identifier

Fault Tolerant Control of an Over Actuated UAV

TEKİNALP O., YAVRUCUK İ.
AIAAGuidance, Navigation, and Control Conference, 8 - 11 Temmuz 2011 identifier

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

TEKİNALP O., KAYASTHA S., ÖZGÖREN K., NADJİM H.
Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011, Istanbul, Turkey, 9 - 11 Haziran 2011

Attitude control of a piezo-strut mounted camera on a spacecraft with deployed solar panels

Kayastha S., Akbulut B., TEKİNALP O., ÖZGÖREN M. K.
2011 IEEE Aerospace Conference, AERO 2011, Big Sky, MT, Amerika Birleşik Devletleri, 5 - 12 Mart 2011 identifier

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

Elmas T. C., TEKİNALP O.
ASME Dynamic Systems and Control Conference, Cambridge, Kanada, 12 - 15 Eylül 2010, ss.189-196 identifier identifier

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

TEKİNALP O., ÖZGÖREN K., KAYASHTA S.
AIAA/AAS Astrodynamics Specialist Conference, Toronto, Ontario, Canada, 2 - 05 Ağustos 2010

POINTING PERFORMANCE CONTROL OF A SPACECRAFT CAMERA USING PIEZOELECTRIC ACTUATORS

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

ATTITUDE CONTROL OF MULTIPLE RIGID BODY SPACECRAFT WITH FLEXIBLE HINGE JOINTS

Akbulut B., ÖZGÖREN M. K., TEKİNALP O.
20th AAS/AIAA Spaceflight Mechanics Meeting, California, Amerika Birleşik Devletleri, 14 - 18 Şubat 2010, cilt.136, ss.2477-2478 identifier identifier

Helicopter Flight Simulation and Automatic Flight Control System Design

TEKİNALP O., YAVRUCUK İ.
AIAC 2009, 17 - 19 Ağustos 2009

Flight Control System Design and Integration for a Small UAV Test Bed

TEKİNALP O., YAVRUCUK İ.
AIAC 2009, 17 - 19 Ağustos 2009

Simulation and Flight Control of a Tilt Duct UAV

TEKİNALP O., ÜNLÜ T., YAVRUCUK İ.
Modeling and Simulation Technologies Conference, Chicago, Amerika Birleşik Devletleri, 10 - 12 Ağustos 2009 identifier

Gimbal Angle Restricted Control Moment Gyroscope Clusters

TEKİNALP O., Elmas T., YAVRUCUK İ.
4th International Conference on Recent Advances in Space Technologies, İstanbul, Türkiye, 11 - 13 Haziran 2009, ss.585-590 identifier identifier

SATELLITE ATTITUDE CONTROL USING DISSIMILAR REDUNDANT ACTUATORS

Kahraman O., TEKİNALP O.
AAS/AIAA 19th Space Flight Mechanics Meeting, Savannakhet, Laos, 8 - 12 Şubat 2009, cilt.134, ss.2303-2315 identifier identifier

POINTING PERFORMANCE INVESTIGATION OF A MULTIPLE RIGID BODY SPACECRAFT

Akbulut B., ÖZGÖREN M. K., TEKİNALP O.
AAS/AIAA 19th Space Flight Mechanics Meeting, Savannakhet, Laos, 8 - 12 Şubat 2009, cilt.134, ss.1029-1030 identifier identifier

KALMAN FILTER BASED MULTIMODE ATTITUDE DETERMINATION ALGORITHMS FOR A LEO SATELLITE

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

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

Kutlu A., Haciyev C., TEKİNALP O.
3rd International Conference on Recent Advances in Space Technologies, İstanbul, Türkiye, 14 - 16 Haziran 2007, ss.458-459 identifier identifier

Trajectory optimization of advanced launch system

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

Spacecraft energy storage and attitude control

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

Modeling and robust control of a spinning missile

Semerci B., Merttopcuoglu O., TEKİNALP O.
22nd International Conference on Modelling Identification and Control, Innsbruck, Avusturya, 10 - 13 Şubat 2003, ss.584-590 identifier

Flight control of a tilt-duct VTOL UAV

Okan A., TEKİNALP O., Kavsaoǧlu M.
1st UAV Conference 2002, Portsmouth, VA, Amerika Birleşik Devletleri, 20 - 23 Mayıs 2002 identifier

Flight Control of a Tilt-Duct UAV

TEKİNALP O., KAVSAOĞLU M. Ş., OKAN A.
1st UAV Conference, Portsmouth, Virginia, Amerika Birleşik Devletleri, 20 - 23 Mayıs 2002

Modeling of laminated plates with surface bonded piezoelectric sensors and actuators

Erturk C., TEKİNALP O.
43rd Structures, Structural Dynamics and Materials Conference, Denver, CO, Amerika Birleşik Devletleri, 22 - 25 Nisan 2002, cilt.3, ss.1914-1924 identifier

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

TEKİNALP O., ÖZEMRE M.
AIAA Guidance, Navigation, and Control Conference and Exhibit, Montreal,Canada, 6 - 09 Ağustos 2001

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

Simulated annealing for missile trajectory planning and multidisciplinary missile design optimization

TEKİNALP O., Utalay S.
38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, Amerika Birleşik Devletleri, 10 - 13 Ocak 2000 identifier

Minimum fuel station keeping maneuver strategy for Turksat geostationary satellites

Erdal T., Tekinalp O., Tulunay Y.
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

Flight mechanics analysis of a tilt-rotor UAV

Okan A., TEKİNALP O., Kavsaoğlut M., Armutcuoğlu >., Tulunay E.
24th Atmospheric Flight Mechanics Conference, 1999, Oregon, Amerika Birleşik Devletleri, 9 - 11 Ağustos 1999, ss.681-691 identifier

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

Tekinalp O., Uslu O., Tulunay Y.
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

Gokkus L., Erkmen A., Tekinalp O.
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

Gokkus L., Erkmen A., Tekinalp O.
1997 IEEE International Symposium on Intelligent Control, İstanbul, Türkiye, 16 - 18 Temmuz 1997, ss.331-336 identifier identifier

Free bending vibrations of multi-layer, orthotropic, bonded, composite plate system

Yuceoglu U., Toghi F., TEKİNALP O.
Proceedings of the 1995 ASME International Mechanical Congress and Exposition, San-Francisco, Kostarika, 12 - 17 Kasım 1995, cilt.46, ss.83-94 identifier

Free vibrations of rotating, multi-layer, adhesively bonded beams

Yuceoglu U., TEKİNALP O., YAVUZ A.
Proceedings of the 1994 International Mechanical Engineering Congress and Exposition, Chicago, IL, USA, 6 - 11 Kasım 1994, cilt.18, ss.143-150 identifier

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

TEKINALP O., YUCEOGLU U., YAVUZ A.
5th International Conference on Recent Advances in Structural Dynamics, Southampton, Birleşik Krallık, 18 - 21 Temmuz 1994, ss.504-514 identifier

Transient response of simply-supported, adhesively bonded orthotropic plates

Toghi F., Yuceoglu U., TEKİNALP O.
Proceedings of the ASME Winter Conference, New Orleans, LA, USA, 28 Kasım - 03 Aralık 1993, ss.1-9 identifier

Free vibrations of adhesively bonded composite, orthotropic plates

Yuceoglu U., Toghi F., TEKİNALP O.
Proceedings of the 1993 ASME Winter Annual Meeting, New Orleans, LA, USA, 28 Kasım - 03 Aralık 1993, cilt.37, ss.297-307 identifier

Vibrations of two-layer, orthotrophic, beamlike strips connected by mechanical springs

TEKİNALP O., Yuceoglu U., Caglayan N.
Winter Annual Meeting of the American Society of Mechanical Engineers, Dallas, TX, USA, 25 - 30 Kasım 1990, cilt.19, ss.67-72 identifier

Modeling and finite element analysis of drill bit vibrations

Tekinalp O., Ulsoy A.
Advances in Design Automation - 1989, Montreal, Kanada, 17 - 21 Eylül 1989, cilt.18-2, ss.61-68 identifier

Effects of geometric and process parameters on drill transverse vibrations

Tekinalp O., Ulsoy A.
Sensors and Controls for Manufacturing - 1988, Chicago, MI, USA, 27 Kasım - 02 Aralık 1988, cilt.33, ss.33-40 identifier

VIBRATION MODES AND FREQUENCIES OF TWIST DRILLS USING LASER HOLOGRAPHIC INTERFEROMETRY.

MacBain J., Harding K., Tekinalp O.
Miami Beach, FL, USA, 17 - 22 Kasım 1985, cilt.18, ss.1-10 identifier

Metrikler

Yayın

150

Atıf (WoS)

181

H-İndeks (WoS)

9

Atıf (Scopus)

563

H-İndeks (Scopus)

14

Proje

11

Tez Danışmanlığı

72

Açık Erişim

38
BM Sürdürülebilir Kalkınma Amaçları