Academic Staff Roster includes academic activity information for 2017 and before; therefore the visible titles of faculty members may not be up to date. Academic activity information for 2018 and onwards can be tracked through AVESIS (Academic Data Management System).

Prof.Dr. OZAN TEKİNALP
FACULTY OF ENGINEERING
PublicationsResearchMembership & Awards
E-mail :  
Url :  https://www.ae.metu.edu.tr/~ozan
Phone :  +90312210 2471
Fax :  +903122104250
Address :
 

Education

  Bachelor's, Istanbul Technical University, Istanbul, Mechanical Eng.
  Master's, University of Michigan, Ann Arbor, MI, Mechanical Eng.
  Doctorate, University of Michigan, Ann Arbor, MI, Mechanical Eng.

Publications (INTERNATIONAL)

Journal Papers

  A.1 Ulsoy, A.G., Tekinalp, O., Dynamic Modeling of Drill Transverse Vibrations. "CIRP Annals", 33, (1984), p.253-258.
  A.2 Tekinalp, O., Ulsoy, A.G., Modeling and Finite Element Analysis of Drill Bit Vibrations. "ASME Journal of Vibration, Acoustics, Stress and Reliability in Design", 111, (1989), p.148-155.
  A.3 Tekinalp, O., Ulsoy, A.G., Effects of Geometric and Process Parameters on Drill Transverse Vibrations. "ASME Journal of Engineering for Industry", 112, (1990), p.189-194.
  A.4 Yuceoglu, U., Toghi, F. Tekinalp, O., Free Bending Vibrations of Adhesively Bonded Orthotropic Plates with Single Lap Joint. "ASME Journal of Vibration and Acoustics", 118, (1996), p.122-134.
  A.5 Aşkar, M. and Tekinalp, O., Turkish Small Satellite Program: Goals and Policies. "Acta Astronautica", 46, (2000), p.375-378.
  A.6 Ö. Armutçuoğlu, M.Ş. Kavsaoğlu, and O. Tekinalp, Tilt Duct Vertical Takeoff and Landing Uninhabited Aerial Vehicle Concept Design Study. "AIAA Journal of Aircraft", 41, (2004), p.215-223.
  A.7 O. Tekinalp and M. Bingol, Simulated Annealing for Missile Optimization: Developing the Method and Formulation Techniques. "AIAA Journal of Guidance, Control, and Dynamics", 27, (2004), p.616-626.
  A.8 Erturk, C.L., Tekinalp, O., A Layerwise Approach to Piezo-Electric Plates Accounting for Adhesive Layer Flexibility and Delaminated Regions. "Computers and Structures", 83, (2005), p.279-296.
  A.9 Tekinalp, O., Yavuzoglu, E., A New Steering Law for Redundant Control Moment Gyroscope Clusters. "Aerospace Science and Technology", 9, (2005), p.626-634.
  A.10 Tekinalp, O., Karsli, G., A New Multiobjective Simulated Annealing Algorithm. "Journal of Global Optimization", 39, (2007), p.49-77.
  A.11 Prach, A., Tekinalp, O., Bernstein, D.S.,, Infinite-Horizon Linear-Quadratic Control by Forward Propagation of the Differential Riccati Equation. "IEEE Control Systems Magazine", 35, (2015), p.78-93.
  A.12 Prach, A., Tekinalp, O., Bernstein, D.S.,, Output-Feedback Control of Linear Time-Varying and Nonlinear Systems Using the Forward Propagating Riccati Equation. "Journal of Vibration and Control", (2016).
  A.13 GOMROKI MOHAMMAD MEHDI,TOPPUTO FRANCESCO,BERNELLI ZAZZERA FRANKO,TEKINALP OZAN, Solving Constrained Optimal Control Problems Using State-Dependent Factorization and Chebyshev Polynomials. "Journal of Guidance, Control, and Dynamics", (2017), p.1-14.
 

Conference Papers

  A.1 Tekinalp, O. Ulsoy, A.G., Drill Bit Vibrations in Manufacturing Process. "Proceedings of the 1985 Conference on Intelligent Systems and Machines", (1985), p.298-304.
  A.2 MacBain, J.C., Harding, K.G., Tekinalp, O., Vibration Modes and Frequencies of Twist Drills Using Laser Holographic Interferometry. "Sensors and Controls for Manufacturing", PED-Vol.18, (1985).
  A.3 Tekinalp, O., Ulsoy, A.G., Modeling of Drill Bit Transverse Vibrations. "Proc. Int.Symposium on Optical Engr. and Industrial Sensing for Advanced Manufactruing Technologies", (1988).
  A.4 Tekinalp, O., Yuceoglu, U., Caglayan, N., Vibrations of Two-Layer, Orthotropic Beamlike Strips Connected by Mechanical Springs. "Recent Developments in Composite Materials and Structures", AD19, (1990), p.67-72.
  A.5 Yuceoglu, U, Tekinalp, O, Yavuz, A., Natural Vibrations and the Orthogonality Condition in Rotating Composite Multi-Layer Beams and Blades. "22nd Midwestern Mechanics Conference", 16, (1991), p.325-326.
  A.6 Yuceoglu, U, Tekinalp, O, Caglayan, N., Fundamental Modes and Orthogonality Condition for Elastically Connected Multi-Layer Beamlike Strips or Plates. "22nd Midwestern Mechanics Conference", (1991), p.310-311.
  A.7 Yuceoglu, U., Toghi, F., Tekinap, O., Free Vibrations of Adhesively Bonded Single Lap Joint and Symmetric Lap Joint in Composite Orthoropic Plates. "18th International Congress of Theoretical and Applied Mechanics", (1992).
  A.8 Toghi, F., Yuceoglu, U., Tekinalp, O., Free Vibrations of Adhesively Bonded Lap Joints in Orhtropic Plates. "Proceedings of the International Conference on Engineering Applications of Mechanics", 2, (1992), p.83-90.
  A.9 Yuceoglu, U., Toghi, F., Tekinalp, O., Free Vibrations of Adhesively Bonded Composite Orthotropic Plates. "Composite Materials and Structures", AD37, (1993), p.297-313.
  A.10 Toghi, F., Yuceoglu, U., Tekinalp, O., Transient Response for Simply Supported Adhesively Bonded Orthotopic Plates. "Proceedings of the ASME Winter Annual Meeting", NCA, (1993).
  A.11 Tekinalp, O., Yuceoglu, U., Yavuz, A., Natural Vibration Characteristics of Rotating Composite Multilayer Bams and Blades. "Structural Dynamics: Recent Advances", (1994), p.504-514.
  A.12 Yuceoglu, U., Tekinalp, O., Yavuz, A., Free Vibrations of Rotating Multi-Layer Adhesively Bonded Beams. "Materials for Noise and Vibration Control", NCA18, (1994).
  A.13 Yuceoglu, U., Toghi, F., Tekinalp, O., Free Bending Vibrations of Mulit-Layer Orthotropic Bonded Composite Plate System. "Dynamic Response and Behavior of Composites", AD46, (1995), p.83-94.
  A.14 Tekinalp, O., Arslan, E.M., Optimal Midcourse Trajectories for Precision Guided Munitions with Collocation and Nonlinear Programming. "Proc. 20th Congress of International Council of Aeronautical Sciences", 1, (1996), p.593-600.
  A.15 Gokkus, L., Erkmen, A., Tekinalp, O., Interacting Fuzzy Multi Model Intelligent Tracking System for Swift Target Manoeuvres. "Proceedings of IROS'97", (1997).
  A.16 Gokkus, L., Erkmen, A., Tekinalp, O., Tracking Swift Target Using the Interacting Fuzzy Multi-Model Algorithm. "Proceedings of the 12th IEEE International Symposium on Intelligent Control", (1997).
  A.17 Tekinalp, O., Uslu, O. and Tulunay, Y., An Attitude Control System Design Based on the TURKSAT 1B Geostationary Satellites. "COSPAR Colloquium on Scientific Microsatellites as Research Tools", (1997).
  A.18 Erdal, T., Tekinalp, O. and Tulunay, Y., Minimum Fuel Station Keeping Manoeuvre Strategy for TURKSAT Geostationary Satellites. "Third International Symposium on Reducing Space Mission Cost of Spacecraft Ground", (1999).
  A.19 Tekinalp, O. and Arslan, E.M., A Multidisciplinary Design Optimization Tool for Air to Surface Missiles. "3rd World Congress of Structural and Multidisciplinary Design Optimization", (1999).
  A.20 Askar, M. and Tekinalp, O., Turkish Small Satellite Program: Goals and Policies. "International Academy of Astronautics, 2nd IAA Symposium on Small Satellites for", (1999).
  A.21 Okan, A., Tekinalp, O., Armutçuoğlu, Ö., Kavsaoğlu, M.Ş. and Tulunay, E., Flight Mechanics Analysis of a Tilt-rotor UAV. "1999 AIAA Atmospheric Flight Mechanics Conference", (1999).
  A.22 Kavsaoğlu, M.S., Tekinalp, O., Tulunay, E., Okan, A. and Armutcuoğlu, Ö., Design, Flight Mechanics and Control of a VTOL UAV. "NATO RTO AVT Panel, Symposium on Unmanned Vehicles for Aerial, Ground and Naval Military Operations", (2000).
  A.23 Armutcuoğlu, Ö., Kavsaoğlu, M.Ş., Tekinalp, O., Okan, A. and Tulunay, E., Conceptual Design of a Tilt-Duct UAV. "15th International UAV Sustems Conference", (2000), p.28.1-11.
  A.24 Tekinalp, O. and Utalay, S., Simulated Annealing for Missile Trajectory Planning and Multidisciplinary Missile Design Optimization. "38th Aerospace Sciences Conference", (2000).
  A.25 Tekinalp, O. and Aşkar, M., Bilten’deki Uydu Çalışmalarına Genel Bir Bakış. "1st International Symposium: Global Space Activities and Potential In Turkey", (2001), p.35-42.
  A.26 Gökhan, Y. and Tekinalp, O., YAY Uydusu İçin Yönelme Kontrol Sistemi Tasarımı. "1st International Symposium: Global Space Activities and Potential In Turkey", (2001), p.97-104.
  A.27 Özkaptan, C. and Tekinalp, O., Uzay Uygulamalarında Küçük Uyduların Yeri ve Maliyeti Düşürme Yöntemleri. "1st International Symposium: Global Space Activities and Potential In Turkey", (2001), p.69-82.
  A.28 Tekinalp, O. and Özemre, M., Artificial Neural Networks for Transfer Alignment and Calibration of Inertial Navigation Systems. "AIAA 2001 Guidance, Navigation and Control Conference", (2001).
  A.29 Okan, A., Çelenligil, C. and Tekinalp, O., Uyduların Işıl Kontrolu ve Işıl Analizinde Kullanılan Yöntemler. "1st International Symposium: Global Space Activities and Potential In Turkey", (2001), p.435-442.
  A.30 Ertürk, C.L. and Tekinalp, O., Modeling of Laminated Plates With Surface Bonded Piezoelectric Sensors and Actuators. "2002 AIAA, ASME, AHS, Structures, Structural Dynamics, and Materials Conference, Adaptive Structures", (2002).
  A.31 Okan, A., Tekinalp, O. and Kavsaoğlu, M.Ş., Flight Control of a Tilt-Duct UAV. "1st International Conference on Unmanned Aerospace Vehicles", (2002).
  A.32 Tekinalp, O., Semerci, B. and Merttopcuoğlu, O., On the Guidance and Control of a Spinning Missile. "4th International Conference on Nonlinear Problems in Aviation and Aerospace", (2002).
  A.33 B. Semerci, O. Tekinalp, O. Merttopcuoglu, Modeling and Robust Control of a Spinning Missile. "IASTED International Conference on Modeling Identification and Control, Innsbruck", (2003).
  A.34 Karsli, G., Tekinalp, O., Trajectory Optimization of Advanced Launch System. "Proc. of 2nd Int. Conf. on Recent Advances in Space Technologies", (2005), p.374-378.
  A.35 Altay, A., Tekinalp, O., Spacecraft Energy Storage and Attitude Control. "Proceedings of 2nd Int. Conf. on Recent Advances in Space Technologies", (2005), p.201-206.
  A.36 O. Tekinalp, A. Altay, E. Yavuoglu, Control Moment Gyros for Energy Storage and Attitude Control in Small Satellite Missions. "Proceedings of The RTO Specialists' Meeting, Emerging and Future Technologies for Space Based Operat", RTB-SPSM, (2006), p.19(1-13).
  A.37 Kutlu, A., Haciyev, C., Tekinalp, O., Attitude Determination and Rotational Motion Parameters Identification of a LEO Satellite Through Magnetometer and Sun Sensor Data. "Proceedings of the 3rd International Conference on Recent Advances in Space Technologies", (2007).
  A.38 Özgür Kahraman, Ozan Tekinalp, Satellite attitude control using dissimilar redundant actuators. "19th AIAA/AAS Space Flight Mechanics Meeting", (2009).
  A.39 Ozan Tekinalp, Tuba Elmas, İlkay Yavrucuk, Gimbal angle restricted control moment gyroscope clusters. "RAST 2009, Recent Advances in Space Technologies", (2009).
  A.40 Burak Akbulut, Kemal Özgören, Ozan Tekinalp, Pointing performance investigation of a multiple rigid body spacecraft. "19th AIAA/AAS Space Flight Mechanics Meeting", (2009).
  A.41 Ozan Tekinalp, Tuğba Ünlü, İlkay Yavrucuk, Simulation and flight control of a tilt-duct UAV. "2009 AIAA Modeling and Simulation Technologies Conference, Chicago", (2009).
  A.42 Aykut Kutlu, Ozan Tekinalp, Kalman filter based multimode attitude determination algorithms for a low Earth orbit satellite. "19th AIAA/AAS Space Flight Mechanics Meeting", (2009).
  A.43 Tekinalp, O., Yavuzoglu, E., Solakoglu, E., Conceptual Design of Cheap, Modular, Light Weight Control Moment Gyroscopes for Small Satellites. "RTO-MP-AVT171 Workshop on the Multifunctional Structures and Technologies for Small Spacecraft", (2010).
  A.44 Tekinalp, O., Kayastha, S., Ozgoren, K.,, Pointing Performance Control of a Spacecraft Camera Using Piezoelectric Actuators . "20th AAS/AIAA Space Flight Mechanics Meeting, San Diego, CA, Feb. 14-17 2010.", (2010).
  A.45 Akbulut, B., Ozgoren, K., Tekinalp, O., Attitude Control of a Multiple Rigid Body Spacecraft with Flexible Joints. "20th AAS/AIAA Space Flight Mechanics Meeting, San Diego, CA, Feb. 14-17 2010", (2010).
  A.46 Kayastha, S., Tekinalp, O., Ozgoren, K., Quaternion Based State Dependent Ricatti Equation Control of a Satellite Camera on Piezoelectric Actuators. "AIAA Astrodynamics Specialist Conference, Toronto, Canada, 2-5 August 2010.", (2010).
  A.47 Elmas, T.C., Tekinalp, O., Combined Use of Control Moment Gyros and Magnetic Torque Rods for Satellite Attitude Control. "IFAC/ASME Dynamic Systems and Control Conference, Cambridge, MA, 13-15 Sept. 2010.", (2010).
  A.48 Kayastha, S., Horri, N.H., Tekinalp, O., Ozgoren, M.K., Gain scheduled inverse optimal control of a fine pointing spacecraft with deployed solar panels. "RAST 2011, Recent Advances in Space Technologies", (2011).
  A.49 Işık, S., Tekinalp, O., Yavrucuk, İ., Fault tolerant control of an over actuated UAV. "AIAA 2011 Guidance, Navigation and Control Conference", (2011).
  A.50 Kayasta, S., Akbulut, B., Tekinalp, O., Ozgoren, M.K., Attitude control of a piezo-strut mounted camera on spacecraft deployed solar panels. "IEEE Aerospace Conference", (2011).
  A.51 Tekinalp, O., Momentum Envelopes and Steering of Control Moment Gyroscope Clusters. " AIAA GNC/AFM/MST/ASC 2012 Conference, Minneapolis, Minnesota, 13-16 August, 2012.", (2012).
  A.52 Çavuş, N., Tekinalp, O.,, Multiobjective Conceptual Design of an Unmanned Combat Air Vehicle . "AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Indianapolis, Indiana", (2012).
  A.53 Choukroun, D., Tekinalp, O., Spacecraft Attitude and Rate Estimation and Attitude Control Using the SDRE Method,. "5th European Conference on Aeronautical and Space Sciences (EUCASS)", (2013).
  A.54 Prach, A., Tekinalp, O., Development of a State Dependent Ricatti Equation Based Tracking Flight Controller for an Unmanned Aircraft. "2013 AIAA Guidance Navigation and Control Conference", (2013).
  A.55 Tekinalp, O., Atas, O.,, Attitude Control of Satellites with De-Orbiting Solar Sails. "RAST 2013, Recent Advances on Space Technologies", (2013).
  A.56 Choukroun,D., Tekinalp, O., Performance Evaluation of SDRE-Based Spacecraft Attitude Estimation and Control. "54th Israel Annual Conference on Aerospace Sciences", (2014).
  A.57 Gunaydin, K., Cimen, T., Tekinalp, O., Response Surface Based Performance Analysis of an Air-Defense Missile System. "2014 IEEE Aerospace Conference", (2014).
  A.58 Prach, A., Tekinalp, O., Bernstein, D.S., A Numerical Comparison of Frozen-Time and Forward-Propagating Riccati Equations for Stabilization of Periodically Time-Varying Systems. "2014 American Control Conference", (2014).
  A.59 Prach, A., Tekinalp, O., Bernstein, D.S., Faux-Riccati Synthesis of Nonlinear Observer-Based Compensators for Discrete Time Nonlinear Systems. "IEEE 53rd International Conference on Decision and Control", (2014).
  A.60 Prach, A., Tekinalp, O., Design of a Full State SDRE Tracking Controller for an Unmanned Aircraft. "AIAA Guidance Navigation Control Conference, National Harbor, Maryland, January, 13-17, 2014,", (2014).
  A.61 Tekinalp, O., Atas, O,, Attitude Control Mechanization to De-Orbit Satellites Using Solar Sails. " 2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems", (2014).
  A.62 Gunaydin, K., Cimen, T., Tekinalp, O., Response Surface Based Performance Analysis of an Air-Defense Missile System Against Maneuvering Targets. "AIAA Aviation 2014 Modeling and Simulation Technologies Conference", (2014).
  A.63 Gomroki, M.M., Tekinalp, O., Relative Position Control of a Two-Satellite Formation Using the SDRE Control Method. "24th AAS/AIAA Space Flight Mechanics Meeting", (2014).
  A.64 Gomroki, M.M., Tekinalp, O.,, Maneuvering of Two-Craft Coulomb Formation Using ASRE Method. "AIAA, Space 2014, AIAA/AAS Astrodynamics Specialist Conference", (2014).
  A.65 Kutlu, A., Tekinalp, O.,, Development of a Simulation Tool for the Design of Spacecraft Formation Flight. "8th Ankara International Aerospace Conference", (2015).
  A.66 Onen, A.S., Levent, C., Senipek, M., Mutlu, T., Gungor, O., Uzunlar, I.O, Kurtul, Modelling and Controller Design of a VTOL UAV. " 2015 International Conference on Unmanned Air Systems (ICUAS), Denver, CO", (2015).
  A.67 Gomroki, M.M., Tekinalp, O., Nonlinear Control to Maneuver Two-Craft Coulomb Formation at Libration Points. " AIAA SciTech 2015, Orlando, FL", (2015).
  A.68 Tekinalp, O., Kumbasar, S.,, SDRE Based Guidance and Flight Control of Aircraft Formations. "IAA SciTech 2015, Orlando, FL", (2015).
  A.69 Kumbasar, S., Tekinalp, O., Fuzzy Logic Guidance of Formation Flight. "ICUAS 2015, International Conference on Unmanned Air Systems, Denver, CO", (2015).
  A.70 Tekinalp, O., Gomroki, M.M., Atas, O., Nonlinear Tracking Attitude Control of Spacecraft on Time Dependent Trajectories. "AAS/AIAA Astrodynamics Specialist Conference, Vail, CO", (2015).
  A.71 Akbulut, B., Tekinalp, O., Azgin, K.,, Vibrationally Excited Satellite Attitude Actuator: A Feasibility Study. "RAST 2105, Recent Advances on Space Technologies, İstanbul", (2015).
  A.72 Akbulut, B., Tekinalp, O.,, Architectures for Vibrating Mass Attitude Control Actuators. " AIAA/AAS Space Flight Mechanics Meeting, Williamsburg, VA", (2015).
  A.73 Gomroki, M.M., Tekinalp, O.,, State Dependent Riccati Equation Control of Spinning Three-Craft Coulomb Formations. "AIAA/AAS Space Flight Mechanics Meeting, Williamsburg, VA", (2015).
  A.74 Simsek, O., Tekinalp, O., System Identification and Handling Quality Analysis of a UAV from Flight Test Data. "AIAA SciTech 2015, Orlando, FL", (2015).
  A.75 Ariyibi, S., Tekinalp, O., Nonlinear Guidance of Unmanned Aircraft Formations. " AIAA SciTech 2015, Orlando, FL", (2015).
  A.76 Atas, O, Tekinalp, O., Attitude Control of an Earth Orbiting Solar Sail Satellite to Progressively Change the Selected Orbital Element. "AIAA/AAS Space Flight Mechanics Meeting, Williamsburg, VA", (2015).
  A.77 Atas, O., Demiral, E., Tekinalp, O., Solar Sail Spacecraft Boom Vibration During Deployment and Damping Analysis. " AAS/AIAA Astrodynamics Specialist Conference, Vail, CO,", (2015).
  A.78 Prach, A., Tekinalp, O, Bernstein, D.S.,, Nonlinear Aircraft Flight Control Using Forward Propagating Riccati Equation. " AIAA SciTech 2016, San Diego, CA,", (2016).
  A.79 Simsek, O., Haser, A.S., Orhan, E.T., Tekinalp, O.,, Comparison of Time and Frequency Domain Identification of Fixed Wing UAV,. "AIAA SciTech 2016, San Diego, CA", (2016).
  A.80 Kaya, D.D., Kutay, A., Kurtulus, D.F., Tekinalp, O., Simsek, I., Soysal, S., Hos, Propulsion System Selection and Modeling for a Quadrotor with Search and Rescue Mission. "AIAA SciTech 2016, San Diego, CA", (2016).
  A.81 Kutlu, A., Tekinalp, O.,, A Simulation Tool to Design Satellite Formations. "6th International Conference on Astrodynamics Tools and Techniques (ICATT), Darmstadt", (2016).
  A.82 Tekinalp, O., Tekinalp, A.,, Tracking Control of Spacecraft Attitude on Time Dependent Trajectories. "Space 2016, AIAA/AAS Astrodynamics Specialist Conference, Long Beach, CA,", (2016).
  A.83 Tekinalp, O., Kumbasar, S.,, A Novel Flight Control Algorithm for Multicopters. "ICAS 2016, 30th Congress of International Council of the Aeronautical Sciences, Daejeon, Korea", (2016).
  A.84 Kaya, D.,D., Buyukkocak, A.T., Kutay, A.T., Tekinalp, O., Design and Control of a Micro UAV. "AIAA Aviation Forum 2016, Washington D.C.,", (2016).
  A.85 Akbulut, B., Arberkli, F., Azgin, K., Tekinalp, O.,, Vibrating Mass Control Moment Gyroscope Dynamic Model Validation. "Space 2016, AIAA/AAS Astrodynamics Specialist Conference, Long Beach, CA", (2016).
  A.86 KAYA DILBER DERYA,KUTAY ALI TÜRKER,TEKINALP OZAN, Experimental Investigation of Optimal Gap Distance between Rotors of a Quadrotor UAV. "AIAA Aviation Forum 2017", (2017).
  A.87 AKBULUT BURAK,ARBERKLI FERHAT,AZGIN KIVANÇ,TEKINALP OZAN, A Simplified Model for Vibrating Mass Control Moment Gyroscope. "27th AAS/AIAA Space Flight Mechanics Meeting", (2017).
  A.88 AKBULUT BURAK,ARBERKLI FERHAT,AZGIN KIVANÇ,TEKINALP OZAN, Experimental Characterization and Validation of Vibrating Rotor Control Moment Gyroscope. "2017, AIAA SPACE and Astronautics Forum and Exposition", (2017).
  A.89 ATAS ÖMER,TEKINALP OZAN, Orbit Transfer of an Earth Orbiting Solar Sail Cubesat. "27th AAS/AIAA Space Flight Mechanics Meeting", (2017).
  A.90 BÜYÜKKOÇAK ALI TEVFIK,ALTINISIK SÜLEYMAN,TEKINALP OZAN, Constrained Model Predictive Control for Spacecraft Rendezvous. "9th Ankara International Aerospace Conference", (2017).
  A.91 Kapulu Özge,TEKINALP OZAN, Main Rotor Downwash Effect on Seperation Characteristics of External Stores. "AIAA SciTech 2017, Atmospheric Flight Mechanics Conference", (2017).
  A.92 ARBERKLI FERHAT,AKBULUT BURAK,AZGIN KIVANÇ,TEKINALP OZAN, Effects of Rotor Geometry on the Performance of Vibrating Mass Control Moment Gyroscopes. "AAS/AIAA Astrodynamics Specialist Conference", (2017).

Book and Chapter in a Book

  A.1 Tekinalp, O., Uslu Ö. and Tulunay, Y., An Attitude Control System Based on the TURKSAT-1B Geostationary Satellite. "COSPAR Colloquia Series Volume 10, Microsatellites as Research Tools", (1999), p.143-151.
  A.2 Erdal, T., Tekinalp, O. and Tulunay, Y., Minimum Fuel Station Keeping Maneuver Strategy for TURKSAT Geostationary Satellites. "Reducing the Cost of Ground Systems and Operations", (2000), p.33-40.
  A.3 Gomroki, M.M., Topputo, F., Tekinalp, O., Bernelli-Zazzera, F.,, Two ASRE Approaches with Application to Spacecraft Coulomb Formations. "Astrodynamics Network, Astrone II, Astrophysics and Space Sciences Proceedings", (2016), p.109-120.

Publications (NATIONAL)

 

Journal Papers

  A.1 Tekinalp, O., Uyduların Kontrolü. "TAI'nin Sesi", (2006), s.21-24.
  A.2 Kurtulus, D.F., Tekinalp, O., İnsansız hava araçlarına bir bakış. "Savunma Sanayii Gündemi", 2010/2, (2010), s.53-58.
 

Conference Papers

  A.1 Kutay, A.T.K., Tulunay, E., Tulunay, Y. and Tekinalp, O., Yere Eş Zamanlı Uydu İçin Yapay Sinir Ağlı Tabanlı Yörünge Tahmin Etme. "2000’li Yıllarda Uzay, Havacılık, ve Savunma Teknolojilerinin Öncelikleri Sempozyumu", 2, (1999), s.469-490.
  A.2 Tekinalp, O. and Derman, H.O., Yer Eşzamanlı Bir Uydunun Üç Eksende Denetimi. "Kayseri III. Havacılık Sempozyumu", (2000).
  A.3 Yüksel, G. and Tekinalp, O., Bir Alçak İrtifa Uydusunda Yönelme Probleminin İncelenmesi. "Kayseri III. Havacılık Sempozyumu", (2000).
  A.4 Okan, A., Çelenligil, C. and Tekinalp, O., Isıl Ağ Yönteminin Uydu Isıl Analizinde Uygulanması. "Uluslar Arasi Katılımlı 4. Kayseri Havacılık Sempozyumu", (2002), s.168-172.
  A.5 Solakoğlu, E., Tekinalp, O., ve G. Karslı, TAISAT: Askeri Keşif Gözetleme Uydusu. "3. Savunma Teknolojileri Kongresi Bildiriler Kitabi", I, (2006), s.277-289.
  A.6 Yavuzoglu, E., Tekinalp, O., Uydularda Moment Kontrol Jiroskobu Kümeleri ve Sürücü Yöntemleri. "Kayseri VI. Havacılık Sempozyumu", (2006).
  A.7 Kutlu, A., Haciyev, C., Tekinalp, O.,, Leo Uydularda Manyetometre Ölçümleri Kullanılarak Yönelim Tahmini ve LQR Kontrolü. "Kayseri VI. Havacılık Sempozyumu", (2006).
  A.8 Zeynep Çakır, Batu Demir, Ozan Tekinalp, İlkay Yavrucuk, Flight control system design and integratino for a small UAV testbed. "5th Ankara International Aerospace Conference", (2009).
  A.9 Hilal Erçin, Ozan Tekinalp, İlkay Yavrucuk, Helicopter Flight Simulation and Automatic Flight Control System Design. "5th Ankara International Aerospace Conference", (2009).
  A.10 Sinem Işık, Ozan Tekinalp, İlkay Yavrucuk, Flight control system design for an Unmanned Aircraft. "5th Ankara International Aerospace Conference", (2009).
  A.11 Çavuş, N., Tekinalp, O., Multiobjective Design of an Unmanned Combat Air Vehicle. "6th Ankara International Aerospace Conference", (2011).
  A.12 Gambin, N., Tekinalp, O., Ozgoren, M.K., Relative position control of tethered satellite formations. "6th Ankara International Aerospace Conference", (2011).
  A.13 Baran, T., Tekinalp, O., FLAP KONTROLLÜ BİR RÜZGAR TÜRBİNİ PALASININ AERODİNAMİK PARAMETRELERİNİN HESAPLAMALI AKISKALAR MEKANİĞİ KULLANARAK ELDE EDİLMESİ. "Ulusal Havacılık ve Uzay Konferansı, İstanbul", (2012).
  A.14 Mutlu T, Çosgun V. Kurtulus B., Tunca E.,Kurtulus D.F., Tekinalp O., Su Bulanıklığı Dinamiği ve Su Parametrelerini Ölçme Kabiliyeti olan İnsansız Hava Aracı Platformunun Geliştirilmesi. "UHAT 2012, I. ULUSAL HAVACILIK TEKNOLOJİSİ VE UYGULAMALARI KONGRESİ", (2012).
  A.15 Ariyibi, S. Tekinalp, O., Development of Two Nonlinear Controllers for the Control of Aircraft Formations,. "7th Ankara International Conference", (2013).
  A.16 Tekinalp, O., Prach, A., A Multiple Loop Aircraft Flight Controller Using SDRE Technique,. "7th Ankara International Conference", (2013).
  A.17 Dede, E., Tekinalp, O., External Geometry and Flight Performance Optimization of a Turbojet Propelled Air to Ground Missile,. "7th Ankara International Conference", (2013).
  A.18 Mutlu, et.al., UZAKTAN ALGILAMA AMAÇLI AMFİBİ İNSANSIZ HAVA ARACI UÇUŞ PERFORMANS VE OTOPİLOT TESTLERİ. "TMMOB Makina Mühendisleri Odası VI. Ulusal Uçak, Havacılık ve Uzay Mühendisliği Kurultayı", (2013).
  A.19 Ozten, E., Tekinalp, O., Spacecraft Attitude Determination Based on GPS Carrier Phase Measurements. "7th Ankara International Conference", (2013).
  A.20 Simsek, O., Tekinalp, O., System Identification of a UAV from Flight Test Data. ", 7th Ankara International Conference", (2013).
  A.21 Onen,A.S., Şenipek,M., Mutlu,T., Cevher,L., Güngör,O., Kurtuluş, F, Tekinalp, O., Dikey İniş ve Kalkış Yapabilen İHA'nın Pervene İtki Sistemi Rüzgar Tüneli Testleri. "3. Havacılıkta İleri Teknolojiler Konferansı", (2014).
  A.22 Önen, A.S.,Cevher, L., Mutlu, T., Uzunlar, İ.O., Kurtulus, D.F., Tekinalp, O., Konvansiyel Olarak Kalkış ve İniş Yapan bir İnsansız Hava Aracına Dikey İniş ve Kalkış Yeteneğinin Kazandırılması. "SAVTEK, 7. Savunma Teknolojileri Kongresi", (2014).
  A.23 KÖKER ABDÜLKADIR,TEKINALP OZAN, Angle Only Orbit Determination Using a Telescope System.. "9th Ankara International Aerospace Conference", (2017).
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