Prof. Dr. OZAN TEKİNALP

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

JOURNAL OF VIBRATION AND CONTROL , cilt.24, sa.7, ss.1239-1263, 2018 (SCI-Expanded, Scopus)

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

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS , cilt.41, sa.3, ss.618-631, 2018 (SCI-Expanded, Scopus)

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

Tekinalp O., Yavuzoglu E.

IEEE CONTROL SYSTEMS MAGAZINE , cilt.35, sa.2, ss.78-93, 2015 (SCI-Expanded, Scopus)

11. A new multiobjective simulated annealing algorithm

Tekinalp O., Karsli G.

JOURNAL OF GLOBAL OPTIMIZATION , cilt.39, sa.1, ss.49-77, 2007 (SCI-Expanded, Scopus)

12. A new steering law for redundant control moment gyroscope clusters

AEROSPACE SCIENCE AND TECHNOLOGY , cilt.9, sa.7, ss.626-634, 2005 (SCI-Expanded, Scopus)

13. 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, Scopus)

14. 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, Scopus) Sürdürülebilir Kalkınma

15. 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, Scopus)

16. Turkish Small Satellite Program: Goals and policies

Askar M., Tekinalp O.

ACTA ASTRONAUTICA , cilt.46, ss.375-378, 2000 (SCI-Expanded, Scopus)

17. 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, Scopus)

18. 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)

19. 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)

20. 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)

21. 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)

Hakemli Bilimsel Toplantılarda Yayımlanmış Bildiriler 131

1. A Robust Nonlinear MPC and Incremental Dynamic Inversion Control Framework for Quadrotors Under Rotor Failure

Elif C. M., TEKİNALP O.

12th IEEE International Workshop on Metrology for AeroSpace, MetroAeroSpace 2025, Naples, İtalya, 18 - 20 Haziran 2025, ss.274-279, (Tam Metin Bildiri)

2. Visual Navigation for Lunar Missions Using Sequential Triangulation Technique

MURATOĞLU A., SÖKEN H. E., TEKİNALP O.

14th EASN International Conference, Yunanistan, 8 - 11 Ekim 2024, (Tam Metin Bildiri)

3. 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, (Tam Metin Bildiri)

4. 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, (Özet Bildiri)

5. 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, (Tam Metin Bildiri)

6. 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, (Tam Metin Bildiri)

7. 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, (Özet Bildiri) Sürdürülebilir Kalkınma

8. 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, (Tam Metin Bildiri)

9. 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, (Tam Metin Bildiri)

10. 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, (Tam Metin Bildiri)

11. 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, (Tam Metin Bildiri)

12. 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, (Tam Metin Bildiri)

13. 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, (Tam Metin Bildiri)

14. 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, (Tam Metin Bildiri)

15. Oscillating Control Moment Gyroscope Mathematical Model Development, Verification and Results

Güzel M. B., Söken H. E., Tekinalp O.

International Symposium on Space Technology and Science, Fukui, Japonya, 15 - 21 Haziran 2019, (Tam Metin Bildiri)

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

71st International Astronautical Congress, IAC 2020, Virtual, Online, 12 - 14 Ekim 2020, cilt.2020-October, (Tam Metin Bildiri)

17. 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, (Tam Metin Bildiri)

18. 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, (Tam Metin Bildiri)

19. INCORPORATING REAL LIFE DESIGN PROBLEMS INTO THE AEROSPACE CURRICULUM

TEKİNALP O.

10TH ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 18 - 20 Eylül 2019, (Tam Metin Bildiri)

20. 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, (Tam Metin Bildiri)

21. 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, (Tam Metin Bildiri)

22. 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, (Tam Metin Bildiri)

23. 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, (Tam Metin Bildiri)

24. 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, (Tam Metin Bildiri)

25. Oscillating Control Moment Gyroscope Experimental Results

TEKİNALP O., BÜYÜKKOÇAK A. T.

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

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

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

27. 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, (Tam Metin Bildiri)

28. 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, (Tam Metin Bildiri)

29. 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, (Tam Metin Bildiri) Sürdürülebilir Kalkınma

30. 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, (Tam Metin Bildiri)

31. 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, (Tam Metin Bildiri)

32. 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, (Tam Metin Bildiri)

33. 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, (Tam Metin Bildiri)

34. 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, (Tam Metin Bildiri)

35. 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, (Tam Metin Bildiri)

36. 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, (Tam Metin Bildiri)

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

Yaglioglu B., AtaÅŸ Ã., Kahraman D., KÃ¶se S., Koru A., TEKİNALP O., et al.

69th International Astronautical Congress: #InvolvingEveryone, IAC 2018, Bremen, Almanya, 1 - 05 Ekim 2018, cilt.2018-October, (Tam Metin Bildiri)

38. 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, (Tam Metin Bildiri)

39. Angle Only Orbit Determination Using a Telescope System

KÖKER A., TEKİNALP O.

9th Ankara International Aerospace Conference, 20 - 22 Eylül 2017, (Tam Metin Bildiri)

40. Constrained Model Predictive Control for Spacecraft Rendezvous

BÜYÜKKOÇAK A. T., ALTINIŞIK S., TEKİNALP O.

9th Ankara International Aerospace Conference, 20 - 22 Eylül 2017, (Tam Metin Bildiri)

41. Experimental Characterization and Validation of Vibrating Rotor Control Moment Gyroscope

KAYA D. D., KUTAY A. T., TEKİNALP O.

AIAA SPACE and Astronautics Forum and Exposition, Orlando, FL, Amerika Birleşik Devletleri, 12 - 14 Eylül 2017, (Tam Metin Bildiri)

42. 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, (Tam Metin Bildiri)

43. 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)

44. 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, (Tam Metin Bildiri)

45. 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, (Tam Metin Bildiri)

46. 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, (Tam Metin Bildiri)

47. 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, (Tam Metin Bildiri)

48. A Novel Flight Control Algorithm for Multicopters

TEKİNALP O., Kumbasar S.

30th Congress of International Council of Aeronautical Sciences, 26 - 29 Eylül 2016, (Tam Metin Bildiri)

49. 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, (Tam Metin Bildiri)

50. Vibrating Mass Control Moment Gyroscope Dynamic Model Validation

PRACH A., TEKİNALP O., Bernstein D. S.

AIAA/AAS Astrodynamics Specialist Conference, Long Beach, California, Amerika Birleşik Devletleri, 13 - 16 Eylül 2016, (Tam Metin Bildiri)

51. 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, (Tam Metin Bildiri)

52. 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, (Tam Metin Bildiri)

53. 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, (Tam Metin Bildiri)

54. Nonlinear aircraft flight control using the forward propagating riccati equation

AIAA Guidance, Navigation, and Control Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016, (Tam Metin Bildiri)

55. 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, (Tam Metin Bildiri)

56. 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, (Tam Metin Bildiri)

57. 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, (Tam Metin Bildiri)

58. 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, (Tam Metin Bildiri)

59. 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, (Tam Metin Bildiri)

60. 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, (Tam Metin Bildiri)

61. 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, (Tam Metin Bildiri)

62. 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, (Tam Metin Bildiri)

63. 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, (Tam Metin Bildiri)

64. 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, (Tam Metin Bildiri)

65. 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, (Tam Metin Bildiri)

66. 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, (Tam Metin Bildiri)

67. 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, (Tam Metin Bildiri)

68. 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, (Tam Metin Bildiri)

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

TEKİNALP O., MOHAMMAD MEHDI G.

70. 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, (Tam Metin Bildiri)

71. State Dependent Riccati Equation Control of Spinning Three Craft Coulomb Formations

AIAA/AAS space Flight Mechanics Meeting, Williamsburg, Virginia, Amerika Birleşik Devletleri, 12 - 15 Ocak 2015, (Tam Metin Bildiri)

72. 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, (Tam Metin Bildiri)

73. 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, (Tam Metin Bildiri)

74. Nonlinear Guidance of Aircraft Formations

TEKİNALP O., Segun A.

AIAA SciTech 2015 Konferansi, Orlando, Florida, Amerika Birleşik Devletleri, 5 - 09 Ocak 2015, (Tam Metin Bildiri)

75. 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, (Tam Metin Bildiri)

76. 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, (Tam Metin Bildiri)

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

AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015, Florida, Amerika Birleşik Devletleri, 5 - 09 Ocak 2015, (Tam Metin Bildiri)

78. 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, (Tam Metin Bildiri)

79. 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, (Tam Metin Bildiri)

80. 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, (Tam Metin Bildiri)

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

Choukroun D., TEKİNALP O.

American Control Conference, Oregon, Amerika Birleşik Devletleri, 4 - 06 Aralık 2014, ss.5633-5638, (Tam Metin Bildiri)

82. 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, (Tam Metin Bildiri)

83. 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, (Tam Metin Bildiri)

84. Performance evaluation of sdre-based spacecraft attitude estimation and control

54th Israel Annual Conference on Aerospace Sciences, IACAS 2014, Tel-Aviv and Haifa, İsrail, 19 - 20 Şubat 2014, cilt.1, ss.609-634, (Tam Metin Bildiri)

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

24th AAS/AIAA Space Flight Mechanics Meeting, 2014, Mexico, Amerika Birleşik Devletleri, 26 - 30 Ocak 2014, cilt.152, ss.235-254, (Tam Metin Bildiri)

86. Maneuvering of two-craft coulomb formation using ASRE method