Metrikler
Yayın
154
Açık Erişim
38
BM Sürdürülebilir Kalkınma Amaçları
Eğitim Bilgileri
1983 - 1988
1983 - 1988Doktora
University of Michigan, College of Engineerin, Mechanical Engineering And Applied Mechanics Department, Amerika Birleşik Devletleri
1982 - 1983
1982 - 1983Yüksek Lisans
University of Michigan, College of Engineering, Mechanical Engineering and Applied Mechanics Department, Amerika Birleşik Devletleri
1976 - 1981
1976 - 1981Lisans
İstanbul Teknik Üniversitesi, Makine Fakültesi, Makine Mühendisliği Bölümü, Türkiye
Yaptığı Tezler
1988
1988Doktora
Dynamic Modeling of Drill Bit Vibrations
University Of Michigan, Mechanical Engineering And Applied Mechanics Department
Yabancı Diller
C1 İleri
C1 İleriİngilizce
Araştırma Alanları
Havacılık ve Uzay Mühendisliği
Havacılık Mühendisliği
Uzay Mühendisliği
Uçuş Bilimleri
Hava Taşıtı Sistem Teknolojileri
Görev
Uçuş Dinamiği-Kararlılık
Uçuş Kontrol Sistemleri
Uzay aracı dinamiği modelleme
Yönelim ve Yörünge Kontrol
Mühendislik ve Teknoloji
Akademik Ünvanlar / Görevler
1988 - Devam Ediyor
1988 - Devam EdiyorProf. Dr.
Orta Doğu Teknik Üniversitesi, Mühendislik Fakültesi, Havacılık Ve Uzay Mühendisliği Bölümü
Yönetimsel Görevler
2009 - 2018
2009 - 2018Bölüm Başkanı
Orta Doğu Teknik Üniversitesi, Mühendislik Fakültesi, Havacılık ve Uzay Mühendisliği Bölümü
Akademi Dışı Deneyim
2006 - Devam Ediyor
2006 - Devam EdiyorConsultant
TUSAS Aerospace Industries, TAI-TEKNOKENT, Consultant
2006 - Devam Ediyor
2006 - Devam EdiyorProfessor
METU, Aerospace Engineering Department, Professor
2005 - 2006
2005 - 2006Associate Professor (Promotion)
METU, Aerospace Engineering Department, Associate Professor (Promotion)
2005 - 2005
2005 - 2005Consultant
TUSAS Aerospace Industries, TAI-Teknokent, Consultant
1993 - 2005
1993 - 2005Associate Professor (Title)
METU, Aerospace Engineering Department, Associate Professor (Title)
1998 - 2002
1998 - 2002Group Coordinator
TUBITAK METU-BILTEN, Satellite Technologies Group, Group Coordinator
1993 - 1998
1993 - 1998Consultant
Roketsan Missile Industries, Consultant
1988 - 1993
1988 - 1993Assistant Professor
METU, Aeronautical Engineering Department, Assistant Professor
1992 - 1992
1992 - 1992Engineer
CASA Division Projectos, IDS: AFCS, Gethaffe, Madrid, Engineer
1988 - 1988
1988 - 1988Assistant
University of Michigan, Mechanical Engr. and Appl. Mech. Dep, Assistant
1986 - 1987
1986 - 1987Tutor
University of Michigan, Comprehensive Studies Programme, Tutor
1986 - 1986
1986 - 1986Lecturer
University of Michigan, Mech. Engr. and Appl. Mech. Dept., Lecturer
1984 - 1985
1984 - 1985Research Assitant
Industrial Technology Institute, Flexible Manufacturing Lab., Research Assitant
1983 - 1984
1983 - 1984Research Assistant
University of Michigan, Mechanical Engr. Applied Mech. Dept., Research Assistant
1980 - 1980
1980 - 1980Engineering Assitant
Emek Insaat, Ankara, Engineering Assitant
1979 - 1979
1979 - 1979Engineering Assistant
DUC Merkez Atolyesi, Ankara, Engineering Assistant
Yönetilen Tezler
2023
2023Doktora
LONG TERM AND SAFE CLUSTER FLYING FOR DISTRIBUTED SPACE SYSTEMS
Tekinalp O. (Danışman)
B.YAĞLIOĞLU(Öğrenci)
2022
2022Yüksek Lisans
Realtime Magnetometer Calibration for Spinning Aerospace Vehicles
Söken H. E., Tekinalp O. (Eş Danışman)
M.EFE(Öğrenci)
2022
2022Yüksek Lisans
Structured H-infinity controller design and analysis for highly maneuverable jet aircraft
TEKİNALP O. (Danışman)
S.VOLKAN(Öğrenci)
2021
2021Yüksek Lisans
Evaluation of guidance methods for a swarm of munitions
TEKİNALP O. (Danışman)
A.ALP(Öğrenci)
2021
2021Yüksek Lisans
Design of a vision-based three-axis attitude estimationalgorithm for small satellites
Söken H. E. (Eş Danışman), Tekinalp O.
M.BURAK(Öğrenci)
2021
2021Doktora
Güneş yelkenli uzay aracının elastik operasyonel konsept çerçevesinde yönelim ve yörünge kontrolü
Tekinalp O. (Danışman)
H.CAN(Öğrenci)
2020
2020Doktora
Doğal dinamik kullanılarak hale yörüngede ve dünya etrafında seyir eden uzay araçları için kol uçuşu tasarımı
TEKİNALP O. (Danışman)
A.Kutlu(Öğrenci)
2019
2019Doktora
Vibration based and miniaturizable satellite attitude actuator
Tekinalp O.
B.AKBULUT(Öğrenci)
2019
2019Yüksek Lisans
Design, development and control of a hybrid uav
Tekinalp O. (Danışman)
A.MURATOĞLU(Öğrenci)
2019
2019Yüksek Lisans
Smooth slew maneuvers of flexible spacecraft
TEKİNALP O. (Danışman)
S.ALTINIŞIK(Öğrenci)
2019
2019Yüksek Lisans
Control system design and implementation of a tilt rotor UAV
Tekinalp O. (Danışman)
L.CEVHER(Öğrenci)
2019
2019Doktora
Modeling and control of quadrotor formations carrying aslung load
Tekinalp O. (Danışman)
S.OLUMIDE(Öğrenci)
2019
2019Yüksek Lisans
Hibrit hava aracının tasarımı, modellenmesi ve kontrolü.
TEKİNALP O. (Danışman)
A.Muratoğlu(Öğrenci)
2019
2019Yüksek Lisans
Orbit determination strategy and verification for geosynchronous satellites
Tekinalp O. (Danışman)
A.KÖKER(Öğrenci)
2018
2018Yüksek Lisans
Polynomial trajectory shaping guidance algorithm for multi-missile salvo attack
TEKİNALP O. (Danışman)
N.BAŞAK(Öğrenci)
2018
2018Yüksek Lisans
Autonomous spacecraft rendezvous and docking on safe trajectories
TEKİNALP O. (Danışman)
A.TEVFİK(Öğrenci)
2017
2017Doktora
Development of state dependent factorized optimal control methods with application to spacecraft Coulomb formations
TEKİNALP O. (Danışman)
M.MEHDI(Öğrenci)
2015
2015Yüksek Lisans
Modelling and Controller Design of a VTOL Air Vehicle
Kurtuluş D. F. (Eş Danışman), Tekinalp O.
A.Sami(Öğrenci)
2015
2015Doktora
Faux riccati equation techniques for feedback control of nonlinear and time-varying systems
TEKİNALP O. (Danışman)
A.PRACH(Öğrenci)
2015
2015Yüksek Lisans
Nonlinear guidance and control of leader-follower UAV formations
TEKİNALP O. (Danışman)
S.KUMBASAR(Öğrenci)
2015
2015Yüksek Lisans
Separation simulation for helicopter external stores and generation of safe separation envelopes
TEKİNALP O. (Danışman)
Ö.KAPULU(Öğrenci)
2014
2014Yüksek Lisans
Attitude control of an earth orbiting solar sail satellite to progressively change the selected orbital element
TEKİNALP O. (Danışman)
Ö.ATAŞ(Öğrenci)
2014
2014Yüksek Lisans
System identification using flight test data
TEKİNALP O. (Danışman)
O.ŞİMŞEK(Öğrenci)
2014
2014Yüksek Lisans
Response surface based performance analysis of an air-defense missile system
TEKİNALP O. (Danışman)
K.GÜNAYDIN(Öğrenci)
2014
2014Yüksek Lisans
Yüksek by-pass oranlı turbofan motorlarının aerotermodinamik tasarımı ve optimizasyonu.
TEKİNALP O. (Danışman)
S.Arayibi(Öğrenci)
2014
2014Yüksek Lisans
Nonlinear control of unmanned aircraft formations
TEKİNALP O. (Danışman)
S.ARIYIBI(Öğrenci)
2014
2014Yüksek Lisans
Developing an investment decision methodology for helicopter systems related to technology factor and base price
TEKİNALP O. (Eş Danışman), YAVRUCUK İ. (Eş Danışman)
G.KARA(Öğrenci)
2013
2013Yüksek Lisans
Evaluation of rotorcraft system identification approaches
TEKİNALP O. (Danışman)
S.KAYMAK(Öğrenci)
2013
2013Yüksek Lisans
Satellite attitude determination based on GPS carrier phase measurements
TEKİNALP O. (Danışman)
E.ÖZTEN(Öğrenci)
2012
2012Yüksek Lisans
Conceptual design optimization of a nano-satellite launcher
TEKİNALP O. (Danışman)
Y.EMRE(Öğrenci)
2011
2011Yüksek Lisans
Development of a UAV testbed
TEKİNALP O. (Eş Danışman), YAVRUCUK İ. (Eş Danışman)
Z.ÇAKIR(Öğrenci)
2011
2011Yüksek Lisans
Control of a satellite with flexible smart beam during slew maneuver
TEKİNALP O. (Danışman)
H.ÜREK(Öğrenci)
2011
2011Yüksek Lisans
External geometry and flight performance optimization of turbojet propelled air to ground missiles
TEKİNALP O. (Danışman)
E.DEDE(Öğrenci)
2010
2010Yüksek Lisans
Development of control allocation methods for satellite attitude control
TEKİNALP O. (Eş Danışman), YAVRUCUK İ. (Eş Danışman)
T.ÇİĞDEM(Öğrenci)
2010
2010Yüksek Lisans
Flight control system design for an over actuated UAV against actuator failures
TEKİNALP O. (Danışman)
S.IŞIK(Öğrenci)
2009
2009Yüksek Lisans
Attitude control of multiple rigid body spacecraft with flexible hinge joints
TEKİNALP O. (Eş Danışman), ÖZGÖREN M. K. (Eş Danışman)
B.AKBULUT(Öğrenci)
2009
2009Yüksek Lisans
Multiobjective design optimization of rockets and missiles
TEKİNALP O. (Danışman)
M.YAVUZ(Öğrenci)
2009
2009Yüksek Lisans
Flight control of a tilt duct UAV with emphasis on the over actuated transition flight phase
TEKİNALP O. (Danışman)
T.ÜNLÜ(Öğrenci)
2009
2009Yüksek Lisans
Multidisciplinary and multiobjective design optimization of an unmanned combat aerial vehicle (UCAV)
TEKİNALP O. (Eş Danışman), YAVRUCUK İ. (Eş Danışman)
N.ÇAVUŞ(Öğrenci)
2008
2008Yüksek Lisans
Design of kalman filter based attitude determination algorithms for a leo satellite and for a satellite attitude control test setup
TEKİNALP O. (Danışman)
A.KUTLU(Öğrenci)
2008
2008Yüksek Lisans
Flight simulation and control of a helicopter
TEKİNALP O. (Danışman)
G.HİLAL(Öğrenci)
2007
2007Yüksek Lisans
Control allocation against actuator failures in overactuated small satellites
TEKİNALP O. (Danışman)
Ö.KAHRAMAN(Öğrenci)
2006
2006Yüksek Lisans
Steering of redundant robotic manipulators and spacecraft integrated power and attitude control-control moment gyroscopes
TEKİNALP O. (Danışman)
A.ALTAY(Öğrenci)
2005
2005Yüksek Lisans
Tarımsal robot uçak kavramsal tasarımı eniyilemesi
TEKİNALP O. (Danışman)
S.Özdemir(Öğrenci)
2005
2005Doktora
A layerwise approach to modeling piezolaminated plates
TEKİNALP O. (Danışman)
C.LEVENT(Öğrenci)
2005
2005Yüksek Lisans
Multi objective conceptual design optimization of an agricultural aerial robot
TEKİNALP O. (Danışman)
S.ÖZDEMİR(Öğrenci)
2004
2004Yüksek Lisans
Simulated annealing for the generation of pareto fronts with aerospace applications
TEKİNALP O. (Danışman)
G.KARSLI(Öğrenci)
2003
2003Yüksek Lisans
Steering laws for control moment gyroscope systems used in spacecrafts attitude control
TEKİNALP O. (Danışman)
E.YAVUZOĞLU(Öğrenci)
2002
2002Yüksek Lisans
Development of a flexible satellite simulator and associated control algorithms
TEKİNALP O. (Danışman)
K.TAYLAN(Öğrenci)
2001
2001Yüksek Lisans
Missile trajectory optimization using genetic algorithm
TEKİNALP O. (Danışman)
M.SOYLUOĞLU(Öğrenci)
2001
2001Yüksek Lisans
Optimization of north south station keeping manoeuvers for geostationary satellites
TEKİNALP O. (Danışman)
Z.YILDIZ(Öğrenci)
2001
2001Yüksek Lisans
Guidance and control of a spinning missile
TEKİNALP O. (Danışman)
B.SEMERCİ(Öğrenci)
2000
2000Yüksek Lisans
Neural network initalization of strapdown inertial navigation systems
TEKİNALP O. (Danışman)
M.Özemre(Öğrenci)
2000
2000Yüksek Lisans
Neural network initialization of strapdown inertial navigation systems
TEKİNALP O. (Danışman)
M.ÖZEMRE(Öğrenci)
2000
2000Yüksek Lisans
Multi-discplinary design optimization of missiles
TEKİNALP O. (Danışman)
M.Bingöl(Öğrenci)
2000
2000Yüksek Lisans
Modeling and control of a tilt-duct VTOL UAV
TEKİNALP O. (Danışman)
A.OKAN(Öğrenci)
2000
2000Yüksek Lisans
Multi-disciplinary design optimization of missiles
TEKİNALP O. (Danışman)
M.BİNGÖL(Öğrenci)
1999
1999Yüksek Lisans
Missile design optimization using simulated annealing techniue
TEKİNALP O. (Danışman)
S.UTALAY(Öğrenci)
1999
1999Yüksek Lisans
Modeling and simulation of the Türksat 1B Satellite using artificial neural networks
TULUNAY Y. (Eş Danışman), TEKİNALP O. (Eş Danışman)
A.Türker(Öğrenci)
1999
1999Yüksek Lisans
3- Axis attitude control of a geostationary satellite
TEKİNALP O. (Danışman)
H.ÖZGÜR(Öğrenci)
1999
1999Yüksek Lisans
Missile design optimization using simulated annealing technique
TEKİNALP O. (Danışman)
S.Utalay(Öğrenci)
1998
1998Yüksek Lisans
Modeling and control of beam type structures with surface bonded piezoelectric sensors and actuators
TEKİNALP O. (Eş Danışman), TULUNAY Y. (Eş Danışman)
B.Yağcı(Öğrenci)
1998
1998Yüksek Lisans
Modelling and control of beam type structures with surface bonded piezoelectric sensors and actuators
TEKİNALP O. (Danışman)
B.YAĞCI(Öğrenci)
1998
1998Yüksek Lisans
Investigation of minimum fuel maneuvers of Türksat 1B satellite with possible use of its simulator
TULUNAY Y. (Eş Danışman), TEKİNALP O. (Eş Danışman)
T.Erdal(Öğrenci)
1998
1998Yüksek Lisans
Robust control of a highly maneuverable aircraft
TEKİNALP O. (Danışman)
M.ERGÜN(Öğrenci)
1997
1997Yüksek Lisans
Orbit dynamics, attitude dynamics and control: Investigation into possible applications to TURKSAT
TEKİNALP O. (Danışman)
H.ÖZGE(Öğrenci)
1997
1997Yüksek Lisans
Orbit dynamics attitude dynamics and control:Investigation into possible applications to Türksat
TEKİNALP O. (Eş Danışman), TULUNAY Y. (Eş Danışman)
H.Özge(Öğrenci)
1996
1996Yüksek Lisans
Optimal trajectories for air-to-surface missiles using direct collocation and nonlinear programming
TEKİNALP O. (Danışman)
E.MURAT(Öğrenci)
1996
1996Yüksek Lisans
Optimal trajectories for air-tosurfaces missiles using direct collocation and nonlinear programming
TEKİNALP O. (Danışman)
E.Murat(Öğrenci)
1992
1992Yüksek Lisans
Free vibration analysis of multi-layer adhesively bonded rotating beams
TEKİNALP O. (Danışman)
A.KADİR(Öğrenci)
1992
1992Yüksek Lisans
Free vibration analysis of adhesively bonded multi-layer beams and lap-joints
TEKİNALP O. (Danışman)
N.ÇAĞLAYAN(Öğrenci)
Makaleler
Tümü (21)
SCI-E, SSCI, AHCI (13)
SCI-E, SSCI, AHCI, ESCI (14)
ESCI (1)
Scopus (19)
Diğer Yayınlar (2)
2025
20251. Trajectory tracking controller design and simulation of a tethered aircraft
Onen A. S., TEKİNALP O.
CEAS AERONAUTICAL JOURNAL
, 2025 (ESCI, Scopus)
2025
20252. Visual Navigation for Lunar Missions Using Sequential Triangulation Technique
Muratoğlu A., Soken H. E., Tekinalp O.
ENGINEERING PROCEEDINGS , cilt.90, sa.1, ss.27-36, 2025 (Scopus)
2023
20233. 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, Scopus)
2021
20214. 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, Scopus)
2021
20215. 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)
2021
20216. 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)
2020
20207. 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, Scopus)
2018
20188. 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, Scopus)
2018
20189. 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, Scopus)
2015
201510. 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, Scopus)
2007
200711. 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)
2005
200512. 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, Scopus)
2005
200513. 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)
2004
200414. 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)
2004
200415. 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)
2000
200016. Turkish Small Satellite Program: Goals and policies
Askar M., Tekinalp O.
ACTA ASTRONAUTICA
, cilt.46, ss.375-378, 2000 (SCI-Expanded, Scopus)
1996
199617. 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)
1990
199018. 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)
1989
198919. 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)
1988
198820. 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)
1984
198421. 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
2025
20251. 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)
2024
20242. 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)
2022
20223. 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)
2022
20224. 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)
2021
20215. 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)
2021
20216. 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)
2021
20217. 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)
2020
20208. 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)
2021
20219. 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)
2020
202010. 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)
2020
202011. 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)
2020
202012. 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)
2020
202013. 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)
2020
202014. 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)
2019
201915. 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, (Tam Metin Bildiri)
2020
202016. 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, (Tam Metin Bildiri)
2019
201917. 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)
2019
201918. 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)
2019
201919. 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)
2019
201920. 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)
2019
201921. 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)
2019
201922. 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)
2019
201923. 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)
2019
201924. 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)
2019
201925. 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, (Tam Metin Bildiri)
2019
201926. 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, (Tam Metin Bildiri)
2019
201927. 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)
2019
201928. 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)
2019
201929. 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)
2018
201830. 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)
2018
201831. 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)
2018
201832. 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)
2018
201833. 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)
2018
201834. 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)
2018
201835. 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)
2017
201736. 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)
2018
201837. 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, (Tam Metin Bildiri)
2018
201838. 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)
2017
201739. Angle Only Orbit Determination Using a Telescope System
KÖKER A., TEKİNALP O.
9th Ankara International Aerospace Conference, 20 - 22 Eylül 2017, (Tam Metin Bildiri)
2017
201740. 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)
2017
201741. 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, (Tam Metin Bildiri)
2017
201742. 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)
2017
201743. 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, (Tam Metin Bildiri)
2017
201744. 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)
2017
201745. 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)
2017
201746. 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)
2017
201747. 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)
2016
201648. 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)
2016
201649. 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)
2016
201650. 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, (Tam Metin Bildiri)
2016
201651. 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)
2016
201652. 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)
2016
201653. 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)
2016
201654. 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, (Tam Metin Bildiri)
2016
201655. 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)
2016
201656. 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)
2016
201657. 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)
2015
201558. 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)
2015
201559. 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)
2015
201560. 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)
2015
201561. 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)
2015
201562. 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)
2015
201563. 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)
2015
201564. 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)
2015
201565. 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)
2015
201566. 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)
2015
201567. 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)
2015
201568. 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)
2015
201569. 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, (Tam Metin Bildiri)
2015
201570. 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)
2015
201571. 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, (Tam Metin Bildiri)
2015
201572. 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)
2015
201573. 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)
2015
201574. 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)
2015
201575. 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)
2015
201576. 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)
2015
201577. 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, (Tam Metin Bildiri)
2014
201478. 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)
2015
201579. 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)
2014
201480. 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, (Tam Metin Bildiri)
2014
201481. 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, (Tam Metin Bildiri)
2014
201482. 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)
2014
201483. 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)
2014
201484. 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, (Tam Metin Bildiri)
2014
201485. 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, (Tam Metin Bildiri)
2014
201486. 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, (Tam Metin Bildiri)
2013
201387. 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, (Tam Metin Bildiri)
2013
201388. 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, (Tam Metin Bildiri)
2013
201389. 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, (Tam Metin Bildiri)
2013
201390. 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, (Tam Metin Bildiri)
2013
201391. 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, (Tam Metin Bildiri)
2012
201292. 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, (Tam Metin Bildiri)
2012
201293. 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, (Tam Metin Bildiri)
2011
201194. Fault Tolerant Control of an Over Actuated UAV
TEKİNALP O., YAVRUCUK İ.
AIAAGuidance, Navigation, and Control Conference, 8 - 11 Temmuz 2011, (Tam Metin Bildiri)
2011
201195. 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, (Tam Metin Bildiri)
2011
201196. 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, (Tam Metin Bildiri)
2010
201097. 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, (Tam Metin Bildiri)
2010
201098. 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, (Tam Metin Bildiri)
2010
201099. 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, (Tam Metin Bildiri)
2010
2010100. 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, (Tam Metin Bildiri)
2009
2009101. Helicopter Flight Simulation and Automatic Flight Control System Design
TEKİNALP O., YAVRUCUK İ.
AIAC 2009, 17 - 19 Ağustos 2009, (Tam Metin Bildiri)
2009
2009102. Flight Control System Design and Integration for a Small UAV Test Bed
TEKİNALP O., YAVRUCUK İ.
AIAC 2009, 17 - 19 Ağustos 2009, (Tam Metin Bildiri)
2009
2009103. 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, (Tam Metin Bildiri)
2009
2009104. 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, (Tam Metin Bildiri)
2009
2009105. 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, (Tam Metin Bildiri)
2009
2009106. 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, (Tam Metin Bildiri)
2009
2009107. 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, (Tam Metin Bildiri)
2007
2007108. 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, (Tam Metin Bildiri)
2005
2005109. 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, (Tam Metin Bildiri)
2005
2005110. 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, (Tam Metin Bildiri)
2003
2003111. 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, (Tam Metin Bildiri)
2002
2002112. 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, (Tam Metin Bildiri)
2002
2002113. 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, (Tam Metin Bildiri)
2002
2002114. 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, (Tam Metin Bildiri)
2001
2001115. 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, (Tam Metin Bildiri)
2001
2001116. 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, (Tam Metin Bildiri)
2000
2000117. 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, (Tam Metin Bildiri)
1999
1999118. 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, (Tam Metin Bildiri)
1999
1999119. 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, (Tam Metin Bildiri)
1997
1997120. 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, (Tam Metin Bildiri)
1997
1997121. 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, (Tam Metin Bildiri)
1997
1997122. 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, (Tam Metin Bildiri)
1995
1995123. 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, (Tam Metin Bildiri)
1994
1994124. 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, (Tam Metin Bildiri)
1994
1994125. 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, (Tam Metin Bildiri)
1993
1993126. 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, (Tam Metin Bildiri)
1993
1993127. 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, (Tam Metin Bildiri)
1990
1990128. 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, (Tam Metin Bildiri)
1989
1989129. 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, (Tam Metin Bildiri)
1988
1988130. 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, (Tam Metin Bildiri)
1985
1985131. 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, (Tam Metin Bildiri)
Desteklenen Projeler
2017 - 2024
2017 - 2024ODTÜ-TAİ VLA projesi 1. faz
Şirket
(Proje Özeti)
Kurtuluş D. F., Tekinalp O. (Yürütücü), Kayran A., Yaman Y., Gürses E., Çöker D., et al.
2015 - 2020
2015 - 2020Titreşim Temelli Uydu Yönelim Denetimi Eyleyicisi Kavramsal Doğrulaması
TÜBİTAK Projesi , 1001 - Bilimsel ve Teknolojik Araştırma Projelerini Destekleme Programı
(Proje Özeti)
Tekinalp O. (Yürütücü), Azgın K.
2019 - 2019
2019 - 2019Küçük Otonom İnsansız Hava Aracı Geliştirme Projesi (KO-İHA)
Diğer Özel Kurumlarca Desteklenen Proje
Tekinalp O. (Yürütücü), Kurtuluş D. F., Yaman Y., Şahin M., Sezer Uzol N., Ciğeroğlu E., et al.
2016 - 2017
2016 - 2017Orta Doğu Teknik Üniversitesi Ar-Ge Strateji Belgesi (Havacılık Ve Uzay)
TÜBİTAK Projesi , 1000 - Üniversitelerin Araştırma ve Geliştirme Potansiyelinin Arttırılmasına Yönelik Destek Programı
Zeyrek M. T., Tekinalp O.
2016 - 2017
2016 - 2017Orta Dou Teknik Üniversitesi Ar-Ge Strateji Belgesi (Havacılık Ve Uzay)
TÜBİTAK Projesi
TEKİNALP O. (Yürütücü), LELOĞLU U. M.
2016 - 2016
2016 - 2016ODTÜ Havacılık ve Uzay Mühendisliği Bölümünden Eğitim Hizmeti Alınması
Diğer Özel Kurumlarca Desteklenen Proje
TEKİNALP O. (Yürütücü), YAMAN Y.
2016 - 2016
2016 - 2016Airbus A350 XWB uçağı A350 1000 serisi kanatçıkların ARGE falliyetinin incelenmesi
Diğer Özel Kurumlarca Desteklenen Proje
TEKİNALP O. (Yürütücü)
2014 - 2016
2014 - 2016Birlikte Sarkan Yük Tasıyan Kol Uçusundaki Quadrotorların Modellenmesi Ve Kontrolü
TÜBİTAK Projesi
TEKİNALP O. (Yürütücü)
Etkinlik Organizasyonlarındaki Görevler
Ekim 2019
Ekim 2019VTOL Aircraft Competition, Dikine Kalkan İnsansız Hava Araçları Yarışması
Sosyal Faaliyet Organizasyonu
Tekinalp O., Kutay A. T., Perçin M.
Ankara, Türkiye
Ekim 2018
Ekim 2018METU VTOL Aircraft Competetion 2
Sosyal Faaliyet Organizasyonu
Tekinalp O., Perçin M., Kutay A. T.
Ankara, Türkiye
Ödüller
Eylül 2019
Eylül 2019ODTÜ-Tusaş Çok Hafif Uçak (Very Light Aircraft (VLA)) Tasarım ve Geliştirme
Yüksek Öğretim Kurumu