Ozan Tekinalp 个人学术档案

引用次数

	总计	2019 年至今
引用	1018	326
h 指数	18	9
i10 指数	25	7

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合著作者

Anna PrachMiddle East Technical University, Northern Cyprus Campus在 metu.edu.tr 的电子邮件经过验证
A. Galip UlsoyDistinguished University Prof. Emeritus of Mechanical Engineering, Univ. of Michigan, Ann Arbor在 umich.edu 的电子邮件经过验证
Dilek Funda KurtulusMiddle East Technical University在 metu.edu.tr 的电子邮件经过验证
Dennis S. BernsteinAerospace Engineering Department, University of Michigan在 umich.edu 的电子邮件经过验证
Mehmet Şerif KavsaoğluEskişehir Teknik Üniversitesi在 eskisehir.edu.tr 的电子邮件经过验证
Ali Turker KutayMETU Aerospace Engineering在 metu.edu.tr 的电子邮件经过验证
Murat ŞenipekPhD Candidate at Middle East Technical University Aerospace Engineering在 metu.edu.tr 的电子邮件经过验证
Anıl Sami ÖnenMiddle East Technical University在 metu.edu.tr 的电子邮件经过验证
KIVANÇ AZGINMIDDLE EAST TECHNICAL UNIVERSITY在 metu.edu.tr 的电子邮件经过验证
Derya KayaMiddle East Technical University在 metu.edu.tr 的电子邮件经过验证
Sharmila KayasthaRMIT University在 rmit.edu.au 的电子邮件经过验证
Ali Tevfik BuyukkocakUniversity of Minnesota在 umn.edu 的电子邮件经过验证
Bedri KurtulusAssoc.Prof., Mugla Sıtkı Koçman University在 mu.edu.tr 的电子邮件经过验证
sarper kumbasarMiddle East Technical University在 metu.edu.tr 的电子邮件经过验证
Metehan YaylaEsen System Integration Ltd Co在 metu.edu.tr 的电子邮件经过验证
Ismail UzunlarTOBB University of Economics and Technology在 etu.edu.tr 的电子邮件经过验证
Murat OzemreNAUTILICA DIGITAL SERVICES在 nautilica.com 的电子邮件经过验证
Daniel ChoukrounSenior Lecturer (Assistant Professor) Mechanical Engineering Dept. Ben-Gurion University在 bgu.ac.il 的电子邮件经过验证
Yurdanur TulunayPlease Note that: For such a long time my e-address has been:” [email protected] “在 ae.metu.edu.tr 的电子邮件经过验证
Abdulkadir KokerTübitak Uzay在 tubitak.gov.tr 的电子邮件经过验证

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Ozan Tekinalp

Middle East Technical University, Department of Aerospace Engineering

在 metu.edu.tr 的电子邮件经过验证 - 首页

flight mechanics guidance and control mechanical vibrations optimization of aerospace vehicles


标题按引用次数排序按年份排序按标题排序	引用次数引用次数	年份
Modeling and finite element analysis of drill bit vibrations O Tekinalp, AG Ulsoy	102	1989
Effects of geometric and process parameters on drill transverse vibrations O Tekinalp, AG Ulsoy	73	1988
Free bending vibrations of adhesively bonded orthotropic plates with a single lap joint U Yuceoglu, F Toghi, O Tekinalp	60	1996
Simulated annealing for missile optimization: Developing method and formulation techniques O Tekinalp, M Bingol Journal of guidance, control, and dynamics 27 (4), 616-626, 2004	44	2004
Quaternion-based nonlinear attitude control of quadrotor formations carrying a slung load SO Ariyibi, O Tekinalp Aerospace Science and Technology 105, 105995, 2020	43	2020
A new steering law for redundant control moment gyroscope clusters O Tekinalp, E Yavuzoglu Aerospace science and technology 9 (7), 626-634, 2005	42	2005
Tilt duct vertical takeoff and landing uninhabited aerial vehicle concept design study O Armutcuoglu, MS Kavsaoglu, O Tekinalp Journal of aircraft 41 (2), 215-223, 2004	39	2004
A new multiobjective simulated annealing algorithm O Tekinalp, G Karsli Journal of Global Optimization 39, 49-77, 2007	36	2007
Modeling and controller design of a VTOL UAV AS Onen, L Cevher, M Senipek, T Mutlu, O Gungor, IO Uzunlar, ... 2015 International Conference on Unmanned Aircraft Systems (ICUAS), 329-337, 2015	33	2015
A layerwise approach to piezo-electric plates accounting for adhesive flexibility and delaminated regions CL Erturk, O Tekinalp Computers & structures 83 (4-5), 279-296, 2005	31	2005
Artificial neural networks for transfer aligment and calibration of inertial navigation systems O Tekinalp, M Ozemre AIAA Guidance, Navigation, and Control Conference and Exhibit, 4406, 2001	31	2001
A numerical comparison of frozen-time and forward-propagating Riccati equations for stabilization of periodically time-varying systems A Prach, O Tekinalp, DS Bernstein 2014 American Control Conference, 5633-5638, 2014	25	2014
Simulation and flight control of a tilt duct uav O Tekinalp, T Unlu, I Yavrucuk AIAA Modeling and Simulation Technologies Conference, 6138, 2009	22	2009
Dynamic modeling of transverse drill bit vibrations AG Ulsoy, O Tekinalp, E Lenz CIRP Annals 33 (1), 253-258, 1984	21	1984
Development of a state dependent riccati equation based tracking flight controller for an unmanned aircraft A Prach, O Tekinalp Proc. AIAA Guidance, Navigation, and Control Conference, Boston, MA, 51-67, 2013	20	2013
Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data A Kutlu, C Haciyev, O Tekinalp 2007 3rd International Conference on Recent Advances in Space Technologies …, 2007	20	2007
Simulated annealing for missile trajectory planning and multidisciplinary missile design optimization O Tekinalp, S Utalay 38th Aerospace Sciences Meeting and Exhibit, 684, 2000	19	2000
Flight control of a tilt-duct UAV A Okan, O Tekinalp, M Kavsaoglu 1st UAV Conference, 3466, 2002	18	2002
Infinite-horizon linear-quadratic control by forward propagation of the differential Riccati equation [lecture notes] A Prach, O Tekinalp, DS Bernstein IEEE Control Systems Magazine 35 (2), 78-93, 2015	16	2015
Flight mechanics analysis of a tilt-rotor UAV A Okan, O Tekinalp, M Kavsaoglu, O Armutcuoglu, E Tulunay 24th Atmospheric Flight Mechanics Conference, 4255, 1999	15	1999

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