Jafar Roshanian

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	전체	2020년 이후
서지정보	1713	756
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Masoud EbrahimiAssociate Prof. of Aerospace Engineering, Tarbiat Modares Universitymodares.ac.ir의 이메일 확인됨
Ali Asghar BatalebluFree University of Bozen-Bolzanounibz.it의 이메일 확인됨
Abdol Majid KhoshnoodK. N. Toosi University of Technologykntu.ac.ir의 이메일 확인됨
Professor Mohsen BahramiAmirkabir University of Technologyaut.ac.ir의 이메일 확인됨
Amir Ali Nikkhahprofessor of aerospace engineering, K.N. Toosi University of technologykntu.ac.ir의 이메일 확인됨
Behrouz EbrahimiEngineering Managerhalliburton.com의 이메일 확인됨
Ali Khaki SedighProf of Control Systems at K. N. Toosi University of Technology, APAC Research Groupkntu.ac.ir의 이메일 확인됨
Mehran ZarehARSControl group, University of Modena and Reggio Emilia, Italy.daikineurope.com의 이메일 확인됨
Alireza ‌BASOHBAT NOVINZADEHAerospace of Eng. Associate of Professor, K.N. Toosi University of Technologykntu.ac.ir의 이메일 확인됨
Seyed M.Mehdi Hassani.NMcMaster Univeristymcmaster.ca의 이메일 확인됨
Hamed Afshari, PhDMcMaster Universitymcmaster.ca의 이메일 확인됨
A.A.JafariProfessor of Mechanical Engeenring, KNTU Universitykntu.ac.ir의 이메일 확인됨
Ali GhaffariProfessor of mechanical engineering, K. N. Toosi University of Technologykntu.ac.ir의 이메일 확인됨
Masoud Mirzaeik.n.toosi university of technologykntu.ac.ir의 이메일 확인됨
Mehran MirshamsAssociate Professor of K.N. Toosi University of Technologykntu.ac.ir의 이메일 확인됨
Mehdi MoghadasianPh.D, Aerospace Engineering, KNToosi Universitymail.kntu.ac.ir의 이메일 확인됨
mahdi mortazaviUniversity of Isfahan/ Amirkabir University of Technologyeng.ui.ac.ir의 이메일 확인됨
M.R. Jahed-MotlaghIran University of Science and Technologyiust.ac.ir의 이메일 확인됨
Farid NajafiProfessor of Mechanical Engineering, University of Guilanguilan.ac.ir의 이메일 확인됨
Ehsan TaheriAssistant Professor, Auburn Universityauburn.edu의 이메일 확인됨

팔로우

Jafar Roshanian

K. N. Toosi University of Technology , Professor of Aerospace Engineering

kntu.ac.ir의 이메일 확인됨 - 홈페이지

Flight Dynamics and Control Design Optimization


제목 서지정보순 정렬 연도순 정렬 제목순 정렬	인용 인용	연도
Optimal sliding-mode guidance with terminal velocity constraint for fixed-interval propulsive maneuvers B Ebrahimi, M Bahrami, J Roshanian Acta Astronautica 62 (10-11), 556-562, 2008	129	2008
Aerospace launch vehicle control: an intelligent adaptive approach AR Mehrabian, C Lucas, J Roshanian Aerospace Science and technology 10 (2), 149-155, 2006	114	2006
Configurations, flight mechanisms, and applications of unmanned aerial systems: A review S Darvishpoor, J Roshanian, A Raissi, M Hassanalian Progress in Aerospace Sciences 121, 100694, 2020	88	2020
Latin hypercube sampling applied to reliability-based multidisciplinary design optimization of a launch vehicle J Roshanian, M Ebrahimi Aerospace Science and Technology 28 (1), 297-304, 2013	88	2013
Optimal redundant sensor configuration for accuracy and reliability increasing in space inertial navigation systems M Jafari, J Roshanian The journal of navigation 66 (2), 199-208, 2013	54	2013
Multidisciplinary design of a small satellite launch vehicle using particle swarm optimization M Ebrahimi, MR Farmani, J Roshanian Structural and Multidisciplinary Optimization 44, 773-784, 2011	48	2011
Model reference adaptive control for a flexible launch vehicle A Khoshnood, J Roshanian, A Khaki-Sedig Proceedings of the Institution of Mechanical Engineers, Part I: Journal of …, 2008	46	2008
An optimal guidance law applied to quadrotor using LQR method H Jafari, M Zareh, J Roshanian, A Nikkhah Transactions of the Japan Society for Aeronautical and Space Sciences 53 …, 2010	43	2010
Multidisciplinary design optimization of a small solid propellant launch vehicle using system sensitivity analysis J Jodei, M Ebrahimi, J Roshanian Structural and Multidisciplinary Optimization 38, 93-100, 2009	43	2009
Effect of variable selection on multidisciplinary design optimization: a flight vehicle example J Roshanian, Z Keshavarz Chinese Journal of Aeronautics 20 (1), 86-96, 2007	37	2007
Skid-to-turn missile autopilot design using scheduled eigenstructure assignment technique AR Mehrabian, J Roshanian Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2006	34	2006
Flutter of wings involving a locally distributed flexible control surface S Mozaffari-Jovin, RD Firouz-Abadi, J Roshanian Journal of Sound and Vibration 357, 377-408, 2015	33	2015
Monte Carlo simulation of stage separation dynamics of a multistage launch vehicle J Roshanian, M Talebi Applied Mathematics and Mechanics 29, 1411-1426, 2008	33	2008
A novel concept of VTOL bi-rotor UAV based on moving mass control S Darvishpoor, J Roshanian, M Tayefi Aerospace Science and Technology 107, 106238, 2020	32	2020
Star identification based on euclidean distance transform, voronoi tessellation, and k-nearest neighbor classification J Roshanian, S Yazdani, M Ebrahimi IEEE Transactions on Aerospace and Electronic Systems 52 (6), 2940-2949, 2016	30	2016
Implementation of an intelligent adaptive controller for an electrohydraulic servo system based on a brain mechanism of emotional learning A Sadeghieh, J Roshanian, F Najafi International Journal of Advanced Robotic Systems 9 (3), 84, 2012	30	2012
Determination of nonlinear optimal feedback law for satellite injection problem using neighboring optimal control HH Afshari, AB Novinzadeh, J Roshanian American Journal of Applied Sciences 6 (3), 430, 2009	28	2009
Inertial navigation accuracy increasing using redundant sensors M Jafari, J Roshanian Journal of Science and Engineering 1 (1), 55-66, 2013	26	2013
Multidisciplinary design optimization approach to conceptual design of a LEO earth observation microsatellite A Ravanbakhsh, M Mortazavi, J Roshanian SpaceOps 2008 Conference, 3259, 2008	24	2008
Robust ascent trajectory design and optimization of a typical launch vehicle J Roshanian, AA Bataleblu, M Ebrahimi Proceedings of the Institution of Mechanical Engineers, Part C: Journal of …, 2018	22	2018

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