Amit Sanyal

Dikutip oleh

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36 artikel

5 artikel

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Dennis S. BernsteinAerospace Engineering Department, University of MichiganEmail yang diverifikasi di umich.edu
Melvin LeokProfessor of Mathematics, University of California, San DiegoEmail yang diverifikasi di ucsd.edu
Taeyoung LeeProfessor, Mechanical and Aerospace Engineering, George Washington UniversityEmail yang diverifikasi di gwu.edu
Ilya KolmanovskyProfessor of Aerospace Engineering, University of MichiganEmail yang diverifikasi di umich.edu
Dr. Frederick A. LeveAir Force Office of Scientific ResearchEmail yang diverifikasi di us.af.mil
Carlos SilvestreUniversity of Macau, on leave from the Institute for Systems and Robotics (ISR/IST), LARSySEmail yang diverifikasi di um.edu.mo
Sérgio BrásEuropean Space AgencyEmail yang diverifikasi di esa.int
Ambarish GoswamiDirector, System Analyst, Intuitive SurgicalEmail yang diverifikasi di ambarish.com
Avishai WeissSenior Principal Research Scientist, Mitsubishi Electric Research LaboratoriesEmail yang diverifikasi di merl.com
Ryan N. SmithAssociate Professor, Fort Lewis CollegeEmail yang diverifikasi di fortlewis.edu
Trevor C. SorensenSpecialist, University of Hawaii at ManoaEmail yang diverifikasi di hsfl.hawaii.edu
benjamin shapiroProfessor of Bioengineering, Institute for Systems Research, University of Maryland at College ParkEmail yang diverifikasi di umd.edu
Adrian SanduVirginia TechEmail yang diverifikasi di vt.edu
Christopher E. CarrAssistant Professor, Georgia Institute of TechnologyEmail yang diverifikasi di gatech.edu

Ikuti

Amit Sanyal

Associate Professor, Mechanical and Aerospace Engineering, Syracuse University

Email yang diverifikasi di syr.edu - Beranda

geometric mechanics geometric and nonlinear control nonlinear observer design


Judul Urutkan menurut kutipan Urutkan menurut tahun Urutkan menurut judul	Dikutip oleh Dikutip oleh	Tahun
Rigid-body attitude control NA Chaturvedi, AK Sanyal, NH McClamroch IEEE control systems magazine 31 (3), 30-51, 2011	814	2011
Inertia-free spacecraft attitude tracking with disturbance rejection and almost global stabilization A Sanyal, A Fosbury, N Chaturvedi, DS Bernstein Journal of guidance, control, and dynamics 32 (4), 1167-1178, 2009	215	2009
Dynamics and control of a 3D pendulum J Shen, AK Sanyal, NA Chaturvedi, D Bernstein, H McClamroch 2004 43rd IEEE conference on decision and control (CDC)(IEEE cat. no …, 2004	169	2004
Asymptotic tracking control for spacecraft formation flying with decentralized collision avoidance D Lee, AK Sanyal, EA Butcher Journal of Guidance, Control, and Dynamics 38 (4), 587-600, 2015	158	2015
Decentralized consensus control of a rigid-body spacecraft formation with communication delay M Nazari, EA Butcher, T Yucelen, AK Sanyal Journal of Guidance, Control, and Dynamics 39 (4), 838-851, 2016	135	2016
Global optimal attitude estimation using uncertainty ellipsoids AK Sanyal, T Lee, M Leok, NH McClamroch Systems & Control Letters 57 (3), 236-245, 2008	129	2008
An almost global tracking control scheme for maneuverable autonomous vehicles and its discretization A Sanyal, N Nordkvist, M Chyba IEEE Transactions on Automatic control 56 (2), 457-462, 2010	111	2010
Almost global finite‐time stabilization of rigid body attitude dynamics using rotation matrices J Bohn, AK Sanyal International Journal of Robust and Nonlinear Control 26 (9), 2008-2022, 2016	103	2016
Finite-time control for spacecraft body-fixed hovering over an asteroid D Lee, AK Sanyal, EA Butcher, DJ Scheeres IEEE Transactions on Aerospace and Electronic Systems 51 (1), 506-520, 2015	89	2015
Rigid body attitude estimation based on the Lagrange–d’Alembert principle M Izadi, AK Sanyal Automatica 50 (10), 2570-2577, 2014	87	2014
A Lie group variational integrator for rigid body motion in SE (3) with applications to underwater vehicle dynamics N Nordkvist, AK Sanyal 49th IEEE conference on decision and control (CDC), 5414-5419, 2010	84	2010
Almost global robust attitude tracking control of spacecraft in gravity A Sanyal, N Chaturvedi AIAA guidance, navigation and control conference and exhibit, 6979, 2008	76	2008
Coupled orbit–attitude dynamics and relative state estimation of spacecraft near small Solar System bodies G Misra, M Izadi, A Sanyal, D Scheeres Advances in Space Research 57 (8), 1747-1761, 2016	75	2016
Almost Global Asymptotic Tracking Control for Spacecraft Body-Fixed Hovering near an Asteroid D Lee, AK Sanyal, E Butcher, D Scheeres Aerospace Science and Technology 38, 105-115, 2014	66	2014
Finite-time stabilisation of simple mechanical systems using continuous feedback AK Sanyal, J Bohn International Journal of Control 88 (4), 783-791, 2015	63	2015
Geometric structure-preserving optimal control of a rigid body AM Bloch, II Hussein, M Leok, AK Sanyal Journal of Dynamical and Control Systems 15 (3), 307-330, 2009	61	2009
Inertia-free spacecraft attitude control using reaction wheels A Weiss, I Kolmanovsky, DS Bernstein, A Sanyal Journal of Guidance, Control, and Dynamics 36 (5), 1425-1439, 2013	52	2013
Stabilization of a 3D rigid pendulum NA Chaturvedi, F Bacconi, AK Sanyal, D Bernstein, NH McClamroch Proceedings of the 2005, American Control Conference, 2005., 3030-3035, 2005	52	2005
Rigid body pose estimation based on the Lagrange–d’Alembert principle M Izadi, AK Sanyal Automatica 71, 78-88, 2016	49	2016
A discrete variational integrator for optimal control problems on SO (3) II Hussein, M Leok, AK Sanyal, AM Bloch Proceedings of the 45th IEEE Conference on Decision and Control, 6636-6641, 2006	49	2006

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