Amit Sanyal
Amit Sanyal
Associate Professor, Mechanical and Aerospace Engineering, Syracuse University
Bestätigte E-Mail-Adresse bei - Startseite
Zitiert von
Zitiert von
Rigid-body attitude control
NA Chaturvedi, AK Sanyal, NH McClamroch
IEEE control systems magazine 31 (3), 30-51, 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
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
Global optimal attitude estimation using uncertainty ellipsoids
AK Sanyal, T Lee, M Leok, NH McClamroch
Systems & Control Letters 57 (3), 236-245, 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
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
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
Rigid body attitude estimation based on the Lagrange–d’Alembert principle
M Izadi, AK Sanyal
Automatica 50 (10), 2570-2577, 2014
Almost global robust attitude tracking control of spacecraft in gravity
A Sanyal, N Chaturvedi
AIAA guidance, navigation and control conference and exhibit, 6979, 2008
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
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
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
Nonlinear attitude control of the micro satellite ESEO
MP Topland, JT Gravdahl
55th International Astronautical Congress of the International Astronautical …, 2004
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
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
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
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
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
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
Finite-time stabilisation of simple mechanical systems using continuous feedback
AK Sanyal, J Bohn
International journal of control 88 (4), 783-791, 2015
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