Amit Sanyal
Amit Sanyal
Associate Professor, Mechanical and Aerospace Engineering, Syracuse University
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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
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
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
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
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
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
Nonlinear attitude control of the micro satellite ESEO
MP Topland, JT Gravdahl
55th International Astronautical Congress of the International Astronautical …, 2004
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
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
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
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
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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