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Srinivas R Vadali
Srinivas R Vadali
Professor of Aerospace Engineering, Texas A&M University
Verified email at tamu.edu
Title
Cited by
Cited by
Year
Spacecraft formation flying: Dynamics, control and navigation
K Alfriend, SR Vadali, P Gurfil, J How, L Breger
Elsevier, 2009
9582009
Spacecraft formation flying control using mean orbit elements
H Schaub, SR Vadali, JL Junkins, KT Alfriend
The Journal of the Astronautical Sciences 48, 69-87, 2000
3622000
Variable-structure control of spacecraft large-angle maneuvers
SR Vadali
Journal of Guidance, Control, and Dynamics 9 (2), 235-239, 1986
3571986
Formation establishment and reconfiguration using impulsive control
SS Vaddi, KT Alfriend, SR Vadali, P Sengupta
Journal of Guidance, Control, and Dynamics 28 (2), 262-268, 2005
2472005
Formation flying: accommodating nonlinearity and eccentricity perturbations
SS Vaddi, SR Vadali, KT Alfriend
Journal of Guidance, Control, and Dynamics 26 (2), 214-223, 2003
2442003
Feedback control law for variable speed control moment gyros
H Schaub, SR Vadali, JL Junkins
The Journal of the astronautical sciences 46, 307-328, 1998
2221998
Robust time-optimal control-Frequency domain approach
T Singh, SR Vadali
Journal of Guidance, Control, and Dynamics 17 (2), 346-353, 1994
2141994
Feedback control and steering laws for spacecraft using single gimbal control moment gyros
S Vadali
Guidance, Navigation and Control Conference, 3475, 1988
1951988
Robust time-delay control
T Singh, SR Vadali
1891993
Preferred gimbal angles for single gimbal control moment gyros
SR Vadali, HS Oh, SR Walker
Journal of Guidance, Control, and Dynamics 13 (6), 1090-1095, 1990
1791990
Optimal open-loop and stable feedback control of rigid spacecraft attitude maneuvers
SR Vadali
Journal of Astronautical Sciences, 1984
1161984
Initial conditions and fuel-optimal control for formation flying of satellites
S Vadali, H Schaub, K Alfriend
Guidance, Navigation, and Control Conference and Exhibit, 4265, 1999
1151999
Optimal variable-structure control tracking of spacecraft maneuvers
JL Crassidis, SR Vadali, FL Markley
Journal of Guidance, Control, and Dynamics 23 (3), 564-566, 2000
1132000
An intelligent control concept for formation flying satellites
SR Vadali, SS Vaddi, KT Alfriend
International Journal of Robust and Nonlinear Control: IFAC‐Affiliated …, 2002
1122002
Robust time-delay control of multimode systems
T Singh, SR Vadali
International Journal of Control 62 (6), 1319-1339, 1995
981995
Relative motion and the geometry of formations in Keplerian elliptic orbits with arbitrary eccentricity
P Sengupta, SR Vadali
Journal of guidance, control, and dynamics 30 (4), 953-964, 2007
852007
Fuel-optimal, low-thrust, three-dimensional Earth-Mars trajectories
RS Nah, SR Vadali, E Braden
Journal of Guidance, Control, and Dynamics 24 (6), 1100-1107, 2001
822001
Modeling issues related to retrieval of flexible tethered satellite systems
E Kim, SR Vadali
Journal of Guidance, Control, and Dynamics 18 (5), 1169-1176, 1995
761995
Near-minimum time, closed-loop slewing of flexible spacecraft
RM Byers, SR Vadali, JL Junkins
Journal of Guidance, Control, and Dynamics 13 (1), 57-65, 1990
761990
Quasi-closed-form solution to the time-optimal rigid spacecraft reorientation problem
RM Byers, SR Vadali
Journal of Guidance, Control, and Dynamics 16 (3), 453-461, 1993
751993
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