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Prasenjit Sengupta
Prasenjit Sengupta
Sandbox AQ
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Title
Cited by
Cited by
Year
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
2432005
Relative motion and the geometry of formations in keplerian elliptic orbits
P Sengupta, SR VADALI
Journal of guidance, control, and dynamics 30 (4), 953-964, 2007
902007
Impaired aircraft performance envelope estimation
PK Menon, P Sengupta, S Vaddi, BJ Yang, J Kwan
Journal of Aircraft 50 (2), 410-424, 2013
69*2013
Second-order state transition for relative motion near perturbed, elliptic orbits
P Sengupta, SR Vadali, KT Alfriend
Celestial Mechanics and Dynamical Astronomy 97 (2), 101-129, 2007
682007
Periodic relative motion near a keplerian elliptic orbit with nonlinear differential gravity
P Sengupta, R Sharma, SR Vadali
Journal of guidance, control, and dynamics 29 (5), 1110-1121, 2006
502006
Satellite orbit design and maintenance for terrestrial coverage
P Sengupta, SR Vadali, KT Alfriend
Journal of Spacecraft and Rockets 47 (1), 177-187, 2010
482010
Controller design for hypersonic vehicles accommodating nonlinear state and control constraints
S Vaddi, P Sengupta
AIAA Guidance, Navigation, and Control Conference, 6286, 2009
412009
Averaged Relative Motion and Applications to Formation Flight Near Perturbed Orbits
P SENGUPTA, SR VADALI, KT ALFRIEND
Journal of guidance, control, and dynamics 31 (2), 258-272, 2008
382008
Optimal design of satellite formation relative motion orbits using least-squares methods
HUI YAN, KT ALFRIEND, SR VADALI, P SENGUPTA
Journal of guidance, control, and dynamics 32 (2), 599-604, 2009
332009
Queueing network models of the national airspace system
M Tandale, P Menon, J Rosenberger, K Subbarao, P Sengupta, V Cheng
The 26th Congress of ICAS and 8th AIAA ATIO, 8942, 2008
332008
Fundamental Frequencies of Satellite Relative Motion and Control of Formations
SR VADALI, P SENGUPTA, HUI YAN, KT ALFIIEND
Journal of guidance, control, and dynamics 31 (5), 1239-1248, 2008
33*2008
Modeling and control of satellite formations in high eccentricity orbits
P Sengupta, SR Vadali, KT Alfriend
Journal of Astronautical Sciences 52 (1), 149-168, 2004
302004
Near-optimal feedback rendezvous in elliptic orbits accounting for nonlinear differential gravity
R SHARMA, P SENGUPTA, SR VADALI
Journal of guidance, control, and dynamics 30 (6), 1803-1813, 2007
292007
Analytical solution for power-limited optimal rendezvous near an elliptic orbit
P Sengupta, SR Vadali
Journal of Optimization Theory and Applications 138 (1), 115-137, 2008
282008
Dynamics and control of satellite relative motion in a central gravitational field
P Sengupta
Texas A&M University, 2007
232007
Satellite relative motion propagation and control in the presence of J2 perturbations
P Sengupta
Texas A&M University, 2004
192004
Satellite orbit transfer and formation reconfiguration via an attitude control analogy
P Sengupta, SR Vadali
Journal of guidance, control, and dynamics 28 (6), 1200-1209, 2005
17*2005
A framework for stochastic air traffic flow modeling and analysis
P Menon, M Tandale, J Kim, P Sengupta
AIAA Guidance, Navigation, and Control Conference, 7852, 2010
152010
Development of a state transition matrix for relative motion using the unit sphere approach
H Yan, P Sengupta, SR Vadali, KT Alfriend
Adv. Astronaut. Sci 119 (1), 935-946, 2004
112004
The Lambert W function and solutions to Kepler’s equation
P Sengupta
Celestial Mechanics and Dynamical Astronomy 99, 13-22, 2007
102007
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