| 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 | 247 | 2005 |
| 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 | 91 | 2007 |
| 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 | 69 | 2007 |
| Impaired aircraft performance envelope estimation PK Menon, P Sengupta, S Vaddi, BJ Yang, J Kwan Journal of Aircraft 50 (2), 410-424, 2013 | 68* | 2013 |
| Satellite orbit design and maintenance for terrestrial coverage P Sengupta, SR Vadali, KT Alfriend Journal of Spacecraft and Rockets 47 (1), 177-187, 2010 | 51 | 2010 |
| 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 | 51 | 2006 |
| Controller design for hypersonic vehicles accommodating nonlinear state and control constraints S Vaddi, P Sengupta AIAA Guidance, Navigation, and Control Conference, 6286, 2009 | 41 | 2009 |
| 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 | 38 | 2008 |
| 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 | 34 | 2008 |
| 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 | 33 | 2009 |
| 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 | 31 | 2004 |
| 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 | 29 | 2007 |
| 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 | 28 | 2008 |
| Dynamics and control of satellite relative motion in a central gravitational field P Sengupta Texas A&M University, 2007 | 23 | 2007 |
| Satellite relative motion propagation and control in the presence of J2 perturbations P Sengupta Texas A&M University, 2004 | 19 | 2004 |
| 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 | 16* | 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 | 15 | 2010 |
| 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 | 11 | 2004 |
| The Lambert W function and solutions to Kepler’s equation P Sengupta Celestial Mechanics and Dynamical Astronomy 99, 13-22, 2007 | 10 | 2007 |
Srinivas R VadaliProfessor of Aerospace Engineering, Texas A&M UniversityVerified email at tamu.edu
