New density estimates derived using accelerometers on board the CHAMP and GRACE satellites PM Mehta, AC Walker, EK Sutton, HC Godinez Space Weather 15 (4), 558-576, 2017 | 50 | 2017 |
Modeling satellite drag coefficients with response surfaces PM Mehta, A Walker, E Lawrence, R Linares, D Higdon, J Koller Advances in Space Research 54 (8), 1590-1607, 2014 | 43 | 2014 |
Comparing physical drag coefficients computed using different gas–surface interaction models PM Mehta, A Walker, CA McLaughlin, J Koller Journal of Spacecraft and Rockets 51 (3), 873-883, 2014 | 40 | 2014 |
Drag Coefficient Model using the Cercignani-Lampis-Lord Gas-Surface Interaction Model A Walker, PM Mehta, J Koller Journal of Spacecraft and Rockets 51 (5), 1544-1563, 2014 | 38 | 2014 |
Drag Coefficient Model Using the Cercignani–Lampis–Lord Gas–Surface Interaction Model A Walker, PM Mehta, J Koller Journal of Spacecraft and Rockets 51 (5), 1544-1563, 2014 | 38 | 2014 |
Drag coefficient modeling for grace using Direct Simulation Monte Carlo PM Mehta, CA McLaughlin, EK Sutton Advances in Space Research 52 (12), 2035-2051, 2013 | 37 | 2013 |
A methodology for reduced order modeling and calibration of the upper atmosphere PM Mehta, R Linares Space Weather 15 (10), 1270-1287, 2017 | 27 | 2017 |
A quasi‐physical dynamic reduced order model for thermospheric mass density via hermitian space‐dynamic mode decomposition PM Mehta, R Linares, EK Sutton Space Weather 16 (5), 569-588, 2018 | 17 | 2018 |
An open source hypersonic aerodynamic and aerothermodynamic modelling tool P Mehta, E Minisci, M Vasile, AC Walker, M Brown 8th European Symposium on Aerothermodynamics for Space Vehicles, 2015 | 14 | 2015 |
A new transformative framework for data assimilation and calibration of physical ionosphere‐thermosphere models PM Mehta, R Linares Space Weather 16 (8), 1086-1100, 2018 | 13 | 2018 |
Photometric data from non-resolved objects for space object characterization and improved atmospheric modeling R Linares, MA Shoemaker, AC Walker, PM Mehta, D Palmer, ... Los Alamos National Lab.(LANL), Los Alamos, NM (United States), 2013 | 13 | 2013 |
Sensitivity analysis towards probabilistic re-entry modeling of spacecraft and space debris PM Mehta, A Walker, M Brown, E Minisci, ML Vasile AIAA Modeling and Simulation Technologies Conference, 3098, 2015 | 12 | 2015 |
Sensitivity analysis and probabilistic re-entry modeling for debris using high dimensional model representation based uncertainty treatment PM Mehta, M Kubicek, E Minisci, M Vasile Advances in Space Research 59 (1), 193-211, 2017 | 9 | 2017 |
Break-up modelling and trajectory simulation under uncertainty for asteroids PM Mehta, E Minisci, M Vasile Proceeding of the 4th IAA Planetary Defense Conference, Frascati, Roma, 13-17, 2015 | 9 | 2015 |
Density and ballistic coefficient estimation revisited PM Mehta, CA McLaughlin 2011 AAS/AIAA Astrodynamics Specialist Conference, ASTRODYNAMICS 2011, 3247-3264, 2012 | 9 | 2012 |
Computer graphics for space debris PM Mehta, GB Arnao, D Bonetti, E Minisci, M Vasile Proceedings of the 6th International Conference on Astrodynamics Tools and …, 2016 | 8 | 2016 |
Benchmarking forecasting models for space weather drivers RJ Licata, WK Tobiska, PM Mehta Space Weather 18 (10), e2020SW002496, 2020 | 4 | 2020 |
Quantifying the storm time thermospheric neutral density variations using model and observations EC Kalafatoglu Eyiguler, JS Shim, MM Kuznetsova, Z Kaymaz, ... Space Weather 17 (2), 269-284, 2019 | 4 | 2019 |
Data-driven framework for real-time thermospheric density estimation PM Mehta, R Linares arXiv preprint arXiv:1808.06014, 2018 | 4 | 2018 |
Different implementations of diffuse reflection with incomplete accommodation for drag coefficient modeling A Walker, P Mehta, J Koller Journal of Spacecraft and Rockets 51 (5), 1522-1532, 2014 | 4 | 2014 |