Piyush M. Mehta
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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
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
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
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
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
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
A methodology for reduced order modeling and calibration of the upper atmosphere
PM Mehta, R Linares
Space Weather 15 (10), 1270-1287, 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
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
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
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
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
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
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
Density and ballistic coefficient estimation revisited
PM Mehta, CA McLaughlin
2011 AAS/AIAA Astrodynamics Specialist Conference, ASTRODYNAMICS 2011, 3247-3264, 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
Benchmarking forecasting models for space weather drivers
RJ Licata, WK Tobiska, PM Mehta
Space Weather 18 (10), e2020SW002496, 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
Data-driven framework for real-time thermospheric density estimation
PM Mehta, R Linares
arXiv preprint arXiv:1808.06014, 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
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