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Tarek A. Elgohary
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Time domain inverse problems in nonlinear systems using collocation & radial basis functions
TA Elgohary, L Dong, JL Junkins, SN Atluri
CMES: Computer Modeling in Engineering & Sciences 100 (1), 59-84, 2014
352014
A simple, fast, and accurate time-integrator for strongly nonlinear dynamical systems
TA Elgohary, L Dong, JL Junkins, SN Atluri
CMES: Computer Modeling in Engineering & Sciences 100 (3), 249-275, 2014
322014
AN RBF-COLLOCATION ALGORITHM FOR ORBIT PROPAGATION
TA Elgohary, JL Junkins, SN Atluri
Advances in Astronautical Sciences: AAS/AIAA Space Flight Mechanics Meeting, 2015
252015
Accuracy and efficiency comparison of six numerical integrators for propagating perturbed orbits
AM Atallah, RM Woollands, TA Elgohary, JL Junkins
The Journal of the Astronautical Sciences 67, 511-538, 2020
212020
High Accuracy Trajectory and Uncertainty Propagation Algorithm for Long-Term Asteroid Motion Prediction
JD Turner, TA Elgohary, M Majji, JL Junkins
Adventures on the Interface of Mechanics and Control: K. T. Alfriend, M …, 2012
172012
Nonlinear analysis of a 2-DOF piecewise linear aeroelastic system
T Kalmár-Nagy, R Csikja, TA Elgohary
Nonlinear Dynamics 85, 739-750, 2016
162016
Solution of Post-Buckling & Limit Load Problems, Without Inverting the Tangent Stiffness Matrix & Without Using Arc-Length Methods
TA Elgohary, L Dong, JL Junkins, SN Atluri
CMES: Computer Modeling in Engineering & Sciences 98 (6), 543 - 563, 2014
152014
An adaptive analytic continuation method for computing the perturbed two-body problem state transition matrix
TH Tasif, TA Elgohary
The Journal of the Astronautical Sciences 67, 1412-1444, 2020
122020
ANALYTIC POWER SERIES SOLUTIONS FOR TWO-BODY AND J2–J6 TRAJECTORIES AND STATE TRANSITION MODELS
K Hernandez, JL Read, TA Elgohary, JD Turner, JL Junkins
Advances in Astronautical Sciences: AAS/AIAA Astrodynamics Specialist Conference, 2015
122015
Inertial space-based orbit estimation: A new measurement model for multiple observers
J Hippelheuser, TA Elgohary
Acta Astronautica 181, 717-732, 2021
112021
A new method for space objects probability of collision
A Probe, TA Elgohary, JL Junkins
AIAA/AAS Astrodynamics Specialist Conference, 5653, 2016
112016
Analytic Transfer Functions for the Dynamics & Control of Flexible Rotating Spacecraft Performing Large Angle Maneuvers
TA Elgohary, JD Turner, JL Junkins
The Journal of the Astronautical Sciences 62 (2), 168-195, 2015
112015
STATE TRANSITION TENSOR MODELS FOR THE UNCERTAINTY PROPAGATION OF THE TWO-BODY PROBLEM
TA Elgohary, JD Turner
Advances in Astronautical Sciences: AAS/AIAA Astrodynamics Conference 150 …, 2014
112014
High-Order Analytic Continuation and Numerical Stability Analysis for the Classical Two-Body Problem
T Elgohary, JD Turner, JL Junkins
Advances in Astronautical Sciences: The Jer-Nan Juang Astrodynamics …, 2012
112012
A novel analytic continuation power series solution for the perturbed two-body problem
K Hernandez, TA Elgohary, JD Turner, JL Junkins
Celestial Mechanics and Dynamical Astronomy 131, 1-32, 2019
102019
ANALYTIC CONTINUATION POWER SERIES SOLUTION FOR THE TWO-BODY PROBLEM WITH ATMOSPHERIC DRAG
K Hernandez, TA Elgohary, JD Turner, JL Junkins
Advances in Astronautical Sciences: AAS/AIAA Space Flight Mechanics Meeting …, 2016
92016
Novel computational and analytic techniques for nonlinear systems applied to structural and celestial mechanics
TAA Elgohary
Texas A&M University, 2015
92015
NEW GEOMETRIC APPROACH FOR MULTI NODE SPACE-BASED ORBIT ESTIMATION
JE Hippelheuser, TA Elgohary
2nd IAA Conference on Space Situational Awareness, 2020
72020
An adaptive local variational iteration method for orbit propagation and strongly nonlinear dynamical systems
X Wang, TA Elgohary, S Atluri
AIAA Scitech 2020 Forum, 0957, 2020
72020
A HIGH ORDER ANALYTIC CONTINUATION TECHNIQUE FOR THE PERTURBED TWO-BODY PROBLEM STATE TRANSITION MATRIX
TH Tasif, TA Elgohary
AAS/AIAA Space Flight Mechanics Meeting, 2019
72019
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