Parallel Finite Element Gravity Model

Author:

Atallah Ahmed1,Bani Younes Ahmad1

Affiliation:

1. San Diego State University

Publisher

American Institute of Aeronautics and Astronautics

Reference25 articles.

1. Analytical Nonlinear Propagation of Uncertainty in the Two-Body Problem

2. X. Bai, “Modified Chebyshev-Picard Iteration for Solution of Initial Value and Boundary Value Problems,” PhD. Dissertation, Texas A&M,College Station, Texas, USA,2010.

3. A. B. Younes, Ph.D. Dissertation: Orthogonal Polynomial Approximation in Higher Dimensions: Applications in Astrodynamics. PhD thesis, Texas A&M University,Department of Aerospace Engineering, 2013.

4. B. Macomber, Enhancements to Chebyshev-Picard Iteration Efficiency for Generrally Perturbed Orbits and Constrained Dynamical Systems. PhD thesis, Texas A&MUniversity, 2015.

5. R. Woollands, “Regularization and Computational Methods for Precise Solution of Perturbed Orbit Transfer Problems,” PhD. Dissertation, Texas A&M,College Station, Texas, USA,2016.

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