Accuracy and Efficiency Comparison of Six Numerical Integrators for Propagating Perturbed Orbits

Author:

Atallah Ahmed M.,Woollands Robyn M.,Elgohary Tarek A.ORCID,Junkins John L.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference45 articles.

1. Atallah, A.: An Implementation and Verification of Of a High-Precision Orbit Propagator. Master’s Thesis, Cairo University, Cairo (2018)

2. Atallah, A., Bani Younes, A.: Parallel integration of perturbed orbital motion. In: AIAA Scitech 2019 (2019)

3. Atallah, A., Woollands, R.M., Bani Younes, A., Junkins, J.: Tuning orthogonal polynomial degree and segment interval length to achieve prescribed precision approximation of irregular functions. In: 2018 Space Flight Mechanics Meeting, pp 2225. https://doi.org/10.2514/6.2018-2225 (2018)

4. Bai, X.: Modified Chebyshev-Picard Iteration for Solution of Initial Value and Boundary Value Problems. Ph.D. Thesis, Texas A&M, College Station (2010)

5. Bai, X., Junkins, J.: Modified chebyshev-Picard iteration methods for solution of initial value problems. Adv. Astronaut. Sci. 139, 345–362 (2011)

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