Communications at congresses:
Solving the Kepler equation with the SDG-code
Solving the Kepler equation with the SDG-code
Year:2017
Research Areas
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Aeronautical engineering
Information
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Abstract
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| A new code to solve the Kepler equation for elliptic and hyperbolic orbits has been developed. The motivation of the study is the determination of an appropriate seed to initialize the numerical method, considering the optimization already tested of the well known Newton-Raphson method. To do that, we take advantage of the full potential of the symbolic manipulators. The final algorithm is stable, reliable and solves successfully the solution of the Kepler equation in the singular corner (M << 1 and e ~ 1). | |
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International
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Si |
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Congress
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27th AAS/AIAA Space Flight Mechanics Meeting |
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730 |
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Place
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San Antonio (Texas) |
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Reviewers
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Si |
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ISBN/ISSN
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1081-6003 |
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Start Date
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05/02/2017 |
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End Date
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09/02/2017 |
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From page
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4143 |
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To page
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4160 |
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Advances in the Astronautical Sciences, Vol. 160 |
Participants
- Autor: Virginia Raposo Pulido (UPM)
- Autor: Jesus Pelaez Alvarez (UPM)
Research Group, Departaments and Institutes related
- Creador: Grupo de Investigación: Dinámica Espacial (SDG-UPM)
- Departamento: Física Aplicada a Las Ingenierías Aeronáutica y Naval
S2i 2021 Observatorio de investigación @ UPM con la colaboración del Consejo Social UPM
Cofinanciación del MINECO en el marco del Programa INNPACTO (IPT-020000-2010-22)