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Memorias de investigación
Communications at congresses:
On the resolution of the Lambert's problem with the SDG-code
Year:2017
Research Areas
  • Aeronautical engineering
Information
Abstract
Based on the Lambert's problem, once identified the one-parameter family of orbits that verify the geometric constraints of the problem, we must express the orbits based on a single parameter that allows to select those that satisfy the kinematic condition. The aim of this paper is to reformulate the problem choosing as parameter the true anomaly of the bisector defined by the directions of the two position vectors. The algorithm applied is the SDG-code, developed by the Space Dynamics Group at UPM, which has already been assessed on the resolution of the Kepler equation proving its stability and reliability.
International
Si
Congress
27th AAS/AIAA Space Flight Mechanics Meeting
730
Place
San Antonio (Texas)
Reviewers
Si
ISBN/ISSN
1081-6003
Start Date
05/02/2017
End Date
09/02/2017
From page
4125
To page
4142
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
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