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Memorias de investigación
Communications at congresses:
Optimal 3D Orbit Corrections in Curvilinear Coordinates
Year:2016
Research Areas
  • Space technology,
  • Aeronautical engineering
Information
Abstract
The minimum-time, constant-thrust orbit correction between two close non-coplanar circular orbits is studied using a relative motion formulation in curvilinear coordinates. The associated optimal control problem in the thrust orientation is tackled using the direct method to numerically solve a diverse set of problems for varying orbital radius and inclination. Additionally, an analytical estimate for the minimum-time inclination change maneuver is obtained. Fundamental changes in the structure of the solution and objective function are highlighted depending on the relation between the required radial displacement, inclination change and available thrust.
International
Si
Congress
26th AAS/AIAA Space Flight Mechanics Meeting
960
Place
Napa, California (EEUU)
Reviewers
Si
ISBN/ISSN
1081-6003
Start Date
14/02/2016
End Date
18/02/2016
From page
397
To page
414
Advances in the Astronautical Sciences Volume 158, Spaceflight Mechanics 2016
Participants
  • Autor: Juan Luis Gonzalo Gomez (UPM)
  • Autor: Claudio Bombardelli (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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