Efficient trajectory design for distant planetary orbiters

Francesca Scala; Ioannis Gkolias; Camilla Colombo

doi:10.2514/1.g007236

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arXiv · 2401.14755

Efficient trajectory design for distant planetary orbiters

Francesca Scala·Ioannis Gkolias·Camilla Colombo

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Abstract

Starting from the Hamiltonian representation of the dynamics in \cite{rosengren2015chaos,colombo2019long}, this work proposes an innovative procedure to design fully-analytical maneuvers for post-mission disposal of HEOs satellites, exploiting the third-body perturbations. The Hamiltonian representation has been selected to include the external perturbing effects and to obtain a phase space representation. Notably, the orbit evolution can be described through the variation of double-averaged orbital elements over the orbital periods of the spacecraft and the perturbing bodies around the central planet. this work conveys a two-dimensional Hamiltonian representation under the third-body perturbations and the central planet's oblateness. The effect of solar radiation pressure has been neglected in this analysis.

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Francesca Scala, Ioannis Gkolias, Camilla Colombo. 2024-01-26. Efficient trajectory design for distant planetary orbiters. https://doi.org/10.2514/1.g007236

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