Spacecraft Trajectory Design via Quasi-periodic Invariant Tori.

Lead Research Organisation: University of Surrey
Department Name: Surrey Space Centre Academic

Abstract

Spacecraft Trajectory Design via Quasi-periodic Invariant Tori. This project aims at implementing modern numerical
procedures for calculating quasi-periodic trajectories and their manifolds, thereby researching into novel transfer
opportunities to send low-cost satellite missions towards the Moon and beyond.

Publications

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Studentship Projects

Project Reference Relationship Related To Start End Student Name
EP/T518050/1 01/10/2020 30/09/2025
2598157 Studentship EP/T518050/1 01/10/2021 30/09/2024 Danny Owen