To access the full text documents, please follow this link: http://hdl.handle.net/2117/24981
Title: | Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun-Earth circular restricted three-body problem |
---|---|
Author: | Mingotti, Giorgio; Sánchez Cuartielles, Joan Pau; McInnes, Colin |
Other authors: | Universitat Politècnica de Catalunya. Departament de Matemàtica Aplicada I |
Abstract: | |
Abstract: | |
Subject(s): | -Àrees temàtiques de la UPC::Matemàtiques i estadística -Three-body problem -Orbital mechanics -Near-Earth object capture -Invariant manifolds -Low-thrust propulsion -Special dedicated sets -Optimal control problem -Libration point periodic orbit (LPO) -Distant prograde periodic orbit (DPO) -Easily retrievable objects (EROs) -Asteroid retrieval candidates -PERIODIC-ORBITS -EQUILIBRIUM POINTS -MOON TRAJECTORIES -TRANSIT ORBITS -MISSION DESIGN -TRANSFERS -ASTEROIDS -OPTIMIZATION -DYNAMICS -OBJECTS -Mecànica orbital -Problema dels tres cossos |
Rights: | Attribution-NonCommercial-NoDerivs 3.0 Spain
http://creativecommons.org/licenses/by-nc-nd/3.0/es/ |
Document type: | Article - Published version Article |
Share: |