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Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun-Earth circular restricted three-body problem
Mingotti, Giorgio; Sánchez Cuartielles, Joan Pau; McInnes, Colin
Universitat Politècnica de Catalunya. Departament de Matemàtica Aplicada I
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
Attribution-NonCommercial-NoDerivs 3.0 Spain
http://creativecommons.org/licenses/by-nc-nd/3.0/es/
info:eu-repo/semantics/publishedVersion
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