المؤلفون: Mingotti, Giorgio, Sánchez Cuartielles, Joan Pau, McInnes, Colin

المساهمون: Universitat Politècnica de Catalunya. Departament de Matemàtica Aplicada I

مصطلحات موضوعية: 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

وصف الملف: 28 p.

العلاقة: http://link.springer.com/article/10.1007%2Fs10569-014-9589-9Test; Mingotti, G.; Sánchez, J.P.; McInnes, C. Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun-Earth circular restricted three-body problem. "Celestial mechanics and dynamical astronomy", 01 Novembre 2014, vol. 120, núm. 3, p. 309-336.; http://hdl.handle.net/2117/24981Test

الإتاحة: https://doi.org/10.1007/s10569-014-9589-9Test
http://hdl.handle.net/2117/24981Test

المؤلفون: Joan Pau Sánchez, Colin R. McInnes, Giorgio Mingotti

المساهمون: Universitat Politècnica de Catalunya. Departament de Matemàtica Aplicada I

المصدر: UPCommons. Portal del coneixement obert de la UPC
Universitat Politècnica de Catalunya (UPC)
Recercat. Dipósit de la Recerca de Catalunya
Universitat Jaume I

مصطلحات موضوعية: DYNAMICS, Invariant manifold, Special dedicated sets, ASTEROIDS, Propulsion, Topology, MOON TRAJECTORIES, Mecànica orbital, Easily retrievable objects (EROs), Three-body problem, TRANSFERS, Initial value problem, Orbital mechanics, Homoclinic orbit, Optimal control problem, OPTIMIZATION, Mathematical Physics, Asteroid retrieval candidates, Physics, EQUILIBRIUM POINTS, Problema dels tres cossos, Low-thrust propulsion, Applied Mathematics, Distant prograde periodic orbit (DPO), Libration point periodic orbit (LPO), PERIODIC-ORBITS, Matemàtiques i estadística [Àrees temàtiques de la UPC], Astronomy and Astrophysics, MISSION DESIGN, Invariant (physics), Stable manifold, Near-Earth object capture, Computational Mathematics, Classical mechanics, Space and Planetary Science, Invariant manifolds, Modeling and Simulation, Physics::Space Physics, TRANSIT ORBITS, Heteroclinic orbit, Astrophysics::Earth and Planetary Astrophysics, OBJECTS

وصف الملف: application/pdf

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e71501dce9cde9352babe97504c84ff5Test
http://hdl.handle.net/2117/24981Test

المؤلفون: Atanasova, Diana

المساهمون: Hall, Glen R.

مصطلحات موضوعية: Mathematics, Annulus map, Parabolic restricted three-body problem, Transit orbits

العلاقة: https://hdl.handle.net/2144/39615Test

الإتاحة: https://hdl.handle.net/2144/39615Test

مصطلحات الفهرس: 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, Article

URL: http://hdl.handle.net/2117/24981Test
http://link.springer.com/article/10.1007%2Fs10569-014-9589-9Test
http://link.springer.com/article/10.1007%2Fs10569-014-9589-9Test