Exploració per autor "Masdemont Soler, Josep"
Ara es mostren els items 54-73 de 101
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Leaving the Moon by means of invariant manifolds of libration point orbits
Masdemont Soler, Josep; Alessi, Elisa Maria; Gómez, Gerard (Elsevier, 2009)
Article
Accés restringit per política de l'editorialThe aim of this work is to look for rescue trajectories that leave the surface of the Moon, belonging to the hyperbolic manifolds associated with the central manifold of the Lagrangian points L1 and L2 of the Earth–Moon ... -
Libration transfer design using patched elliptic three-body models and graphics processing units
Peng, Hao; Bai, Xiaoli; Masdemont Soler, Josep; Gómez Muntané, Gerard; Xu, Shijie (2017-01-01)
Article
Accés obertCopyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. Design of the transfer from lunar orbits to the sun-Earth libration point region by direct searching in the highfidelity ephemeris model is ... -
Low-energy impact dynamics in the Earth – Moon system
Masdemont Soler, Josep; Gómez Muntané, Gerard; Alessi, Elisa Maria (2010)
Text en actes de congrés
Accés obertMost of the craters on the surface of the Moon were created by the collision of minor bodies of the Solar System, in particular asteroids coming from the Main Belt as a consequence of different types of resonance. Our ... -
Low-energy trajectory design and autonomous navigation to flyby near-Earth asteroids using CubeSats
Machuca, Pablo; Sànchez Cuartielles, Joan Pau; Masdemont Soler, Josep; Gómez Muntané, Gerard (2018)
Text en actes de congrés
Accés restringit per política de l'editorialIn response to the current interest in CubeSats and potential applications for planetary exploration, this work studies the feasibility of using autonomous CubeSats to flyby near-Earth asteroids. Considering the limited ... -
Low-thrust station-keeping control for lunar near rectilinear halo orbits
Gao, Chen; Masdemont Soler, Josep; Gómez Muntaner, Gerard; Yuan, Jianping (Springer Nature, 2023-04-01)
Article
Accés obertThis paper studies a low-thrust station-keeping of near rectilinear halo orbits in the Earth–Moon quasi-bicircular dynamical model, and it is illustrated using resonant near rectilinear halo orbits as nominal orbits. The ... -
Maneuvering spacecraft formations using a dynamically maneuvering spacecraft formations using a dynamically adapted finite element methodology
Masdemont Soler, Josep; García Taberner, Laura (2009)
Article
Accés restringit per política de l'editorialThe formation reconfiguration or the deployment of multiple spacecraft is a key issue that demands a robust methodology safely avoiding collision hazards. In this paper we present a systematic procedure to perform proximity ... -
Maneuvering spacraft formations using a dynamically adapted finite element methodology
Masdemont Soler, Josep; García Taberner, Laura (2009-11-10)
Article
Accés restringit per política de l'editorialThe formation reconfiguration or the deployment of multiple spacecraft is a key issue that demands a robust methodology safely avoiding collision hazards. In this paper we present a systematic procedure to perform ... -
Mathematical Methods Applied to the Celestial Mechanics of Artificial Satellites
Bertachini A. Prado, Antonio F.; Zanardi, Maria Cecilia; Yokoyama, Tadashi; Giuliatti Winter, Silvia Maria; Masdemont Soler, Josep (2012)
Article
Accés obert -
Mathematical methods applied to the celestial mechanics of artificial satellites
Prado, Antonio F. Bertachini A.; Masdemont Soler, Josep; Zanardi, Maria Cecilia; Winter, Silvia Maria Giuliatti; Yokoyama, Tadashi; Gomes, Vivian Martins (2015-02-02)
Article
Accés obert -
Mathematical Methods Applied to the Celestial Mechanics of Artificial Satellites 2013
Prado, Antonio F. Bertachini A.; Masdemont Soler, Josep; Zanardi, Maria Cecilia; Winter, Silvia Maria Giuliatti; Yokoyama, Tadashi; Gomes, Vivian Martins (2013)
Article
Accés obert -
Methodology and estimation costs for proximity maneuvering spacecraft formations in the vicinity of libration points
García Taberner, Laura; Masdemont Soler, Josep (2012)
Text en actes de congrés
Accés obertThe aim of this paper is to study and provide estimations of the cost of reconfiguration maneuvers in the neighbor- hood of L1 and L2 libration points of the Sun-Earth system. The problem is considered as a function of ... -
Natural configurations for formation flying around triangular libration points for the elliptic and the bicircular problem in the earth-moon system
Salazar, Francisco; Winter, O. C.; Macau, E.E.N.; Masdemont Soler, Josep; Gómez Muntané, Gerard (2014)
Text en actes de congrés
Accés obertThe concept of Satellite Formation Flying (SFF) means to have two or more satellites in orbit such that their relative positions remain constant or obeying a certain dynamical configuration along the trajectory. This ... -
Natural formations at the Earth-Moon triangular point in perturbed restricted problems
Salazar, Francisco; Winter, O. C.; Macau, E.E.N.; Masdemont Soler, Josep; Gómez Muntané, Gerard (2015-07-01)
Article
Accés obertPrevious studies for small formation flying dynamics about triangular libration points have determined the existence of regions of zero and Minimum Relative Radial Acceleration with respect to the nominal trajectory, that ... -
Nonlinear dynamics in an extended neighbourhood of the translunar equilibrium point
Jorba, Angel; Masdemont Soler, Josep (1995)
Article
Accés obert -
On the cucker-smale flocking model applied to a formation moving in a central force field around the Earth
Paita, Fabrizio; Gomez Muntaner, Gerard; Masdemont Soler, Josep (2013)
Text en actes de congrés
Accés restringit per política de l'editorialThe Cucker – Smale (CS) flocking model is an interacting particles control system where every particle adjusts its dynamics according to a weighted average between its velocity and those of the other elements of the ... -
On the mechanisms of natural transport in the solar system
Masdemont Soler, Josep; Ren, Yuan; Gómez Muntané, Gerard; Fantino, Elena (2010)
Text en actes de congrés
Accés obertSome minor bodies in the solar system (i.e., comets, asteroids and planetary ejecta) are capable of performing transfers from their original location to very distant places, provided they possess sufficiently large ... -
On the relationship between the weak stability boundary region of the earth and the low-energy transfers to the moon
Masdemont Soler, Josep; Ren, Yuan; Gómez Muntané, Gerard; Fantino, Elena (2009)
Text en actes de congrés
Accés obertThe term Weak Stability Boundary (WSB) is related to a region of stable motion around the second primary of a circular restricted three-body problem (CR3BP). Previous work on this subject has shown that, at a given energy ... -
On the relationship between the weak stability boundary region of the earth and the low-energy transfers to the moon
Masdemont Soler, Josep; Ren, Yuan; Fantino, Elena; Gómez Muntané, Gerard (2009)
Text en actes de congrés
Accés obertThe term Weak Stability Boundary (WSB) is related to a region of stable motion around the second primary of a circular restricted three-body problem (CR3BP). Previous work on this subject has shown that, at a given energy ... -
On the rotational Cucker-Smale model: optimal formation configuration and adaptive gains design
Paita, Fabrizio; Gómez Muntané, Gerard; Masdemont Soler, Josep (2015)
Text en actes de congrés
Accés restringit per política de l'editorialIn the present paper we consider the attitude synchronization problem for a formation of spacecraft flying in free space. In particular, we consider the same control laws of [1] and we expand on the results presented there. ... -
On the scattering map and homoclinic connections between Lyapunov orbits
Cancalias Vila, Elisabet; Delshams Valdés, Amadeu; Masdemont Soler, Josep; Roldán González, Pablo (2005-09)
Comunicació de congrés
Accés obertHomoclinic and heteroclinic connections between planar Lyapunov orbits of the Sun-Earth and Earth-Moon models can be found by using their hyperbolic invariant manifolds and Poincare section representations. These connections ...