Portal de Transparencia

Actividad investigadora:

• Artículos en revistas
  • [2019] RESIDENT SPACE OBJECT PROPER ORBITAL ELEMENTS
  • [2017] Accurate numerical orbit propagation of planetary close encounters
  • [2017] Accurate numerical orbit propagation of planetary close encounters
  • [2017] Approximate solutions of non-linear circular orbit relative motion in curvilinear coordinates
  • [2017] Deflection of fictitious asteroid 2017 PDC: Ion beam vs. kinetic impactor
  • [2017] Deflection of fictitious asteroid 2017 PDC: Ion beam vs. kinetic impactor
  • [2017] Environmental effect of space debris repositioning
  • [2017] Environmental effect of space debris repositioning
  • [2017] Optimal Continuous-Thrust Rephasing Maneuver in Circular Orbit
  • [2017] Optimal Continuous-Thrust Rephasing Maneuver in Circular Orbit
  • [2016] APPROXIMATE ANALYTICAL SOLUTION OF THE MULTIPLE REVOLUTION LAMBERT'S TARGETING PROBLEM
  • [2016] Approximate Solution of Non-linear Circular Orbit Relative Motion in Curvilinear Coordinates
  • [2016] COMPACT SOLUTION OF CIRCULAR ORBIT RELATIVE MOTION IN CURVILINEAR COORDINATES
  • [2016] CONTACTLESS ION BEAM ASTEROID DESPINNING
  • [2016] Compact solution of circular orbit relative motion in curvilinear coordinates
  • [2016] GTOC8: RESULTS AND METHODS OF POLIMI-UPM
  • [2016] OPTIMAL 3D ORBIT CORRECTIONS IN CURVILINEAR COORDINATES
  • [2016] OPTIMAL LOW THRUST ORBIT CORRECTION IN CURVILINEAR COORDINATES
  • [2016] Optimal low thrust orbit correction in curvilinear coordinates
  • [2015] Impact of Nonideal Effects on Bare Electrodynamic Tether Performance
  • [2015] Impact of nonideal effects on bare electrodynamic tether performance
  • [2015] LOW-THRUST TRAJECTORY OPTIMIZATION IN DROMO VARIABLES
  • [2015] MITIGATION OF PROPAGATION ERROR IN INTERPLANETARY TRAJECTORIES
  • [2015] OPTIMAL LOW-THRUST-BASED RENDEZVOUS MANEUVERS
  • [2015] Optimal Impulsive Collision Avoidance in Low Earth Orbit
  • [2015] Optimal Impulsive Collision Avoidance in Low Earth Orbit
  • [2015] Temporarily Captured Asteroids as a Pathway to Affordable Asteroid Retrieval Missions
  • [2014] Analytical formulation of impulsive collision avoidance dynamics
  • [2014] TIME ELEMENTS FOR ENHANCED PERFORMANCE OF THE DROMO ORBIT PROPAGATOR
  • [2013] A new set of integrals of motion to propagate the perturbed two-body problem
  • [2013] Deorbiting Performance of Bare Electrodynamic Tethers in Inclined Orbits
  • [2013] The ion beam shepherd: A new concept for asteroid deflection
  • [2013] The ion beam shepherd: A new concept for asteroid deflection
  • [2012] Accurate analytical approximation of asteroid deflection with constant tangential thrust
  • [2012] Adaptative scheme for Accurate orbit propagation
  • [2012] Dynamic stabilization of L2 periodic orbits using attitude-orbit coupling effects
  • [2012] Power Density of a Bare Electrodynamic Tether Generator
  • [2012] STABLE ARTIFICIAL EQUILIBRIUM POINTS IN THE MARS-PHOBOS SYSTEM
  • [2012] The ion beam shepherd: A new concept for asteroid deflection
  • [2011] ADAPTIVE SCHEME FOR ACCURATE ORBIT PROPAGATION
  • [2011] Asymptotic Solution for the Two-Body Problem with Constant Tangencial Acceleration
  • [2011] Ion Beam Shepherd for Asteroid Deflection
  • [2011] Ion Beam Shepherd for Contactless Space Debris Removal
  • [2011] On the stability of artificial equilibrium points in the circular restricted three-body problem
  • [2010] Asymptotic Solution for the Current Profile of Passive Bare Electrodynamic Tethers
  • [2010] On the Stability of Artificial Equilibrium Points in the Circular Restricted Three Body Problem
  • [2010] Three-Body Dynamics and Self-Powering of an Electrodynamic Tether in a Plasmasphere
  • [2009] Electrodynamic Tether at Jupiter-II: Fast Moon Tour After Capture
  • [2009] Jupiter Power Generation with Electrodynamic Tethers at Constant Orbital Energy.
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• Capítulos de libros
  • [2016] Advanced orbit propagation methods and application to space debris collision avoidance
  • [2013] Ion beam shepherd satellite for space debris removal
• Conferencias invitadas en congresos
  • [2010] Electrodynamic Tethers for Space Debris Removal,
• Otros méritos
  • [2010] Dirección de Proyecto Fin de Carrera
• Patentes
  • [2018] System for generating electrical power in orbit by means of floating conductor cables
  • [2018] System for in-orbit propulsion via floating conductor cables
• Ponencia en Congresos
  • [2017] Deflection of Fictitious Asteroid 2017 PDC: Ion Beam vs. Kinetic Impactor
  • [2017] Last-minute semi-analytical asteroid deflection by nuclear explosion
  • [2017] Last-minute semi-analytical asteroid deflection by nuclear explosion
  • [2017] Unified Formulation for Element-Based Indirect Trajectory Optimization
  • [2016] Advanced special perturbations for asteroids and space debris
  • [2016] Approximate Analytical Solution of the Multiple Revolution Lambert?s Problem
  • [2016] Efficient numerical propagation of planetary close encounters with regularized element methods
  • [2016] Efficient special perturbation techniques for orbital lifetime predictions
  • [2016] GTOC8: Results and Methods of PoliMi-UPM
  • [2016] Impact of the Integration Stop-Condition on the Accuracy of Regularized Orbit Formulations
  • [2016] Multiple Revolution Lambert's Targeting Problem: An Analytical Approximation
  • [2016] New orbital elements for accurate propagation in the Solar System
  • [2016] OCCAM: Optimal Computation of Collision Avoidance Maneuvers
  • [2016] Optimal 3D Orbit Corrections in Curvilinear Coordinates
  • [2016] Orbit Uncertainty Propagation Using Dromo
  • [2016] Quantification of the Performance of Numerical Orbit Propagators
  • [2015] Compact solution of circular orbit relative motion in curvilinear coordinates
  • [2015] Low-Thrust Trajectory Optimization in Dromo Variables
  • [2015] Mission analysis for the ion beam deflection of fictitious asteroid 2015PDC
  • [2015] Mitigation of propagation error in interplanetary trajectories
  • [2015] Numerical criteria for the definition of dynamical regimes in interplanetary orbit propagation
  • [2015] Optimal Low Thrust Orbit Correction In Curvilinear Coordinates
  • [2015] Optimal Low-Thrust-Based Rendezvous Maneuvers
  • [2015] Performance Analysis for Carrier Upper Stage Deorbiting by an Ion Beam Shepherd
  • [2014] A Multiple Scales Solution for the Constant Radial Acceleration Problem
  • [2014] Asymptotic Solution for the Two Body Problem with Radial Perturbing Acceleration
  • [2014] Collision Avoidance Maneuver Optimization
  • [2014] What Does it Take to Capture an Asteroid? A Case Study on Capturing Asteroid 2006 RH120
  • [2013] GNC Design for asteroid orbit modification missions
  • [2013] Multiple Removal of Spent Rocket Upper Stages with an Ion Beam Shepherd
  • [2013] Optimal Impulsive Collision Avoidance
  • [2012] Asymptotic Solution for the Low-Thrust Restricted Two-Body Problem
  • [2012] Earth Delivery of a Small NEO with an Ion Beam Shepherd
  • [2012] Relative Dynamics and Control of an Ion Beam Shepherd Satellite
  • [2012] The SIROCO Asteroid Deflection Demostrator
  • [2011] A new approach on the long term dynamics of neo's under Yarkorsky effect
  • [2011] DROMO: a new regularized orbital propagator
  • [2011] Dynamic stabilization of L2 periodic orbits using attitude-orbit coupling effects
  • [2011] Ion-Beam-Propelled Space Debris
  • [2011] Reverse electric propulsion with electrodynamic tethers
  • [2011] SPACE DEBRIS REMOVAL WITH AN ION BEAM SHEPHERD SATELLITE: DYNAMICS AND CONTROL
  • [2010] A Variational Method for the Propagation of Spacecraft Relative Motion.
  • [2010] A light tether, low-orbit scientific misión at Jupiter.
  • [2010] Performance Analysis of Electrodynamic Tethers as Microsats Deorbiting Systems
  • [2010] Space Debris Removal with Bare Electrodynamic Tethers
  • [2009] EXPLORATION OF THE JUPITER PLASMA TORUS WITH A SELF-POWERED ELECTRODYNAMIC TETHER
  • [2009] On the Orbit Raising Capability of Spinning Electrodynamic Tethers working in Generator Mode.
  • [2009] Saturn Power generation with Electrodynamic Tethers in Polar Orbit.
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• Premios
  • [2017] Best Paper Award del 26th International Symposium in Space Flight Dynamics
• Proyectos de I+D+i
  • [2019] Analisis Dinámico de Misiones Interplanetarias Complejas
  • [2018] DAOCIM: Análisis Dinámico de Misiones Interplanetarias Complejas
  • [2018] IMPROVING LOW EEARTGH ORBIT SECURITY WITH ENHANCED ELECTRIC PROPULSION- LEOS WEEP
  • [2016] Environmental aspects of passive de-orbiting devices
  • [2014] Análisis dinámico, propagación orbital avanzada y simulación de sistemas espaciales complejos
  • [2014] IMPROVING LOW EEARTGH ORBIT SECURITY WITH ENHANCED ELECTRIC PROPULSION- LEOS WEEP
  • [2014] ION BEAM SHEPHERD IOD MISSION (IBS-IOD)
  • [2014] SIMULACION DINAMICA DE SISTEMAS ESPACIALES COMPLEJOS
  • [2013] CONTACLESS ASTEROID ORBIT MODIFICATION SYSTEM AND BINARY ASTEROID ORBIT MODIFICATION
  • [2013] IMPROVING LOW EEARTGH ORBIT SECURITY WITH ENHANCED ELECTRIC PROPULSION- LEOS WEEP
  • [2013] Ion Beam Shepherd IOD Mission
  • [2013] SSASNVII
  • [2013] STARDUST-THE ASTEROID AND SPACE DEBRIS NETWORK (MARIE CURIE)
  • [2012] SIMULACION DINAMICA DE SISTEMAS ESPACIALES COMPLEJOS
  • [2012] SUBVENCIÓN DEL PROGRAMA RAMÓN Y CAJAL. AYUDA PARA LA CONTRATACIÓN
  • [2011] BETs: Propellantless deorbiting of space debris by bare electrodynamic tether
  • [2011] SIMULACION DINAMICA DE SISTEMAS ESPACIALES COMPLEJOS
  • [2010] SIMULACION DINAMICA DE SISTEMAS ESPACIALES COMPLEJOS
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• Registros de Software
  • [2014] OCCAM (Optimal Computation of Collision Avoidance Maneuvers)
  • [2014] OCCAM - Optimal Computation of Collision Avoidance Maneuvers
• Responsabilidades
  • [2015] Director de Escuela de verano Universidad Internacional Menéndez Pelayo (UIMP)
  • [2014] Science and Technology Challenges of Space Debris Removal and Asteroid Deflection
• Tesis Doctorales
  • [2017] Advanced Orbit Propagation Methods Applied to Asteroids and Space Debris
  • [2017] Propagation and Optimal Control of Space Trajectories Using Perturbation Methods
  • [2015] High Fidelity Models for Near-Earth Object Dynamics