Observatorio de I+D+i UPM
• ESPAÑOL
• ENGLISH
INVESTIGADORES
ESTRUCTURAS DE I+D+I
ACTIVIDAD INVESTIGADORA
INNOVACIÓN
Investigador
Claudio Bombardelli
Categoría Investigador
TITULAR UNIVERSIDAD
Escuela UPM
E.T.S.I. AERONÁUTICA Y DEL ESPACIO
Departamento:
FÍSICA APLICADA A LAS INGENIERÍAS AERONÁUTICA Y NAVAL
Area Conocimiento
INGENIERIA AEROESPACIAL
Grupo de Investigación:
Dinámica Espacial (SDG-UPM)
Email (Directorio UPM)
claudio.bombardelli
upm.es
Teléfono (Directorio UPM)
910675911
Datos de Memorias relacionados
Proyectos de I+D+i y generación de recursos
22 Proyectos de I+D+i
1: (2010)
SIMULACION DINAMICA DE SISTEMAS ESPACIALES COMPLEJOS
2: (2011)
BETs: Propellantless deorbiting of space debris by bare electrodynamic tether
3: (2011)
Electrodynamic Tethers: Reversed Electric Propulsion with Electrodynamic Tethers
4: (2011)
SIMULACION DINAMICA DE SISTEMAS ESPACIALES COMPLEJOS
5: (2012)
SIMULACION DINAMICA DE SISTEMAS ESPACIALES COMPLEJOS
6: (2012)
SSASNVII: SN-VII NEO Impact Effects and Mitigation Measures
7: (2012)
SUBVENCIÓN DEL PROGRAMA RAMÓN Y CAJAL. AYUDA PARA LA CONTRATACIÓN
8: (2013)
CONTACLESS ASTEROID ORBIT MODIFICATION SYSTEM AND BINARY ASTEROID ORBIT MODIFICATION
9: (2013)
IMPROVING LOW EEARTGH ORBIT SECURITY WITH ENHANCED ELECTRIC PROPULSION- LEOS WEEP
10: (2013)
Ion Beam Shepherd IOD Mission
11: (2013)
LEOSWEEP: Improving Low Earth Orbit Security With Enhanced Electric Propulsion
12: (2013)
SSASNVII
13: (2013)
Stardust: Stardust-The Asteroid and Space Debris Network
14: (2013)
STARDUST-THE ASTEROID AND SPACE DEBRIS NETWORK (MARIE CURIE)
15: (2014)
Análisis dinámico, propagación orbital avanzada y simulación de sistemas espaciales complejos
16: (2014)
IMPROVING LOW EEARTGH ORBIT SECURITY WITH ENHANCED ELECTRIC PROPULSION- LEOS WEEP
17: (2014)
ION BEAM SHEPHERD IOD MISSION (IBS-IOD)
18: (2014)
SIMULACION DINAMICA DE SISTEMAS ESPACIALES COMPLEJOS
19: (2016)
Environmental aspects of passive de-orbiting devices
20: (2018)
DAOCIM: Análisis Dinámico de Misiones Interplanetarias Complejas
21: (2018)
IMPROVING LOW EEARTGH ORBIT SECURITY WITH ENHANCED ELECTRIC PROPULSION- LEOS WEEP
22: (2019)
Analisis Dinámico de Misiones Interplanetarias Complejas
Formación de Investigadores y Movilidad
3 Tesis Doctorales
1: (2015)
High Fidelity Models for Near-Earth Object Dynamics
2: (2017)
Advanced Orbit Propagation Methods Applied to Asteroids and Space Debris
3: (2017)
Propagation and Optimal Control of Space Trajectories Using Perturbation Methods
Difusión de Resultados de Investigación
64 Artículos en revistas
1: (2009)
Electrodynamic Tether at Jupiter-II: Fast Moon Tour After Capture
2: (2009)
Jupiter Power Generation with Electrodynamic Tethers at Constant Orbital Energy.
3: (2010)
Asymptotic Solution for the Current Profile of Passive Bare Electrodynamic Tethers
4: (2010)
On the Stability of Artificial Equilibrium Points in the Circular Restricted Three Body Problem
5: (2010)
Three-Body Dynamics and Self-Powering of an Electrodynamic Tether in a Plasmasphere
6: (2011)
ADAPTIVE SCHEME FOR ACCURATE ORBIT PROPAGATION
7: (2011)
Asymptotic Solution for the Two-Body Problem with Constant Tangencial Acceleration
8: (2011)
Ion Beam Shepherd for Asteroid Deflection
9: (2011)
Ion Beam Shepherd for Contactless Space Debris Removal
10: (2011)
On the stability of artificial equilibrium points in the circular restricted three-body problem
11: (2012)
A NEW APPROACH ON THE LONG TERM DYNAMICS OF NEO'S UNDER YARKOVSKY EFFECT
12: (2012)
A Proposed Two-Stage Two-Tether Scientific Mission at Jupiter
13: (2012)
Accurate analytical approximation of asteroid deflection with constant tangential thrust
14: (2012)
Adaptative scheme for Accurate orbit propagation
15: (2012)
Dynamic stabilization of L2 periodic orbits using attitude-orbit coupling effects
16: (2012)
Dynamics of a Tethered Observatory at Jupiter
17: (2012)
Periodic Orbits of a Hill-Tether Problem Originated from Collinear Points
18: (2012)
Power Density of a Bare Electrodynamic Tether Generator
19: (2012)
STABLE ARTIFICIAL EQUILIBRIUM POINTS IN THE MARS-PHOBOS SYSTEM
20: (2012)
The ion beam shepherd: A new concept for asteroid deflection
21: (2013)
A new set of integrals of motion to propagate the perturbed two-body problem
22: (2013)
Deorbiting Performance of Bare Electrodynamic Tethers in Inclined Orbits
23: (2013)
The ion beam shepherd: A new concept for asteroid deflection
24: (2013)
The ion beam shepherd: A new concept for asteroid deflection
25: (2014)
Analytical formulation of impulsive collision avoidance dynamics
26: (2014)
TIME ELEMENTS FOR ENHANCED PERFORMANCE OF THE DROMO ORBIT PROPAGATOR
27: (2015)
Impact of Nonideal Effects on Bare Electrodynamic Tether Performance
28: (2015)
Impact of nonideal effects on bare electrodynamic tether performance
29: (2015)
LOW-THRUST TRAJECTORY OPTIMIZATION IN DROMO VARIABLES
30: (2015)
MITIGATION OF PROPAGATION ERROR IN INTERPLANETARY TRAJECTORIES
31: (2015)
Non-singular orbital elements for special perturbations in the two-body problem
32: (2015)
Optimal Impulsive Collision Avoidance in Low Earth Orbit
33: (2015)
Optimal Impulsive Collision Avoidance in Low Earth Orbit
34: (2015)
OPTIMAL LOW-THRUST-BASED RENDEZVOUS MANEUVERS
35: (2015)
Temporarily Captured Asteroids as a Pathway to Affordable Asteroid Retrieval Missions
36: (2016)
APPROXIMATE ANALYTICAL SOLUTION OF THE MULTIPLE REVOLUTION LAMBERT'S TARGETING PROBLEM
37: (2016)
Approximate Solution of Non-linear Circular Orbit Relative Motion in Curvilinear Coordinates
38: (2016)
COMPACT SOLUTION OF CIRCULAR ORBIT RELATIVE MOTION IN CURVILINEAR COORDINATES
39: (2016)
Compact solution of circular orbit relative motion in curvilinear coordinates
40: (2016)
CONTACTLESS ION BEAM ASTEROID DESPINNING
41: (2016)
GTOC8: RESULTS AND METHODS OF POLIMI-UPM
42: (2016)
OPTIMAL LOW THRUST ORBIT CORRECTION IN CURVILINEAR COORDINATES
43: (2016)
Optimal low thrust orbit correction in curvilinear coordinates
44: (2016)
OPTIMAL 3D ORBIT CORRECTIONS IN CURVILINEAR COORDINATES
45: (2017)
Accurate numerical orbit propagation of planetary close encounters
46: (2017)
Accurate numerical orbit propagation of planetary close encounters
47: (2017)
Accurate orbit propagation in the presence of planetary close encounters
48: (2017)
Approximate solutions of non-linear circular orbit relative motion in curvilinear coordinates
49: (2017)
Deflection of fictitious asteroid 2017 PDC: Ion beam vs. kinetic impactor
50: (2017)
Deflection of fictitious asteroid 2017 PDC: Ion beam vs. kinetic impactor
51: (2017)
Environmental effect of space debris repositioning
52: (2017)
Environmental effect of space debris repositioning
53: (2017)
Optimal Continuous-Thrust Rephasing Maneuver in Circular Orbit
54: (2017)
Optimal Continuous-Thrust Rephasing Maneuver in Circular Orbit
55: (2017)
Orbit covariance propagation via quadratic-order state transition matrix in curvilinear coordinates
56: (2018)
Approximate Analytical Solution of the Multiple Revolution Lambert's Targeting Problem
57: (2018)
Relative control of an ion beam shepherd satellite using the impulse compensation thruster
58: (2018)
The circular restricted three-body problem in curvilinear coordinates
59: (2019)
A preliminary design procedure for an ion-beam shepherd mission
60: (2019)
Multiple scales asymptotic solution for the constant radial thrust problem
61: (2019)
Non-averaged regularized formulations as an alternative to semi-analytical orbit propagation methods
62: (2019)
Rate and Collision Probability of Tethers and Sails Against Debris or Spacecraft
63: (2019)
RESIDENT SPACE OBJECT PROPER ORBITAL ELEMENTS
64: (2019)
Uncertainty propagation in the N-body problem using Dromo elements
2 Capítulos de libros
1: (2013)
Ion beam shepherd satellite for space debris removal
2: (2016)
Advanced orbit propagation methods and application to space debris collision avoidance
1 Conferencias invitadas en congresos
1: (2010)
Electrodynamic Tethers for Space Debris Removal,
48 Ponencia en Congresos
1: (2009)
EXPLORATION OF THE JUPITER PLASMA TORUS WITH A SELF-POWERED ELECTRODYNAMIC TETHER
2: (2009)
On the Orbit Raising Capability of Spinning Electrodynamic Tethers working in Generator Mode.
3: (2009)
Saturn Power generation with Electrodynamic Tethers in Polar Orbit.
4: (2010)
A light tether, low-orbit scientific misión at Jupiter.
5: (2010)
A Variational Method for the Propagation of Spacecraft Relative Motion.
6: (2010)
Performance Analysis of Electrodynamic Tethers as Microsats Deorbiting Systems
7: (2010)
Space Debris Removal with Bare Electrodynamic Tethers
8: (2011)
A new approach on the long term dynamics of neo's under Yarkorsky effect
9: (2011)
DROMO: a new regularized orbital propagator
10: (2011)
Dynamic stabilization of L2 periodic orbits using attitude-orbit coupling effects
11: (2011)
Ion-Beam-Propelled Space Debris
12: (2011)
Reverse electric propulsion with electrodynamic tethers
13: (2011)
SPACE DEBRIS REMOVAL WITH AN ION BEAM SHEPHERD SATELLITE: DYNAMICS AND CONTROL
14: (2012)
Asymptotic Solution for the Low-Thrust Restricted Two-Body Problem
15: (2012)
Earth Delivery of a Small NEO with an Ion Beam Shepherd
16: (2012)
Relative Dynamics and Control of an Ion Beam Shepherd Satellite
17: (2012)
The SIROCO Asteroid Deflection Demostrator
18: (2013)
GNC Design for asteroid orbit modification missions
19: (2013)
Multiple Removal of Spent Rocket Upper Stages with an Ion Beam Shepherd
20: (2013)
Optimal Impulsive Collision Avoidance
21: (2014)
A Multiple Scales Solution for the Constant Radial Acceleration Problem
22: (2014)
Asymptotic Solution for the Two Body Problem with Radial Perturbing Acceleration
23: (2014)
Collision Avoidance Maneuver Optimization
24: (2014)
What Does it Take to Capture an Asteroid? A Case Study on Capturing Asteroid 2006 RH120
25: (2015)
Compact solution of circular orbit relative motion in curvilinear coordinates
26: (2015)
Low-Thrust Trajectory Optimization in Dromo Variables
27: (2015)
Mission analysis for the ion beam deflection of fictitious asteroid 2015PDC
28: (2015)
Mitigation of propagation error in interplanetary trajectories
29: (2015)
Numerical criteria for the definition of dynamical regimes in interplanetary orbit propagation
30: (2015)
Optimal Low Thrust Orbit Correction In Curvilinear Coordinates
31: (2015)
Optimal Low-Thrust-Based Rendezvous Maneuvers
32: (2015)
Performance Analysis for Carrier Upper Stage Deorbiting by an Ion Beam Shepherd
33: (2016)
Advanced special perturbations for asteroids and space debris
34: (2016)
Approximate Analytical Solution of the Multiple Revolution Lambert?s Problem
35: (2016)
Efficient numerical propagation of planetary close encounters with regularized element methods
36: (2016)
Efficient special perturbation techniques for orbital lifetime predictions
37: (2016)
GTOC8: Results and Methods of PoliMi-UPM
38: (2016)
Impact of the Integration Stop-Condition on the Accuracy of Regularized Orbit Formulations
39: (2016)
Multiple Revolution Lambert's Targeting Problem: An Analytical Approximation
40: (2016)
New orbital elements for accurate propagation in the Solar System
41: (2016)
OCCAM: Optimal Computation of Collision Avoidance Maneuvers
42: (2016)
Optimal 3D Orbit Corrections in Curvilinear Coordinates
43: (2016)
Orbit Uncertainty Propagation Using Dromo
44: (2016)
Quantification of the Performance of Numerical Orbit Propagators
45: (2017)
Deflection of Fictitious Asteroid 2017 PDC: Ion Beam vs. Kinetic Impactor
46: (2017)
Last-minute semi-analytical asteroid deflection by nuclear explosion
47: (2017)
Last-minute semi-analytical asteroid deflection by nuclear explosion
48: (2017)
Unified Formulation for Element-Based Indirect Trajectory Optimization
Explotación de Resultados y Transferencia de Tecnología
5 Patentes
1: (2012)
Sistema de modificación de la posición y actitud de cuerpos en órbita por medio de satélites guia
2: (2017)
Sistema de generación de potencia eléctrica en órbita por medio de cables conductores flotantes
3: (2017)
Sistema de propulsión en órbita por medio de cables conductores flotantes
4: (2018)
System for generating electrical power in orbit by means of floating conductor cables
5: (2018)
System for in-orbit propulsion via floating conductor cables
2 Registros de Software
1: (2014)
OCCAM - Optimal Computation of Collision Avoidance Maneuvers
2: (2014)
OCCAM (Optimal Computation of Collision Avoidance Maneuvers)
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S2i 2023 Observatorio de investigación @ UPM con la colaboración del Consejo Social UPM
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