Name: 6th International Conference on Astrodynamics Tools and Techniques (ICATT)
Start: 2016-03-14T08:00:00+01:00
End: 2016-03-17T13:00:00+01:00
Location: Darmstadtium

6th International Conference on Astrodynamics Tools and Techniques (ICATT)

from Monday, 14 March 2016 (08:00) to Thursday, 17 March 2016 (13:00)

Monday, 14 March 2016

08:00

08:00 - 09:30
Room: Main Conference Room

09:30 Rosetta mission analysis tools and techniques
Rosetta mission analysis tools and techniques
09:30 - 10:30
Room: Main Conference Room

10:30 Trajectory design around Churyumov-Gerasimenko and its optical navigation
Trajectory design around Churyumov-Gerasimenko and its optical navigation
10:30 - 11:30
Room: Main Conference Room

11:30 Coffee Break
Coffee Break
11:30 - 11:50
Room: Main Conference Room

11:50 WebGeocalc and Cosmographia demos by NAIF
WebGeocalc and Cosmographia demos by NAIF
11:50 - 12:50
Room: Main Conference Room

12:50 Lunch break
Lunch break
12:50 - 14:00

14:00 GMAT (General Mission Analysis Tool) at NASA.
GMAT (General Mission Analysis Tool) at NASA.
14:00 - 15:30
Room: Main Conference Room

15:30 Coffee Break
Coffee Break
15:30 - 15:50
Room: Main Conference Room

15:50 Continuation of GMAT (General Mission Analysis Tool) at NASA.
Continuation of GMAT (General Mission Analysis Tool) at NASA.
15:50 - 17:20
Tuesday, 15 March 2016

07:00

07:00 - 08:00
Room: 3.11 Foyer

08:00

08:00 - 08:20
Room: 3.02 Hassium
08:20
08:20 - 10:20
Room: 3.02 Hassium
Contributions

09:00 Modeling and Performance Evaluation of Multistage Launch Vehicles through Firework Algorithm - Marco Pallone (Sapienza - University of Rome)

09:20 An RST Design Approach for the Launchers Flight Control System - Adrian Danciu (University Politecnica of Bucharest)

09:40 Innovative Strategy for Z9 Reentry - Elena Vellutini (Aizoon)
08:20 - 10:20
Room: 3.03 Germanium
Contributions

08:20 Modelling and Simulation of Autonomous Cubesats for Orbital Debris Mitigation - Christopher Sprague (Rensselaer Polytechnic Institute)

08:40 OCCAM: Optimal Computation of Collision Avoidance Maneuvers - Javier Hernando-Ayuso (The University of Tokyo)

09:00 Innovative Method for the Computation of Safety Re-entry Area Based on the Probability of Uncertainities in the Input Parameters - Emilio De Pasquale (European Space Agency) Simone Flavio Rafano Carnà (Politecnico di Milano)

09:20 Conjunction Risk Assessment and Avoidance Maneuver Planning Tools - Saika Aida (DLR/GSOC)

09:40 Attitude/orbit simulation tools for drag-augmented deorbiting - The DGNC Project - Florio Dalla Vedova (LuxSpace)

10:00 Applicability of COBRA concept to de-tumbling space debris objects - Thomas Peters (GMV)
08:20 - 10:20
Room: 3.06 Xenon
Contributions

08:20 An efficient code to solve the Kepler equation for elliptic and hyperbolic orbits - Virginia Raposo Pulido (SDG-UPM)

08:40 A fast and efficient algorithm for onboard LEO intermediary propagation - Martin Lara (Space Dynamics Group, Polytechnic University of Madrid, and GRUCACI, University of La Rioja)

09:00 SIRIUS-DV: The new Flight Dynamics algorithms for the future CNES missions - IVÁN LLAMAS (GMV)

09:20 A semi-analytical orbit propagator program for Highly Elliptical Orbits - Juan Félix San-Juan (Scientific Computing Group (GRUCACI), University of La Rioja)

09:40 DESEO Design Engineering Suite for Earth Observation - Federico Letterio (Deimos Space)
10:20
10:20 - 10:40
Room: 3.11 Foyer
Contributions

10:20 A new Mars EDL mission design and simulation tool - MEDLMDST - Shuang Li (Nanjing University of Aeronautics and Astronautics)

10:20 The Horizon 2020 project ReDSHIFT: Revolutionary Design of Spacecraft through Holistic Integration of Future Technologies - Alessandro Rossi (IFAC-CNR)

10:20 The ESPaCE consortium as a European producer of spacecraft and natural moon ephemerides - Valéry Lainey (IMCCE-Observatoire de Paris) William Thuillot (Paris Observatory)

10:20 Using accurate ephemerides of solar system objects for autonomous navigation - Yann Duchemin (IMCCE, Obs. de Paris/PSL Research University)

10:20 Caviar: a Software Package for the Astrometric Reduction of Spacecraft Images - Nicholas Cooper (Queen Mary University of London)

10:20 The NAROO project for overcoming past, current, and future ephemeris errors - Vincent Robert (IPSA & IMCCE - OBSPM)

10:20 Low Thrust transfers applications for Earth Orbiting Satellites and Constellations - Cerreto Marco (Thales Alenia Space)

10:20 STAVOR: Transition from desktop to new mobile platforms - Luc Maisonobe (CS SI)

10:20 Dromobile: A multi-platform tool for orbit propagation on mobile devices - Javier Hernando-Ayuso (The University of Tokyo)

10:20 Analysis of spacecraft trajectories in proximity to small bodies: Phobos & NEO - Daniel HESTROFFER (IMCCE/PAris observatory - CNRS) Siegfried EGGL (IMCCE/PAris observatory - CNRS)

10:20 Modular Fuzzy Interacting Multiple Model for Maneuvering Target Tracking - Zhengyang Mao (National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnical University)

10:20 Application of Kalman Filters in Orbit Determination: A Literature Survey - Abdul Manarvi (Embry-Riddle Aeronautical University)

10:20 open-source publication: a strategic choice for private companies - Luc Maisonobe (CS SI)

10:20 Mercury rotational state estimation applied to the BepiColombo Mission: an optimized approach on the selection of optical observations - Davide Silvestri (University of Bologna)
10:40
10:40 - 12:40
Room: 3.02 Hassium
Contributions

11:00 Launch vehicle multibody dynamics modeling framework for preliminary design studies - Paul Acquatella (DLR, German Aerospace Center)

11:20 Launch Vehicle Design and GNC Sizing with ASTOS - Francesco Cremaschi (Astos Solutions GmbH)

11:40 Model Validation Framework for Launchers: Post-Flight Performance Analysis - Juan Antonio Bejar-Romero (GMV Aerospace and Defence S.A.U.)

12:00 Wave-Based Attitude Control of Launch vehicle with Structural Flexibility and Fuel Sloshing Dynamics - David McKeown (University College Dublin)
10:40 - 12:40
Room: 3.03 Germanium
Contributions

10:40 A Series for the Collision Probability in the Short-Encounter Model - Ricardo García-Pelayo (Universidad Politécnica de Madrid)

11:00 Probabilistic orbit lifetime assessment with ESA’s DRAMA/OSCAR tool - Vitali Braun (IMS Space Consultancy GmbH)

11:20 Debris operational support through the web applications - Daniel Novak (CGI)

11:40 Tools and Techniques Supporting the Operational Collision Avoidance Process at ESOC - Klaus Merz (ESA)

12:00 Sensor fusion analysis for HEO space debris using BAS3E - Carlos YANEZ (GMV Innovating Solutions)

12:20 Fragmentation Event Model and Assessment Tool (FREMAT) supporting in-orbit fragmentation analysis - Roxana Larisa Andrisan (DEIMOS Space)
10:40 - 12:40
Room: 3.06 Xenon
Contributions

11:00 Hybrid SGP4: tools and methods - Juan Félix San-Juan (Scientific Computing Group (GRUCACI), University of La Rioja)

11:20 Proposed algorithm for on-board maneouvres calculation - Itziar Barat (Deimos Space @ ESA/ESTEC)

11:40 Fast Low Earth Orbit Acquisition Plan Optimiser - Sérgio Brás (National Trainee @ ESA/ESTEC)

12:00 An implementation of SGP4 in non-singular variables using a functional paradigm - Pablo Pita Leira (Goetzfried Professionals GmbH)

12:20 New tool for finding periodic Halo orbits: the solver of a Spacecraft Simulator (ESPSS -EcosimPro® European Space Propulsion System Simulation) - christophe Koppel (KopooS Consulting Ind.)
12:40 Lunch
Lunch
12:40 - 14:00
14:00
14:00 - 15:40
Room: 3.03 Germanium
Contributions

14:00 Space dynamics software ELECTRA - Philippe PAVERO (CAPGEMINI)

14:20 Computer Graphics for Space Debris - Mehta Piyush (University of Strathclyde)

14:40 Debris de-tumbling & de-orbiting by elastic tether & wave-based control - W. J. O'Connor (School of Mechanical and Materials Engineering. University of College Dublin)

15:00 An Access Point to ESA’s Space Debris Data: The Space Debris Office Web Based Tools - Quirin Funke (IMS Space Consultancy GmbH at ESA)

15:20 From end-of-life to impact on ground: An overview of ESA’s tools and techniques to predicted re-entries from the operational orbit down to the Earth’s surface - Stijn Lemmens (European Space Agency)
14:00 - 15:40
Room: 3.06 Xenon
Contributions

14:00 Indirect Planetary Capture via Periodic Orbits about Libration Points - Xiangyu Li (Beijing Institude of Technology)

14:20 Coupled dynamics of large space structures in Lagrangian points - Lorenzo Bucci (Politecnico di Milano)

14:40 Orbit Determination through Global Positioning Systems: A Literature survey of Past and Present Investigations - Abdul Manarvi (Embry-Riddle Aeronautical University)

15:00 The true nature of the equilibrium for geostationary objects, applications to the high area-to-mass ratio debris - Fabien Gachet (University of Rome 'Tor Vergata')

15:20 A Simulation Tool to Design of Satellite Formations - AYKUT kutlu (Middle East Technical University)
15:40 Coffee break / Poster Session / Booth Exhibition
Coffee break / Poster Session / Booth Exhibition
15:40 - 16:00
Room: 3.11 Foyer
16:00
16:00 - 18:00
Room: 3.02 Hassium
Contributions

16:00 Evaluation of satellite aerodynamic and radiation pressure acceleration models using accelerometer data - Eelco Doornbos (Delft University of Technology)

16:20 Using the attitude response of aerostable spacecraft to determine thermospheric wind - Josep Virgili (Naval Postgraduate School) Peter Roberts (University of Manchester)

16:40 The SPENVIS Next Generation - Neophytos Messios (BIRA-IASB (Belgium))

17:00 Planetary Orbital Dynamics (PlanODyn) suite for long term propagation in perturbed environment - Camilla Colombo (Astronautics Research Group, University of Southampton)

17:20 Application of the Attitude Analysis of Dynamics and Disturbances Tool in EUMETSAT’s study on thruster’s allocation and momentum management for meteorological spacecrafts - Nuno Paulino (GMV)

17:40 DELTA (Debris Environment Long-Term Analysis) - Benjamin Bastida Virgili (ESA/ESOC)
16:00 - 18:00
Room: 3.03 Germanium
Contributions

16:20 Spacecraft formation control using analytical integration of Gauss variational equations - Mohamed Khalil Ben Larbi (Univestität Braunschweig)

16:40 ASTOS 8.1 - Mission Performance Analysis, System Concept Analysis and Other New Features - Sven Weikert (Astos Solutions GmbH)

17:00 Capitalizing on Relative Motion in Electrostatic Detumble of Axi-Symmetric GEO Objects - Trevor Bennett (University of Colorado Boulder)

17:20 Analysis of Electric Propulsion Capabilities in Establishment and Keeping of Formation Flying Nanosatellites - EVIATAR EDLERMAN (Technion)

17:40 Robust Control Design Methodology of the 6DoF Flight-Formation of PROBA-3 - Daniel Serrano (SENER)
16:00 - 18:00
Room: 3.06 Xenon
Contributions

16:00 Evaluation of Iterative Analytical Techniques for Interplanetary Orbiter Missions - PARVATHI SP (INDIAN INSTITUTE OF SPACE SCIENCE AND TECHNOLOGY)

16:20 Tube Dynamics and Low Energy Trajectory from the Earth to the Moon in the Coupled Three-Body System - Kaori Onozaki (Waseda university)

16:40 Efficient numerical propagation of planetary close encounters with regularized element methods - Davide Amato (Technical University of Madrid)

17:00 Coupling High Fidelity Body Modeling with Non-Keplerian Dynamics to Design AIM-MASCOT-2 Landing Trajectories on Didymos Binary Asteroid - Fabio Ferrari (Politecnico di Milano)

17:20 Dynamics in the center manifold around equilibrium points in Periodically Perturbed Three-Body Problems - Bastien Le Bihan (ISAE/Supaéro)

17:40 Simulation of autonomous landing near a plume source in a tiger stripe canyon on the south pole of Enceladus - Konstantinos Konstantinidis (Universität der Bundeswehr München)
18:00 Welcome cocktail / Poster Session / Booth Exhibition
Welcome cocktail / Poster Session / Booth Exhibition
18:00 - 19:30
Room: 3.11 Foyer
Wednesday, 16 March 2016

07:30

07:30 - 08:00
Room: 3.11 Foyer
08:00
08:00 - 10:00
Room: 3.03 Germanium
Contributions

08:00 An Interactive Trajectory Design Environment Leveraging Dynamical Structures in Multi-Body Regimes - Andrew Cox (Purdue University)

08:20 High-fidelity small body lander simulations - Stefaan Van wal (University of Colorado Boulder)

08:40 NEO Threat Mitigation Software Tools - Juan Luis Cano (Elecnor Deimos)

09:00 Monte Carlo Simulation of a Triple Flyby Capture at Jupiter Using Paramat - Darrel Conway (Thinking Systems, Inc.)

09:20 Navigation Tools at ESOC Mission Analysis Section - Amedeo Rocchi (GMV/ESOC)

09:40 SNAPPShot: Suite for the Numerical Analysis of Planetary Protection - Francesca Letizia (University of Southampton)
08:00 - 10:00
Room: 3.02 Hassium
Contributions

08:00 A Self-Boundary Fall Free Algorithm for 2D Open Dimension Rectangle Packing Problem of Satellite Module - Junjie Yang (National University of Defense Technology)

08:20 WORHP Multi-Core Interface, Parallelisation Approaches for an NLP Solver - Sören Geffken (Universität Bremen)

08:40 Non-Keplerian Trajectory Planning via Heuristic-Guided Objective Reachability Analysis - David Surovik (University of Colorado at Boulder)

09:00 Analytical Approximation for the Multiple Revolution Lambert's Problem - Claudio Bombardelli (Space Dynamics Group, Technical University of Madrid)

09:40 Understanding concepts of Optimization and Optimal Control with WORHP Lab - Matthias Knauer (Universität Bremen)
10:00 Coffee break / Poster Session / Booth Exhibition
Coffee break / Poster Session / Booth Exhibition
10:00 - 10:20
Room: 3.11 Foyer
10:20
10:20 - 12:20
Room: 3.03 Germanium
Contributions

10:20 Trajectory Design Tools for Libration and Cis-Lunar Environments - Andrew Cox (Purdue University)

10:40 Asteroid Rendezvous Uncertainty Propagation - Marc Balducci (University of Colorado at Boulder)

11:00 Some validation checks of "TriaXOrbitaL" tool : Earth-Moon L2 orbit, Sun-Moon perturbations. - christophe Koppel (KopooS Consulting Ind.)

11:20 Extended Tisserand graph and multiple lunar swing-by design with Sun perturbation - Daniel Garcia Yarnoz (ISAS/JAXA)

11:40 Solar System geometry tools with SPICE for ESA's planetary missions - Marc Costa (Telespazio VEGA UK SL for ESA)

12:00 ESA's Asteroid Impact Mission: Mission Analysis and Payload Operations state of the art - Fabio Ferrari (Politecnico di Milano)
10:20 - 12:20
Room: 3.02 Hassium
Contributions

10:40 Optimal real-time landing using deep networks - Alexander Wittig (ESA Advanced Concepts Team)

11:00 Development, validation and test of optical based algorithms for autonomous planetary landing - Marco Ciarambino (Politecnico di Milano - Aerospace Science and Technology Dept.)

11:20 Massively parallel optimization of low-thrust trajectories on GPUs - Alexander Wittig (ESA Advanced Concepts Team)

11:40 On Ultimately the Most Highly Inclined, the Most Concise Solar Polar Trajectory with Practically the Shortest Period - Junichiro Kawaguchi (JAXA)

12:00 Spiderman Spacecraft: Tethered Asteroid Hopping in the Main Belt - Alexander Wittig (ESA Advanced Concepts Team)
12:20 Lunch
Lunch
12:20 - 13:20
13:20
13:20 - 15:20
Room: 3.03 Germanium
Contributions

13:40 An Update on NAIF's Package of "SPICE" Astrodynamics Tools - Charles Acton (NASA/JPL)

14:00 SMART-UQ: Uncertainty Quantification Toolbox for Generalized Intrusive and Non Intrusive Polynomial Algebra - Annalisa Riccardi (Strathclyde University)

14:20 CelestLab: Spaceflight Dynamics Toolbox for Mission Analysis - Alain LAMY (CNES)

14:40 from low level toolbox to orbit determination: handling users requests in Orekit - Luc Maisonobe (CS SI)

15:00 The Pointing Error Engineering Tool (PEET): From Prototype to Release Version - Marc Hirth (Astos Solutions GmbH)
13:20 - 15:20
Room: 3.02 Hassium
Contributions

13:20 Processing Two Line Element sets to facilitate re-entry prediction of spent rocket bodies from the geostationary transfer orbit - Aleksander Lidtke (University of Southampton)

13:40 Observation of orbital debris with space-based space surveillance constellations - Cristina Santana (GMV)

14:00 Techniques for assessing space object cataloguing performance during design of surveillance systems - Jan Siminski (ESA/ESOC)

14:20 MONTE: The Next Generation of Mission Design and Navigation Software - Scott Evans (JPL)

14:40 New orbital elements for accurate orbit propagation in the Solar System - Giulio Bau' (University of Pisa)

15:00 Recursive estimation of non-gravitational perturbations from satellite observations - Lamberto Dell'Elce (Université de Liège)
15:20 Coffee break / Poster Session / Booth Exhibition
Coffee break / Poster Session / Booth Exhibition
15:20 - 15:40
Room: 3.11 Foyer
15:40
15:40 - 17:40
Room: 3.03 Germanium
Contributions

15:40 WebGeocalc: Web Interface to SPICE - Boris Semenov (NASA/JPL)

16:20 Rugged: an open-source sensor-to-terrain mapping tool - Luc Maisonobe (CS SI)

16:40 A Comparative Study of Programming Languages for Next-Generation Astrodynamics Systems - Helge Eichhorn (Technische Universität Darmstadt Department of Computer Integrated Design)

17:00 poliastro: : An Astrodynamics library written in Python with Fortran performance - Juan Luis Cano (Universidad Politécnica de Madrid)
15:40 - 17:40
Room: 3.02 Hassium
Contributions

15:40 Assessing Orbit Determination Requirement with Unscented Transformation: Case Study of a Lunar CubeSat Mission - Sun Hur-Diaz (Emergent Space Technologies, Inc.)

16:00 A TLE-based Representation of Precise Orbit Prediction Results - Jizhang Sang (Wuhan University)

16:20 First results of IOTA (In-Orbit Tumbling Analysis) - Patrik Kärräng (Hyperschall Technologie Göttingen (HTG))

16:40 Debris cloud analytical propagation for a space environmental index - Francesca Letizia (University of Southampton)

17:00 Design of Optimal Observation Strategy for Re-entry Prediction Improvement of GTOs Upper Stages - Mirco Rasotto (Dinamica Srl)

17:20 From Simulation to Reality: Cataloguing of Objects in from Ground-based Optical Observations - Raul Domínguez-González (DEIMOS Space)
17:40 Poster Session / Booth Exhibition Ends
Poster Session / Booth Exhibition Ends
17:40 - 18:00
Room: 3.11 Foyer

19:30 Gala dinner
Gala dinner
19:30 - 22:30
Thursday, 17 March 2016
08:00
08:00 - 10:00
Room: 2.02 Chromium
Contributions

08:00 A Sequential Method to Compute Multiobjective Optimal Low-Thrust Earth Orbit Transfers - DAVID MORANTE (Universidad Carlos III ( Madrid ))

08:20 Low Thrust Trajectory Optimization for Autonomous Asteroid Rendezvous Missions - Anne Schattel (University of Bremen)

08:40 About Combining Tisserand Graph Gravity-Assist Sequencing with Low-Thrust Trajectory Optimization - Maiwald Volker (DLR Institute of Space Systems)

09:00 Enhancement of DLR/GSOC FDS for Low Thrust Orbit Transfer and Control - Stefanie Lück (DLR)

09:20 Low thrust orbit transfer optimiser for a Spacecraft Simulator (ESPSS -EcosimPro® European Space Propulsion System Simulation) - christophe Koppel (KopooS Consulting Ind.)

09:40 CAMELOT - Computational-Analytical Multi-fidelity Low-thrust Optimisation Toolbox - Marilena Di Carlo (University of Strathclyde)
08:00 - 10:00
Room: 2.03 Vanadium
Contributions

08:00 Aerodynamic categorization of spacecraft in low Earth orbits - Bent Fritsche (HTG)

08:20 PETbox: Flight Qualified Tools for Atmospheric Flight - Mariano Sánchez Nogales (DEIMOS Space S.L.U.)

08:40 Real-Time Atmospheric Entry Trajectory Generation Using Parametric Sensitivities - David Seelbinder (DLR)

09:20 IXV GNC verification from inspection to flight demonstration - Rodrigo Haya Ramos (SENER)
08:00 - 10:00
Room: 2.04 Titanium
Contributions

08:00 Experimental evaluation of Model Predictive and Inverse Dynamics Control for spacecraft proximity and docking maneuvers - Marcello Romano (Naval Postgraduate School)

08:20 GNC Techniques for Proximity Manoeuvring with Uncooperative Space Objects - Riccardo Benvenuto (Politecnico di Milano)

08:40 JOSCAR/JDRAGON: Tools for Maneuver Strategy Computation Developed in Java and using PATRIUS - Ivan Sumelzo Martinez (Centre National d’Etudes Spatiales, French Space Agency)

09:00 An open-source simulator for spacecraft robotic arm dynamic modeling and control. - Josep Virgili (Naval Postgraduate School)

09:20 GNC simulation tool for active debris removal with a robot arm - Matthias Reiner (DLR)
10:00 Cofee break
Cofee break
10:00 - 10:20
Room: 0.04 Dynamicum
10:20
10:20 - 12:20
Room: 2.02 Chromium
Contributions

10:20 Low Thrust Trajectory Design and Optimization: Case Study of a Lunar CubeSat Mission - Ravishankar Mathur (Emergent Space Technologies, Inc.)

10:40 Low-Thrust Transfers from Distant Retrograde Orbits to L2 Halo Orbits in the Earth-Moon System - Nathan Parrish (University of Colorado Boulder)

11:00 Optimization of low thrust multi-revolution orbital transfers using the method of dual numbers - Ilia Nikolichev (Moscow Aviation Institute)

11:20 Joint Optimization of Main Design Parameters of Electric Propulsion System and Spacecraft Trajectory - MIn Thein (Moscow Aviation Institute)

11:40 Advanced Electric Orbit-Raising Optimization and Analysis with LOTOS 2 - Sven Schaeff (Astos Solutions GmbH)

12:00 Many-Revolution Low-Thrust Orbit Transfer Computation using Equinoctial Q-Law Including J2 and Eclipse Effects - Gabor Varga (ESOC, HSO-GFA)
10:20 - 12:20
Room: 2.04 Titanium
Contributions

10:20 Asteroid proximity GNC assessment through High-fidelity Asteroid Deflection Evaluation Software (HADES) - Massimo Vetrisano (DEIMOS SPACE SLU)

10:40 Dynamical analysis of rendezvous and docking with very large space infrastructures in non-Keplerian orbits - Andrea Colagrossi (Politecnico di Milano)

11:00 Chattering-free Sliding Mode Control for Propellantless Rendez-vous using Differential Drag - Hancheol Cho (Université de Liège)

11:20 GNC design and validation for rendezvous, detumbling, and de-orbiting of ENVISAT using clamping mechanism - José Vasconcelos (Deimos Engenharia)

11:40 ATHENA: Astrodynamics Toolbox for High-fidelity Error-propagation and Navigation - Francesco Torre (University of Strathclyde)

12:00 GNCDE as DD&VV environment for ADR missions GNC - luigi strippoli (gmv)
10:20 - 12:20
Room: 2.03 Vanadium
Contributions

10:20 Dynamic Test Facilities as Ultimate Ground Validation Step for Space Robotics and GNC Systems - Emanuele di Sotto (GMV) Juan Antonio Bejar-Romero (GMV Aerospace and Defence S.A.U.)

10:40 Design and parameter identification by laboratory experiments of a prototype modular robotic arm for orbiting spacecraft applications - Josep Virgili (Naval Postgraduate School)

11:00 Rapid Deployment of Design Environment for EUCLID AOCS design - Francesco Cacciatore (SENER)

11:20 ROSPA, cross validation of the platform-art and ORBIT test facilities for contact dynamic scenario setup and study - Juan Antonio Bejar-Romero (GMV Aerospace and Defence S.A.U.)

11:40 Differential Algebra Space Toolbox for Nonlinear Uncertainty Propagation in Space Dynamics - Pierluigi Di Lizia (Politecnico di Milano)

12:00 Tool for Real-time Pradiction of IXV Trajectory in the Mission Control Center - Martins Sudars (Thales Alenia Space Italia)
12:20

12:20 - 12:40
Room: 2.02 Chromium