Name: 7th International Conference on Astrodynamics Tools and Techniques (ICATT)
Start: 2018-11-06T08:30:00+01:00
End: 2018-11-09T16:00:00+01:00
Location: DLR Oberpfaffenhofen, Germany

7th International Conference on Astrodynamics Tools and Techniques (ICATT)

from Tuesday 6 November 2018 (08:30) to Friday 9 November 2018 (16:00)

Monday 5 November 2018
Tuesday 6 November 2018
11:00 Developing flight dynamics software at ESOC
Developing flight dynamics software at ESOC
11:00 - 12:00
Room: 103 and 105 combined
Contributions

11:00 Developing flight dynamics software at ESOC - Ruaraidh Mackenzie (ESOC)
12:00 PTScientists: Mission to the Moon and the return to Apollo 17
PTScientists: Mission to the Moon and the return to Apollo 17
12:00 - 13:00
Room: 103 and 105 combined
Contributions

12:00 PTScientists: Mission to the Moon and the return to Apollo 17 - Helge Eichhorn (PTScientists GmbH)
13:00 Break for lunch
Break for lunch
13:00 - 14:00
14:00 Trajectory and multi-disciplinary design optimisation
Trajectory and multi-disciplinary design optimisation
14:00 - 16:00
Room: 103 and 105 combined
Contributions

14:00 Trajectory and multi-disciplinary design optimisation - Andreas Wiegand (Astos Solutions GmbH)
Wednesday 7 November 2018
09:00 Opening the 7th ICATT - Guillermo Ortega (ESA) Johann Bals (DLR)
Opening the 7th ICATT
- Guillermo Ortega (ESA)
- Johann Bals (DLR)
09:00 - 10:00
Room: 103 and 105 combined Opening speech of the 7th ICATT conference by Dr. J. Bals from DLR
10:00 Human Enabled Robotic Architecture Capability for Lunar Exploration and Science - Markus Landgraf (ESTEC)
Human Enabled Robotic Architecture Capability for Lunar Exploration and Science
- Markus Landgraf (ESTEC)
10:00 - 11:00
Room: 103 and 105 combined Key note speech by ESA about the exploration of the Moon
11:30
11:30 - 13:00
Room: 103 and 105 combined
Contributions

11:30 Multidisciplinary Modeling and Simulation Framework for Reusable Launch Vehicle System Dynamics and Control - Lale Evrim Briese (DLR, German Aerospace Center)

12:00 Stochastic Constellation Replenishment Planner - Federico Letterio (Deimos Space S.L.U.)

12:30 ASTOS 9.3 - Multibody Feature for Simulations of Flexible Launcher Dynamics - Sven Weikert (Astos Solutions GmbH)
13:00 Lunch break
Lunch break
13:00 - 14:00
14:00
14:00 - 15:30
Room: 103 and 105 combined
Contributions

14:00 POINCARE: A MULTI-BODY, MULTI-SYSTEM TRAJECTORY DESIGN TOOL - Mar Vaquero (NASA Jet Propulsion Laboratory)

14:30 Correlation techniques to build-up and maintain space objects catalogues - Alejandro Pastor-Rodríguez (GMV)

15:00 Are we really covering up the whole sky? - CHRISPHIN KARTHICK (LOYOLA COLLEGE, CHENNAI)
14:00 - 15:30
Room: Single 107
Contributions

14:00 Free CNES Flight Dynamics Tools - Jean François GOESTER (CNES)

14:30 OPEN SOURCE ORBIT DETERMINATION WITH SEMI-ANALYTICAL THEORY - Luc Maisonobe (CS SI)

15:00 Astrodynamics.jl: A Julia-based Open Source Framework for Orbital Mechanics - Helge Eichhorn (PTScientists GmbH)
15:30 Break
Break
15:30 - 16:30
16:30
16:30 - 18:00
Room: 103 and 105 combined
Contributions

16:30 Basilisk: A Flexible, Scalable and Modular Astrodynamics Simulation Framework - Patrick Kenneally (University of Colorado, Boulder)

17:00 Semi-analytical Framework for Precise Relative Motion in Low Earth Orbits - gabriella gaias

17:30 DESEO - Design Engineering Suite for Earth Observation - Gonzalo Vicario de Miguel (DEIMOS SPACE)
16:30 - 18:00
Room: Single 107
Contributions

16:30 TUDAT: the open-source astrodynamics toolbox of Delft University of Technology - Kevin Cowan (Delft University of Technology)

17:00 Visual Orbit design using the open-source VOD tool - Robin Biesbroek (ESA)

17:30 JSatOrb: ISAE-Supaero’s open-source software tool for teaching classical orbital calculations - Thibault Gateau (ISAE-SUPAERO)
18:00 Visit to DLR facilities
Visit to DLR facilities
18:00 - 19:00
Thursday 8 November 2018
09:00
09:00 - 10:30
Room: 103 and 105 combined
Contributions

09:00 Interplanetary trajectory design and mission analysis using gravity assists - Ahmed Magdy Abdelaziz (National Research Institute of Astronomy and Geophysics (NRIAG))

09:30 Efficient design of low lunar orbits based on Kaula recursions - Martin Lara (GRUCACI - University of La Rioja)

10:00 A technique for designing Earth-Mars low-thrust transfers culminating in ballistic capture - Gonçalo Aguiar (Delft University of Technology)
09:00 - 10:30
Room: Single 107
Contributions

09:00 RICADOS - Rendezvous, Inspection, CApturing and Detumbling by Orbital Servicing - Heike Benninghoff (German Aerospace Center (DLR))

09:30 Safe natural far Rendezvous approaches for Cislunar Near Rectilinear Halo Orbits in the Ephemeris model - Emmanuel Blazquez (ISAE-Supaéro)

10:00 ROSSONERO: a tool for preliminary rendezvous mission design in the restricted three-body problem - Giordana Bucchioni (University of Pisa, Department of Information Engineering)
10:30 Break
Break
10:30 - 11:30
11:30
11:30 - 13:00
Room: 103 and 105 combined
Contributions

11:30 Optimized transfers between Earth-Moon invariant manifolds - Laurent Beauregard (ISAE-SUPAERO)

12:00 On the Design of Transfers to Solar-Sail Displaced Orbits in the Earth-Moon System - Jeannette Heiligers (Delft University of Technology)

12:30 Astrodynamics techniques for missions towards Earth trailing or leading heliocentric orbits - Eric JOFFRE (Airbus Defence and Space Ltd)
11:30 - 13:00
Room: Single 107
Contributions

11:30 Analysis of a Rendezvous Mission in Non-Keplerian Orbit using Electric Propulsion - Rubén Vega Astorga David Morante Manuel Sanjurjo-Rivo Manuel Soler

12:00 Commercial Collision Avoidance Service based on JSpOC SP Catalogue - Diego Escobar Anton (GMV)
13:00 Break for lunch
Break for lunch
13:00 - 14:00
14:00
14:00 - 15:30
Room: 103 and 105 combined
Contributions

14:00 Semianalytical Design of Libration Point Formations - Sergey Trofimov (Keldysh Institute of Applied Mathematics)

14:30 Trajectory Design in High-Fidelity Models - Francesco Topputo (Politecnico di Milano)

15:00 Near Rectilinear Orbits around the Moon as Operational Orbit for the Future Deep Space Gateway - Carlos Sanchez (Cranfield University)
14:00 - 15:30
Room: Single 107
Contributions

14:00 Tiangon-1 re-entry follow-up by CNES - Aurélie Bellucci (CNES)

14:30 Cataloguing performance assessment method of SST sensor networks - Diego Escobar Anton (GMV)

15:00 ReDSHIFT software tool for the design and computation of mission end-of-life disposal - Federico Letterio (Deimos Space S.L.U.)
15:30 Break
Break
15:30 - 16:30
16:30
16:30 - 17:30
Room: 103 and 105 combined
Contributions

16:30 DRAMA 3.0.0: A one stop shop for the verification of space debris mitigation requirements - Stijn Lemmens (European Space Agency)

17:00 Rate and collision probability of tethers and sails against debris or spacecraft - Ricardo García-Pelayo (Universidad Politécnica de Madrid)
16:30 - 17:30
Room: Single 107
Contributions

16:30 Mission Design for a Retropropulsive Mars Pinpoint Landing - Tiago Hormigo (Spin.Works S.A.)
19:30

19:30 - 23:30
Friday 9 November 2018
09:30
09:30 - 10:30
Room: 103 and 105 combined
Contributions

09:30 SOLAR-SAIL TRANSFERS FROM INVARIANT OBJECTS TO L5 PERIODIC ORBITS - Alvaro Fernandez Mora (TU Delft Aerospace Engineering)

10:00 Trajectory Optimization of a Low-Thrust Geostationary Orbit Insertion Maneuver for Spacecraft Total Ionizing Dose Reduction - Alexander Starchenko (Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute)
09:30 - 10:30
Room: Single 107
Contributions

09:30 Comparison of different optimization methods to construct an acquisition plan finding the best compromise between calculation time and algorithm performance - Cécile RENAUDIE (CNES)

10:00 Adaptive Pareto Front Sampling Based on Parametric Sensitivity Analysis in a Bi-Objective Setting - Arne Berger
10:30
10:30 - 12:00
Room: 103 and 105 combined
Contributions

10:30 LOTNAV: A low-thrust Interplanetary Navigation Tool - Simone Centuori (DEIMOS Space)

11:00 ELECTRO: a SW tool for the ELECtric propulsion TRajectory Optimization - Juan C. Bastante (OHB System AG)

11:30 OPTELEC - Constrained Low-Thrust Transfer Optimisation Tool applied in Operational Context - Slim Locoche (Airbus Defence and Space)
10:30 - 12:00
Room: Single 107
Contributions

10:30 AO-Car: Transfer of Space Technology to Autonomous Driving with the use of WORHP - Laura Sommer (University of Bremen, WG Optimization and Optimal Control)

11:00 Revisiting Design Aspects of a QP Solver for WORHP - Marcel Jacobse

11:30 MODHOC - Multi Objective Direct Hybrid Optimal Control - Lorenzo Angelo Ricciardi (University of Strathclyde)
12:00 Break for lunch
Break for lunch
12:00 - 13:00
13:00
13:00 - 15:00
Room: 103 and 105 combined
Contributions

13:00 Efficient design of low lunar orbits based on Kaula recursions - Martin Lara (GRUCACI - University of La Rioja)

13:30 MOLTO-OR: A Multi-Objective Low-Thrust Optimization Tool for Orbit Raising - DAVID MORANTE (Universidad Carlos III ( Madrid ))

14:00 MOLTO-IT: A Multi-Objective Low-Thrust Optimization Tool for Interplanetary Trajectories - DAVID MORANTE (Universidad Carlos III ( Madrid ))

14:30 MARS SAMPLE RETURN: MISSION ANALYSIS FOR AN ESA EARTH RETURN ORBITER - Eric Joffre (Airbus Defence and Space)
13:00 - 14:30
Room: Single 107
Contributions

13:00 A fast an efficient algorithm for the computation of distant retrograde orbits - Martin Lara (GRUCACI - University of La Rioja)

13:30 First tests of the C/C++ version of the Draper Semi-analytical Satellite Theory (DSST) - Juan Félix San-Juan (Scientific Computing Group (GRUCACI), University of La Rioja)

14:00 Operational Orbit Determination for the Eumetsat GEO fleet based on optical observations. - Raúl Domínguez (Deimos Space)
15:00 Closing speech and farewell - Guillermo Ortega (ESA)
Closing speech and farewell
- Guillermo Ortega (ESA)
15:00 - 15:30
Room: 103 and 105 combined

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