2014-6-5 Final Programme

http://www.congrexprojects.com/2014-events/14a01/scientific-content/final-programme#Current_Missions 1/14

Monday2 June 2014

Tuesday3 June 2014

Wednesday4 June 2014

Thursday5 June 2014

Friday6 June 2014

09:00

-

10:40

Opening AddressSession 3a:

Miniaturization &

new technology

trends

Session 3b:

Autonomy &

FDIR

Session 5a:

Advances

in Sensors

& Actuators

1

Session 5b:

Advances in

Control &

Estimation 1

Session 7a:

Autonomous

Navigation 1

Session 7b:

Student

Session

Session 9a:

Future

Missions

Session 9b:

Space

TransportationSession 1:

Current Missions

10:40 Coffee Break

11:10

-

12:25

Session 1:

Current Missions

Session

3a:Miniaturization

& new technology

trends

Session

3b:Autonomy

& FDIR

Session 5a:

Advances

in Sensors

& Actuators

1

Session 5b:

Advances in

Control &

Estimation 1

Session 7a:

Autonomous

Navigation 1

Session 7b:

Student

Session

Session 9a:

Future

Missions

Session 9b:

Space

Transportation

Closing Address (12:00)

12:25 Lunch Break

14:00

-

15:40

Session

2a:

Current

Missions

II

Session

2b:

High

Accuracy

Pointing

Session 4a:

In-Orbit

Experiences

Session 4b:

Debris

mitigation &

removal

Session 6a:

Advances

in Sensors

& Actuators

2

Session 6b:

Advances in

Control &

Estimation 2

Session 8a:

Autonomous

Navigation 2

Session 8b:

Exploration

Missions

15:40 Coffee Break

16:10

-

17:50

Session

2a:Current

Missions

II

Session

2b: High

Accuracy

Pointing

Session 4a:

In-Orbit

Experiences

Session 4b:

Debris

mitigation &

removal

Session 6a:

Advances

in Sensors

& Actuators

2

Session 6b:

Advances in

Control &

Estimation 2

Session 8a:

Autonomous

Navigation 2

Session 8b:

Exploration

Missions

17:50 End of Sessions

Evening

events

Conference Dinner at

Graham's Port Wine

Lodge & Vinum

Restaurant

GNC 2014 Exhibition & Poster

Session Opening

Open Bar & Buffet

Click here for Posters

Douro River Cruise and

Dinner Show at

"Herança Magna"

Oceanside Dinner

at Ar d'Mar

Final Programme

Click on the session title in the overview to be redirected to the specific session.

There are no papers included in this version. An updated version will be provided online at the GNC Proceedings

website, availab le via the red button at the far right of the navigation above.

Monday, 2 June 2014

Session 1: Current Missions

Chair: Girouart, B., ESA

Co-Chair: Nugteren, P., ESA

09:00 Opening Address

Benoit, A., ESA

09:25 Eurostar E3000: ADCS Evolutions Towards Future Missions

Fosse, X.1; Bourdon, J.1; Lainé, I.1; Guyot, P.1, Kowaltschek, S.2

1Airbus Defence and Space, France; 2ESA-ESTEC, The Netherlands

09:50 Meteosat Third Generation AOCS Overview Battilana, M.; Ascani, L.; Bindel, D.; Jacquemard, M.; Rigot, G.; Lübke-Ossenbeck, B.OHB System AG, Germany

9th International ESA Conference on Guidance, Navigation & Control Systems / 2 - 6 June 2014 / Oporto, Portugal

The preliminary programme is available below, and will be replaced by a final programme closer to the date.

SCIENTIFIC CONTENTHOME REGISTRATION EXHIBITION SOCIALS DESTINATION LINKEDIN

2014-6-5 Final Programme

http://www.congrexprojects.com/2014-events/14a01/scientific-content/final-programme#Current_Missions 2/14

10:15 The EUCLID AOCS Science Mode Design

Bacchetta, A.1; Saponara, M.1; Torasso, A.1; Saavedra Criado, G.2; Girouart, B.3

1Thales Alenia Space Italy, Italy; 2ESA/ESTEC, Spain; 3ESA/ESTEC, France

10:40 Coffee Break

Session 1: Current Missions

Chair: Girouart, B., ESA

Co-Chair: Nugteren, P., ESA

11:10 Evolution of the AOCS Design for EDRS and the satellites of the Small GEO Family

Chasset, C.; Bodin, P.1; Larsson, R.; Edfors, A. 1OHB Sweden, Sweden; 2OHB System, Germany; 3Airbus Defence and Space, Germany; 4ESTEC,Netherlands

11:35 Design of the NEMO-AM Attitude and Orbit Control System Ibrahim, N. S.; Grocott, S. C. O.; Zee, R. E.Space Flight Laboratory, Canada

12:00 The Sentinel-2 Satellite Attitude Control System - Challenges and Solutions Wiedermann, G.; Gockel, W.; Winkler, S.; Reggio, D.Airbus Defence and Space, Germany

Back to Overview

12:25 Lunch Break

Session 2a: Current Missions II

Chair: Casasco, M., ESA

Co-Chair: Bodin,P., OHB

Sessions 2b: High Accuracy Pointing

Chair: Sechi, G., ESA

Co-chair: Fichter, W., Univerity of Stuttgart

14:00 EXOMARS 2016, Orbiter Modulebus a GNC Development Update

Renault, H.1; Sergent, N.1; Chevallier, M.2;

Bacchetta, A.3; Temperanza, D.4

1Thales Alenia Space - France,

France;2Thales Alenia Space - Italy,

France; 3Thales Alenia Space - Italy,

Italy; 4ESA/ESTEC, Netherlands

Guidance, Navigation, and Control Performance for theGOES-R Spacecraft

Chapel, J1; Clapp, B1; Stancliffe, D1; Bevacqua, T1; Rood,

T2; Freesland, D3; Krimchansky, A4

1Lockheed Martin Space Systems, United States; 2ASI,

Inc., United States; 3ACS Engineering, United

States;4NASA/Goddard Space Flight Center, UnitedStates

14:25 Histogram Filter for AttitudeDetermination of Small Asteroid Lander Schlotterer, M.German Aerospace Center, DLR, Germany

Pointing budgeting using the ESA Pointing ErrorEngineering Handbook and Tool: benefits andlimitations

Ott, T.1; Wiedermann, G.1; Crombez, V.2; Damilano, P.2

1Airbus Defence and Space, Germany; 2Airbus Defenceand Space, France

14:50 The Bepicolombo Attitude And OrbitControl System

Szerdahelyi, L.1; Fugger, S.1; Espeillac, P.1;

Monroig, G.2; Pareaud, Th. 2; Casasco, M.3

1Airbus Defence and Space,

Germany;2Airbus Defence and Space,

France;3ESA/ESTEC, Netherlands

SPICA Micro-vibration Control System Design forPrecision Pointing Stability

Mitani, S1; Kawakatsu, Y2; Sakai, S2; Murakami, N1;

Yamawaki, T1; Mizutani, T1; Komatsu, K2; Nakagawa,

T2

1Aerospace Research and Development Directorate,

JAXA, Japan; 2Institute of Space and AstronauticalScience, JAXA, Japan

15:15 Proba-3: Achieving Formation FlyingMillimetre Accuracy

Tarabini Castellani, L.1; Fernández, J.M.1;

Llorente, J.S.1; Agenjo, A.1; Mestreau-

Garreau, A.2; Cropp, A.2; Santovincenzo, A.2

1SENER Ingeniería y Sistemas, S.A.,

Spain; 2ESA/ESTEC, Netherlands

Reaction-Wheels Based AOCS for high PointingAccuracy and Stability Cirillo, F.; Winkler, S.; Wiedermann, G.; Wilhelm, R.; Ott,T.Airbus Defence and Space - Satellites, Germany

Back to Overview

15:40 Coffee Break

Session 2a: Current Missions II Sessions 2b: High Accuracy Pointing

2014-6-5 Final Programme

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Chair: Casasco, M., ESA

Co-Chair: Bodin, P., OHB

Chair: Sechi, G., ESA

Co-chair: Fichter, W., Univerity of Stuttgart

16:10 Rosetta Hybrid Mode Design Guignard, A.; Val Serra, S.Airbus Defence and Space, France

Meteosat Third Generation Fine Pointing ModeDesignPirson, L; Rouat, O; Deslaef, N; Guichon, D;Roche, YThales Alenia Space, France

16:35 Spacecraft Hybrid (Mixed Actuator)Attitude Control Experiences onNASA Science Missions Dennehy, C.NASA, United States

Robust Active Control for MicrovibrationMitigation in High Stability Satellite Missions

Falcoz, A.1; Boquet, F.1; Secondi, F.1; Bennani,

S.2

1Airbus Defence and Space, France; 2ESA,Netherlands

17:00 Travelling to and Landing on Mars Carryingthe Exomars 2018 Rover

Buonocore, M.1; Oddenino, D.1;

Temperanza, D.2

1Thales Alenia Space Italia,

Italy; 2ESA/ESTEC, Netherlands

Design and Analysis of High Accuracy LOSStabilization for GEO High-Resolution ImagingMissions with Onboard Optical Correlator

Chernykh, V.1; Grzelak , S.1; Janschek, K.1;

Harnisch, B.2

1Technische Universität Dresden,

Germany;2European Space Agency ESTEC,Netherlands

17:25 LPF Journey to L1: Target Approaching Pereira, V.; Povoleri, A.Airbus Defence and Space, United Kingdom

Comprehensive Investigation of Micro-VibrationsImpact due to Different Disturbance Sources onSpacecraft Pointing Stability and InstrumentPerformances for the BepiColombo Mission

Vitelli, M.1; Specht, B.1; Boquet, F.2

1Airbus Defence and Space, Germany; 2Airbus Defenceand Space, France

Back to Overview

17:50 End of Sessions

Evening Activity: Welcome Event at Graham's Port Wine Lodge & Vinum Restaurant

Tuesday, 3 June 2014

GNC Exhibition Day: The exhibition will run the full day of 3 June 2014, for one day only.

There will be a dedicated Exhibition and Poster Session at the end of the day.

Session 3a: Miniaturization & newtechnology trends

Chair: Airey, S., ESA

Co-chair: Brady, T., Draper Labs

Session 3b: Autonomy & FDIR

Chair: Gherardi, D., ESA

Co-chair: Busseuil, J. TAS

09:00 Miniaturized High PerformanceMEMS Accelerometer Detector

Gonseth, S.1; Eichenberger, C2;

Durrant, D3; Airey, P4

1Colibrys (Switzerland) Ltd,

Switzerland;2HMT microelectronic Ag,

Switzerland;3System Engineering &Assessment Ltd, United

Kingdom; 4European Space Agency,Netherlands

Fault-tolerant Spacecraft Attitude Control Choukroun, D.; Sadon, A.Ben-Gurion University, ISRAEL

09:25 Single Axis MEMS-based Accelerometerfor Space Applications Petropoulos, A.; Fikos, G; Metaxas, G;Grammatikakis, V.; Zervakis, E.European Sensor Systems, Greece

Fault Tolerant Control Design for TerminalRendezvous around Mars

Le Peuvédic, C.1; Charbonnel, C.1; Henry, D.2;

Strippoli, L.3; Ankersen, F.4

1Thales Alenia Space - France, France;2Bordeaux

1 University – IMS-LAPS, France;3GMV Aerospace

and Defence, Spain;4ESA/ESTEC, Netherlands

2014-6-5 Final Programme

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09:50 Single Axis Miniaturised MEMS IMUComponent Demonstrator

Durrant, R1; Morris, S2; Ashby, W3; Redant,

S4; Kowaltschek, S5

1SEA, United Kingdom; 2Garfield-Matrics,

United Kingdom; 3Optocap, United

Kingdom; 4IMEC, Belgium; 5ESA,Netherlands

Sensors Failure Detection and Control Reconfigurationfor Entry Phase of USV3 mission Poderico, Mariana; Morani, G.; Sollazzo, A.; Corraro, F.CIRA, Italian Aerospace Research Centre, Italy

10:15 Faint Star - An Intelligent Single-ChipSensor Head for STRs - DevelopmentUpdate

Ogiers, W.1; Gvozdenovic, A.1; Wolfs, B.1; Li,

Z.1; Van Wichelen, K.1; Kowaltschek, S.2

1CMOSIS, Belgium; 2ESTEC, Netherlands

FDIR and Robustness for the Solar OrbiterAOCS

Noteborn, R.1; Stenqvist Hanbury, L.1; Larsson,

R.1; Veldman, S.1; Myatt, J.2; Pigg, M.2; Yu, M.3;

Prezzavento, A.3; Touaty, J.3; Rouquet, J.4;

Girouart, B.4

1OHB Sweden, Sweden; 2Tessella Ltd., United

Kingdom; 3Airbus Defence and Space, United

Kingdom; 4ESA, Netherlands

Back to Overview

10:40 Coffee Break

Session 3a: Miniaturization & newtechnology trends

Chair: Airey, S., ESA

Co-chair: Brady, T., Draper Labs

Session 3b: Autonomy & FDIR

Chair: Gherardi, D., ESA

Co-chair: Busseuil, J. TAS

11:10 Image Processing chip for RelativeNavigation for Lunar Landing

Dunstan, M.1; Hornbostel, K.2

1University of Dundee, United

Kingdom;2Airbus Defence and Space,Germany

Detailed FDI Analysis of AOCS Mode

Brethé, D.1; Dellandrea, B.1; Guiotto, A.2; Jansson, R.3

1Thales Alenia Space - France, France; 2Thales Alenia

Space - Italy, Italy; 3ESA/ESTEC, Netherlands

11:35 A Miniaturised Attitude Control andDetermination System for the QB50 andSME-SAT Missions

Visagie, L1; Forshaw, J L1; Frame, T1; Steyn,

WH2; Lappas, V J1

1University of Surrey, United

Kingdom;2University of Stellenbosch, SouthAfrica

A Study on New GN&C and Propulsion SystemArchitecture by Resilience Engineering Approach Ueda, S.; Nomoto, H.; Kasai, T.Japan Aerospace Exploration Agency (JAXA), Japan

12:00 From space to Earth and back, sunsensorson a detour

Leijtens, J.1; Uittenhout, J.1; Vandersteen,

J.2; Nowak, L.2

1Lens R&D, The Netherlands; 2ESA-ESTEC,The Netherlands

System Health Management Design for a LowEarth Orbit Bus and Mission Indra, S; Masic, I; Ehrhardt, P; Wang, XSpaceTech GmbH, Germany

Back to Overview

12:25 Lunch Break

Session 4a: In-Orbit Experiences

Chair: Van Hattem, F., ESA

Co-chair: Dussy, S., ESA-HQ

Session 4b: Debris Mitigation & Removal

Chair: Erb, S., ESA

Co-chair: Dennehy, C., NASA-GSFC

14:00 In-Flight Demonstration on PROBA-V ofAutonomous Forbidden AttitudeAvoidance

de Lafontaine, J.1; St-Amour, A.1; Naudet,

J.2; Paijmans, B.2; Santandrea, S.3

1NGC Aerospace Ltd., Canada; 2QinetiQ

Space nv, Belgium; 3ESA/ESTEC,Netherlands

Active Debris Removal GNC Challenges over Designand Required Ground Validation Colmenarejo, P.; Avilés, M.; Mollinedo, L.GMV, Spain

14:25 Flight Performance of the IRISAttitude Control System

van Bezooijen, R.1; Knagenhjelm, V.2;

Dougherty, R.2; Boyle, P.2; Pound, D.2

Advanced Navigation Systems for In-OrbitDemonstration of ADR Proximity Operations

Chabot, T.1; Kanani, K.1; Falcoz, A.1; Kervendal, E.1;

Cropp, A.2

1Airbus Defence and Space, France; 2ESA, Netherlands

2014-6-5 Final Programme

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1Lockheed Martin Advanced Technology

Center, United States; 2LockheedMartin Space Systems Company,United States

14:50 ALTS Localization System of VEGALauncher: VV02 Post-Flight Analysis andGPS Issues for Future Hybrid Navigation Roux, C.; Melara, M.

ELV Spa, Italy

TRADE-OFF Orbital Debris Atmospheric Reentry:Design for Demise vs Controlled Reentry Heinrich, S.; Tromba, A.; Leglise, F; Tholot, M.; Nold, O. Altran, France

15:15 Gaia AOCS Flight Results

Colegrove, T.1; Povoleri, A.1; Chapman, P.1;

Ecale, E.2; Girouart, B.3

1Airbus Defence and Space, United

Kingdom;2Airbus Defence and Space ,

France;3European Space Agency,Netherlands

Advances in Experimental Verification of RemoteSpacecraft Attitude Control by Coulomb Charging Stevenson, D.; Schaub, H.University Of Colorado, United States

Back to Overview

15:40 Coffee Break

Session 4a: In-Orbit Experiences

Chair: Van Hattem, F., ESA

Co-chair: Dussy, S., ESA-HQ

Session 4b: Debris Mitigation & Removal

Chair: Erb, S., ESA

Co-chair: Dennehy, C., NASA-GSFC

16:10 GNSS at High Alitudes - Results fromthe SGR-GEO on GIOVE-A

Unwin, M.1; Blunt, P.1; de Vos van

Steenwijk , R.1; Hashida, Y.1;

Kowaltschek, S.2

1SSTL, United Kingdom; 2ESA,Netherlands

Numerical Assessment of the Tumbling Motionof Non-Cooperative Debris Fritsche, B.Hyperschall Technologie Göttingen, Germany

16:35 Agile Satellites In-Orbit AOCSPerformances: From Pleiades toSpot 6, First Application of Airbus DSVersatile LEO Avionics Product

Thieuw, A. Airbus Defence and Space, France

GNC Challenges for Heavy Debris Removalwith Flexible Link BRUN, P. Airbus Defence and Space, France

17:00 In-Flight Experience of the Mars ScienceLaboratory Guidance, Navigation, andControl System for Entry, Descent, andLanding

San Martin, M.

Jet Propulsion Laboratory, CaliforniaInstitute of Technology, United States

MUST: Multi-body Dynamics Simulation Tool tosupport the GNC design for Active DebrisRemoval with flexible elementsBenvenuto, R.; Lavagna, M.Politecnico di Milano, Italy

17:25 ALPHASAT, the First In-OrbitExperience of the New EuropeanLarge Platform

Alvarado, M.1; Massier, S.1; Bettarini,

R.2

1THALES ALENIA SPACE,

France;2SELEX ES, Italy

PRISMA IRIDES: Performance at the end of the DriftPhase and Planned Rendezvous Experiments Bodin, P.; Karlsson, T.; Larsson, R.; Jakobsson, B.;Larsson, B.OHB Sweden, Sweden

Back to Overview

17:50 End of Sessions

Evening Activity: GNC 2014 Exhibition & Poster Session Opening / Open Bar & Buffet

Wednesday, 4 June 2014

Session 5a: Advances in Sensors &Actuators 1

Chair: Palomba, M., ESA

Co-chair: Guay, P., CNES

Session 5b: Advances in Control & Estimation 1

Chair: Bennani, S., ESA

Co-chair: Blas, J., DLR

2014-6-5 Final Programme

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09:00 New Reaction Wheel Assembly Serieswith High Reliability and Low Disturbance

Izawa, K.1; Kanzawa, T.1; Yamanaka, K.1;

Matsumoto, M.2; Taniguchi, N.2

1Japan Aerospace Exploration Agency,

Japan; 2Mitsubishi Precision co. Ltd, Japan

Frequency Shaping of Estimation Error in Hinf-Based Sensor Data FusionWink ler, S.; Dohnal, A.Airbus Defence and Space, Germany

09:25 Low Noise Pointing Mechanisms

Malric-Smith, F.1; Gossant, A.1; Blais, T.1;

Mondier, J.B.2

1Airbus Defence and Space, France; 2CNES,France

Codesign Mechanics/Attitude Control for aSimplified AOCS Preliminary Synthesis

Cumer, Ch.1; Alazard, D.2; Grynagier, A.3; Pittet-

Mechin, Ch.4

1ONERA, France; 2Université de Toulouse,

DMIA,ISAE, France; 3Thales Alenia Space,

France; 4CNES, France

09:50 SPACESTAR Product: a Novel star Trackers’Configuration was Born Boldrini, F.; Procopio, D.; Berrighi, G.SELEX ES, Italy

50 Glitch-Free Data Fusion Algorithm for CombiningMultiple Attitude Solutions Yeh, Ming-Yu; Jan, Ying-Wen; Liu, Chen-Tsung; Wu,AndyNational Space Organization, Taiwan

10:15 Hydra Aps Star Tracker - a Family ofProducts for all Mission Needs

Gelin, B1; Oddos-Marcel, L1; Piot, D1;

Martinez, PE2; Kowaltschek, S3

1SODERN, France; 2CNES,

France;3ESA, Netherlands

Passivity Control for Robotics Satellite DockingSimulators Krenn, R.; Zebenay, M.; Boge, T.DLR German Aerospace Center, Germany

Back to Overview

10:40 Coffee Break

Session 5a: Advances in Sensors &Actuators 1

Chair: Palomba, M., ESA

Co-chair: Guay, P., CNES

Session 5b: Advances in Control & Estimation 1

Chair: Bennani, S., ESA

Co-chair: Bals, J., DLR

11:10 ASTRIX™1000 Ready for Flight

Cros, G.1; Bonnefois, J.J.1; Kowaltschek, S.2;

Delavoipiere, G.3

1Airbus Defence and Space, France; 2ESA,

Netherlands; 3CNES, France

In Flight Results of Adaptive Attitude Controllaw for a Microsatellite

Pittet, C.1; Luzi, A. R.2; Peaucelle, D.3; BiannicC,

J-M.2; Mignot, J.1

1CNES, France; 2ONERA, France; 3LAAS-CNRS,France

11:35 IRES-C: the Best Candidate Sensor for theEarth Pointed Safe Mode on LEO Satellites Boldrini, F.; Brogi, S.; Monnini, E.SELEX ES, Italy

Deterministic L-infinity Actuator Commanding forHigher Agility, Larger Offloading Cycle and LessPropellant Consumption Without Changing Hardware Winkler, S.; Schindler, T.Airbus Defence and Space, Germany

12:00 3D Camera Technology Trade-offand Breadboard Demonstration forSpace Applications

Christy, J.1; Bohn, P.2; Schumann-

Olsen, H.3; Biggio, A.4; Kowaltschek,

S.5

1Thales Alenia Space - France,

France;2TERMA, DENMARK; 3SINTEF,

Norway;4Thales Alenia Space - Italy,

Italy;5ESA/ESTEC, Netherlands

Post-Mission Analysis of Flight Results from theSHEFEX-2 Hybrid Navigation SystemExperiment Theil, S.; Steffes, S,; Samaan, M.DLR Institute of Space Systems, Germany

Back to Overview

12:25 Lunch Break

Session 6a: Advances in Sensors &Actuators 2

Chair: Dauphin, H., ESA

Co-chair: Andrau, B., Airbus Defence andSpace

Session 6b: Advances in Control & Estimation 2

Chair: Bennani, S., ESA

Co-chair: Choukroun, D., TU Delft

14:00 Disturbances in Reaction Wheels: Robust Rendezvous Planning using Model Predictive

2014-6-5 Final Programme

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from Measurement to Modelling

Le, M. P.1; van der Heide, E.2; van Put,

P.2; Seiler, R.3; Ellenbroek, M. H. M4;

Cottaar, E. J. E.5

1Moog Bradford/Eindhoven University of

Technology, Netherlands; 2MOOG

Bradford, Netherlands; 3ESA/ESTEC,

Netherlands; 4University of Twente,Netherlands; Eindhoven University ofTechnology, Netherlands

Control: Some Results Issued from Research andTechnological Studies

Berges, J.-C.1; Arzelier, D.2; Louembet, Ch.2; Cristaldi, A.2

1CNES, France; 2Laas/Cnrs, France

14:25 ACS Actuator Based on MagneticallyLevitated Spherical Rotor

Wawrzaszek, R.1; Rossini, Leopoldo2;

Onillon, Emmanuel2; Seweryn, Karol1; Sidz,

Michal1; Boletis, Alexis3; Mingard, Stefan3;

Beuselinck, Tom4; Van Bavinchove,

Christophe4; Cazorla, Carolina5; Serin,

Jerome6

1Space Research Centre of PAS,

POLAND;2Swiss Center for Electronic andMicrotechnology CSEM,

Switzerland; 3Maxon Motor AG,

Switzerland; 4Redshift, Belgium;5SENERIngeneria

y Sistemas S.A., Spain; 6Societe AnonymeBelge de Constructions AeronautiquesSABCA, Belgium

Robust Controller Design and Testing of an ActiveIsolation for a Payload-Launcher System Strauch, H.; Jetzschmann, C.; Albus, J.Airbus Defence and Space , Germany

14:50 HAS3: A New Generation CMOS ImageSensor for AOCS Star Tracking Deruytere, P.; Innocent, M.; Van Aken, D.ON Semiconductor Belgium, Belgium

Long-Distance, Low-Earth-Orbit, Drag-FreeIntegrated Orbit and Formation Control for theNext Generation Gravity Mission

Canuto, E.1; Colangelo, L.1; Buonocore, M.2;

Massotti, L.3; Girouart, B.3

1Politecnico di Torino, Italy; 2Thales Alenia Space

Italia, Italy; 3ESA/ESTEC, Netherlands

15:15 GYROMETER REGYS20 – LessonLearnt

Flory, R1; Le Noir, Y2

1Thales Alenia Space, France; 2SagemDefense securite, France

Synthesis of Structured Controllers for Performanceand Numerical Implementation Mastering

Falcoz, A.1; Kervendal, E.1; Pittet, C.2

1Airbus Defence and Space, France; 2CNES, France

Back to Overview

15:40 Coffee Break

Session 6a: Advances in Sensors &Actuators 2

Chair: Dauphin, H., ESA

Co-chair: Andrau, B., Airbus Defence andSpace

Session 6b: Advances in Control & Estimation 2

Chair: Bennani, S., ESA

Co-chair: Choukroun, D., TU Delft

16:10 Multi-headed Star Tracker 348K – NextStop is Space. Final in-Earth validationresults Knyazev, V.; Karelin, A.; Zybin, Yu.;Videtskikh, Yu.; Hebhard, A.JSC "SPE "Geofizika-Cosmos", RussianFederation

Robust Precision Pointing Control Design forSpacecraft with Disturbance Transients

Ott, T.1; Wink ler, S.2; Cirillo, F.2; Fichter, W.1

1iFR, University of Stuttgart, Germany; 2AirbusDefence and Space, Germany

16:35 Advances in Quartz CoriolisVibrating Gyroscope for spaceapplications Guerard, J.; Levy, R.; Janiaud, D.; LeTraon, O.ONERA, France

Beyond Kalman Filtering - Evaluation of FilterTechniques for Autonomous RelativeNavigation Benninghoff, H.; Boge, T.German Aerospace Center (DLR), Germany

17:00 Autonomous Star Sensor ASTROAPS – Flight Experience onAlphasat Schmidt, U.; Fiksel, T.; Kwiatkowsk i,A.; Steinbach, I.; Michel, K.Jena-Optronik GmbH, Germany

Applying the Dynamic Inversion Concept on the AgileSpacecraft with Control Moment Gyros Kornienko, A.; Rieber, J.Airbus Defence and Space, Germany

17:25 Breadboard Model of a 3D LIDARSensor for Real-Time PoseEstimation of Spacecraft

Optimisation based Worst Case Analysis ofiGNC of Rendezvous and Capture in MarsSample Return Mission

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http://www.congrexprojects.com/2014-events/14a01/scientific-content/final-programme#Current_Missions 8/14

Rems, F.1; Fritz, S.2; Boge, T.1

1German Aerospace Center (DLR),

Germany; 2Technical University ofMunich (TUM), Germany

Mujumdar, A.1; Gomez, N.2; Menon, P.P.1;

Strippoli, L.2; Ankersen, F.3

1University of Exeter, United Kingdom; 2GMV,

Spain; 3ESA/ESTEC, Netherlands

Back to Overview

17:50 End of Sessions

Evening Activity: Drinks aboard a Rabelo & Dinner Show at "Herança Magna"

Thursday, 5 June 2014

Session 7a: Autonomous Navigation 1

Chair: Dubois Matras, O., ESA

Co-chair: Rebuffat, D., ESA

Session 7b: Student Session

Chair: Benoit, A., ESA

Co-Chair: Lizy Destrez, S., ISAE/Supaero

09:00 StarTiger Dropter Project:Integrated, Closed-Loop Vision-Aided Navigation with HazardDetection and Avoidance

Hormigo, T.1; Gu, C.2; Lutz, T.3;

Gardeck i, S.4; Cordes, F.5; De Maagt,

P.6; Boeljes, A.3

1Spin.Works Lda., Portugal; 2Airbus

Defence and Space, France; 3Airbus

Defence and Space, Germany; 4PoznanUniversity of Technology,

POLAND;5DFKI, Germany; 6ESA,Netherlands

Spacecraft Parameter Identification using S-estimators

Milhano, T.1; Sequeira, J.1; Di Sotto, E.2

1Instituto Superior Técnico, Portugal; 2GMV,Portugal

09:25 PERIGEO: Image ProcessingTechniques Development andTesting for Multimodal Absolute andRelative Navigation Montano, J.Elecnor Deimos, Spain

Model Description and Simulated MissionPerformance of the Next Generation GravityMission E2E Simulator

Colangelo, L.1; Massotti, L.2; Canuto, E.1

1Politecnico di Torino, Italy; 2ESA/ESTEC,Netherlands

09:50 On-Ground Testing OpticalNavigation Systems for ExplorationMissions Krüger, H; Theil, S; Sagliano, M; Maas,BDLR German Space Operation Center,Institute of Space Systems, Germany

Linear Covariance Propagation for Atmospheric re-Entry

Fabacher, E1; Gautron, D2; Profizi, A2

1ISAE, France; 2Airbus Defence and Space, France

10:15 A Neural Network Based HazardDetection Algorithm for PlanetaryLanding Lunghi, P.; Lavagna, M.Politecnico di Milano, Italy

Development, Parameterization andVerification of a Generic Gyro Model Korus, N.University of Bremen, Germany

Back to Overview

10:40 Coffee Break

Session 7a: Autonomous Navigation 1

Chair: Dubois Matras, O., ESA

Co-chair: Rebuffat, D., ESA

Session 7b: Student Session

Chair: Benoit, A., ESA

Co-Chair: Lizy Destrez, S., ISAE/Supaero

11:10 Robust Extraction of Navigation Data fromImages for Planetary Approach andLanding

Jonniaux, G.1; Gherardi, D.2

1Airbus Defence and Space, France; 2ESA,Netherlands

Self-Tuning, Recursive Structure From Motionfor Hazard Detection in Autonomous PlanetaryDescent

Feetham, L1; Aouf, N1; Bourdarias, C2; Voirin, T3;

Dubois-Matra, O3

1Cranfield University, United Kingdom; 2Airbus

Defence and Space, France; 3ESA-ESTEC, Netherlands

11:35 Passive versus Active Hazard Detection &Avoidance Systems

Neveu, D1; Simard Bilodeau, V1; Hamel, J-

Cooperative Control of Multiple Small Satellites usingthe Comprehensive Open-architecture Space MissionOperations System

2014-6-5 Final Programme

http://www.congrexprojects.com/2014-events/14a01/scientific-content/final-programme#Current_Missions 9/14

F1; Woicke, S2; Alger, M1; Mercier, G1;

Beaudette, D1

1NGC Aerospace Ltd., Canada; 2DelftUniversity of Technology, Canada

Nunes, M.1; Sorensen, T.2; Pilger, E.2

1University of Hawaii, United States; 2Hawaii SpaceFlight Laboratory, United States

12:00 Autonomous Lunar Landing Based on Bio-inspired Visual Motion sensors tested in-flight

Sabiron, G.1; Burlion, L.1; Kervendal, E.2;

Bornschlegl, E.3; Raharijaona, T.4; Ruffier,

F.4

1ONERA - DCSD, France; 2Airbus Defence

and Space, France; 3ESA TEC-ECN,

Netherlands;4Institute of Movement Science(CNRS - Aix-Marseille University), France

Modeling and Robust Control of a Space Robotto Remove Massive Debris

Dubanchet, V.1; Saussié, D.1; Alazard, D.2;

Bérard, C.2; Le Peuvédic, C.3

1Ecole Polytechnique de Montréal, Canada;2InstitutSupérieur de l'Aéronautique et de l'Espace (ISAE),

France; 3Thalès Alenia Space, France

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12:25 Lunch Break

Session 8a: Autonomous Navigation 2

Chair: Jansson, R., ESA

Co-chair: Theil, S., DLR

Session 8b: Exploration Missions

Chair: Gherardi, D., ESA

Co-chair: San Martin, M., NASA-JPL

14:00 Navigation Architecture for USV3 Re-Entry, TAEM and Landing Nebula, FrancescoCIRA - Italian Aerospace Research Centre,Italy

Autonomous GNC system for Marco Polo-R AsteroidSample Return Mission

Gil, J.1; di Domenico, M.1; Prieto, T.1; Dominguez, C.1;

Suatoni, M.1; Mollinedo, L.1; Rowell, N.2; Huertas, I.3;

Gherardi, D.4; Agnolon, D.4; Salehi, S.4

1GMV, Spain; 2University Dundee, United

Kingdom;3ESA-ESTEC (SERCO), Netherlands; 4ESA-ESTEC,Netherlands

14:25 Target Relative Navigation PerformanceResults from SINPLEX: a MiniaturizedNavigation System

Steffes, S.1; Theil, S.1; Dumke, M.1; Heise,

D.1; Sagliano, M.1; Samaan, M.1;

Oosterling, H.2; Boslooper, E.2; Schulte, J.3;

Söderholm, S.3; Skaborn, D.3; Yanson, Y.4;

Esposito, M.4; Conticello, S.4; Visee, R.5;

Monna, B.5; Stelwagen, F.5

1DLR, Germany; 2TNO, Netherlands; 3AAC,

Sweden; 4Cosine, Netherlands; 5SystematIC,Netherlands

Vision-Based Absolute Navigation for PreciseLanding: The Full Scale StratosphericExperiment Jonniaux, G.; Despré, N.Airbus Defence and Space, France

14:50 Interest, Design and Implementation ofthe Infrared and LIDAR Experimentswithin ATV5

Vourc'h, S.1; Cavrois, B.1; Donnard, A.1;

Mongrard, O.3; Casiez, P.1; Ankersen, F.3;

Windmüller, M.4;

Kolb, F.4; Pezant, C.5; Bretecher, P.Y.5

1Airbus Defence and Space, France; 3ESA,

Netherlands; 4JenaOptronik,

Germany;5SODERN, France

Demonstrating Autonomous Planetary Landing withGENIE Paschall, S.; Brady, T.Draper Laboratory, United States

15:15 Japanese Next Generation SpaceborneGPS Receiver for LEO Satellites

Yamamoto, T.1; Matsumoto, S.1;

Yamanaka, K.1; Kawakami, S.2; Eda, T.2;

Kasahara, M.2; Takeda, Y.2; Kumagai, S.2;

Ishige, Y.2

1JAXA, JAPAN; 2NEC TOSHIBA SpaceSystems. Ltd., JAPAN

The Verification Approach Of The ExoMars EDM GNC

Martella, P.1; De Sanctis, S.1; Grana', D.2; Amelio, A.3;

Temperanza, D.4; Martinez Barrio, A.4

1ThalesAlenia Space Italy, Italy; 2WinTime at Thales

Alenia Space, Italy, Italy; 3Altran Italia, Italy;4ESA/ESTEC,Netherlands

Back to Overview

15:40 Coffee Break

Session 8a: Autonomous Navigation 2

Chair: Jansson, R., ESA

Session 8b: Exploration Missions

Chair: Gherardi, D., ESA

2014-6-5 Final Programme

http://www.congrexprojects.com/2014-events/14a01/scientific-content/final-programme#Current_Missions 10/14

Co-chair: Theil, S., DLR Co-chair: San Martin, M., NASA-JPL

16:10 Preparing an Autonomous, Low-Cost GNSSPositioning and Timing Function on-Boarda GEO Telecom Mission: a Study Case

Zin, A.1; Mangolini, E.1; Cappelluti, I.1;

Fiordiponti, R.1; Flament, P.2; Kowaltschek,

S.3

1Thales Alenia Space Italia S.p.A,

Italy;2Thales Alenia Space France,

France;3European Space Agency (ESA),Netherlands

Development of a Descent & Landing GNC SubsystemDemonstrator for the Verification of Visual NavigationSolutions for Lunar Landing Applications Hornbostel, K.; Estable, S.; Nuber, C.; Gornig, S.Airbus Defence and Space, Germany

16:35 Integrated Autonomous System forNavigation and Actual Thrust Evaluation byPayload in GEO Insertion with ElectricPropulsion System Assistance

Krasilshchikov, M.1; Kozorez, D.1; Kruzhkov,

D.1; Sypalo, K.2

1Moscow Aviation Institute, Russian

Federation; 2TSAGI, Russian Federation

Data Fusion Strategies for Hazard Detectionand Safe Site Selection for Planetary andSmall Body Landings

Câmara, F.1; Oliveira, J.1; Hormigo, T.1; Araújo,

J.1; Ribeiro, R.2; Falcão, A.2; Gomes, M.2; Dubois-

Matra, O.3; Vijendran, S.3

1Spin.Works Lda, Portugal; 2UNINOVA - Institutode Desenvolvimento de Novas

Tecnologias, Portugal; 3ESA/ESTEC, Netherlands

17:00 The Autonomous Vision ApproachNavigation and Target Identification(AVANTI) Experiment: Objectivesand Design

Gaias, G.1; Ardaens, J.-S.1; D'Amico,

S.2

1DLR/GSOC, Germany; 2StanfordUniversity, United States

StarTiger Dropter Project: Development andFlight Experiment of a Skycrane-LikeTerrestrial Lander Demonstrator

Lutz, T.1; Gardeck i, S.2; Cordes, F.3; Hormigo,

T.4; Gu, C.5; De Maagt, P.6; Boeljes, A.1

1Airbus Defence and Space, Germany; 2Poznan

University of Technology, Poland; 3DFKI,

Germany; 4Spin.Works, Portugal; 5Airbus Defence

and Space, France; 6ESA, Netherlands

17:25 Autonomous Orbit

Determination and StationKeeping in GEO

Boquet, F.Airbus Defence and Space,

FRANCE

Balloon drop tests for aerodynamic stability analysis ofre-entry capsule : possibilities and design guidelines Guerreiro, L.; Branco, J.; Milhano, T.; Di Sotto, E.GMV, Portugal

Back to Overview

17:50 Endof Sessions

Evening Activity: Dinner by the Sea at Ar d'Mar

Friday, 6 June 2014

(There is a possibility the schedule on this day will be moved up to allow for an early ending time)

Session 9a: Future Missions

Chair: Ortega, G., ESA

Co-chair: Berrivin, S., CNES

Session 9b: Space Transportation

Chair: Martinez Barrio, A., ESA

Co-chair: Lefort, X., ESA

09:00 NEOShield Project: GNC Design andPerformance of an Asteroid KineticImpactor Chapuy, M; Vernis, P; Despre, F.;Capolupo, F. Airbus Defence and Space

Launcher Atmospheric Guidance Based On Non-LinearModel Predictive Control

Bourgeois, E.1; Tebbani, S.2; Espinosa Ramos, A.1

1CNES - Launcher Directorate, France; 2SUPELEC, France

09:25 Validation of Differential-DragPropellantless Manoeuvres using 6DoF Simulations and StochasticDynamics Dell'Elce, L.; Kerschen, G.University of Liège, Belgium

IXV GNC&FM Subsystem Phase D Activities: Towards aSuccessful Qualification Review

Contreras, R.1; Rodriguez-Fernandez, G.1; Serrano, D.1;

Kerr, M.2; Fernandez, V.2; De Zaiacomo, G.2; Bejar-

Romero, J.A.3

1SENER Ingenieria y Sistemas S.A., Spain; 2DEIMOS

Space, Spain; 3GMV Aerospace and Defense,

Spain;4Thales Alenia Space Italia Spa, Italy; 5ESA, France

09:50 AOCS and Mission Analysis for the OrbitRaising of the all-Electric PropulsionSatellite Platform Electra

Larsson, R.1; Rathsman, P.1; Edfors, A.1;

ATV Rendezvous Sensors Acceptance Tests atthe EPOSx Facility

Dubois-Matra, O.1; Paris, D.2; Ankersen, F.2

2014-6-5 Final Programme

http://www.congrexprojects.com/2014-events/14a01/scientific-content/final-programme#Current_Missions 11/14

Karlsson, T.1; Cesaro, F2

1OHB Sweden, Sweden; 2OHB System,Germany

1ESA / Telespazio VEGA UK Ltd,

Netherlands;2ESA, Netherlands

10:15 Integrated vision-based GNC forAutonomous Rendezvous and Capturearound Mars

Strippoli, L.1; Colmenarejo, P.1; Novelli, G.1;

Gil Fernandez, J.1; Le Peuvedic, C.2; Lanza,

P.3; Ankersen, F.4

1GMV, Spain; 2TAS France, France; 3TAS

Italy, Italy; 4ESTEC, Netherlands

An Overview of the RFCS V&V Framework:Optimization-Based and Linear Analysis Tools forWorst- Case Search

Marcos, A.1; Rosa, P.2; Roux, C.3; Bartolini, M.3;

Bennani, S.4

1Deimos Space S.L., Spain; 2Deimos Engenharia, Lda.,

Portugal; 3ELV, Italy; 4ESA/ESTEC (TEC- ECN),Netherlands

Back to Overview

10:40 Coffee Break

Session 9a: Future Missions

Chair: Ortega, G., ESA

Co-chair: Berrivin, S., CNES

Session 9b: Space Transportation

Chair: Martinez Barrio, A., ESA

Co-chair: Lefort, X., ESA

11:10 The Results of the Next GenerationGravity Mission AOCS Study

Buonocore, M.1; Bacchetta, A.1;

Cesare, S.1; Parisch, M.1; Torasso,

A.1; Dionisio, S.2; Canuto, E.3;

Girouart, B.4; Massotti, L.4

1Thales Alenia Space Italia,

Italy; 2Ortec-IT, Italy; 3Politecnico di

Torino, Italy;4ESA-ESTEC, Netherlands

Closed Loop Guidance Strategy for Satellite LaunchVehicles Pietrobom, H. C.; Leite Filho, W. C.Aeronautics and Space Institute, Brazil

11:35 Future Interplanetary MissionAutonomous Navigation Challenges Chapuy, M.; Kervendal, E.; Camares, H.;Peacoke, L.; Gherardi, D.; Dubois, O.Airbus Defence and Space, France

Guiding Rocket Science with Passion, Purpose, andTeam Brady, T.; Paschall, S.Draper Laboratory, United States

Back to Overview

12:00 Closing Address

12:25 End of GNC 2014

Poster Session

Current Missions

P01 Integrated Control System (ICS) Test Campaign of Copernicus Sentinel-1A Spacecraft: Test BenchOverview and AOCS Test Results

Anania, M.1; Galvagni, L.1; Sabbioni, F.1; Giulicchi, L.2

1Thales Alenia Space, Italy; 2European Space Agency, Netherlands

P02 Challenges of Solar Orbiter AOCS Development - High Performance, High Flexibility!

Pigg, M.1; van der Drift, A.1; Agg, J.1; Lohner, C.1; Dungate, D.1; Noteborn, R.2; Larsson, R.2;

Prezzavento, A.3; Touaty, J.3; Mafficini, A.3; Rouquet, J.4; Girouart, B.4

1Tessella Ltd., United Kingdom; 2OHB Sweden, Sweden; 3Airbus Defence and Space, United

Kingdom; 4ESA, Netherlands

Back to Overview

High accuracy pointing

P03 Pointing Error Engineering in MTG-GPT – A Practical Hybridization Approach

Bernau, M.1; Mamdy, B.2; van den Braembussche, P.3

1AAirbus Defence and Space, Germany; 2Airbus Defence and Space , France; 3ESTEC, Netherlands

P04 The Pointing Error Engineering Tool (PEET): A Complementary Software to the ESA PointingError Engineering Handbook

2014-6-5 Final Programme

http://www.congrexprojects.com/2014-events/14a01/scientific-content/final-programme#Current_Missions 12/14

Hirth, M.1; Su, H.2; Weikert, S.1; Eggert, J.1; Casasco, M.3

1Astos Solutions GmbH, Germany; 2Institute of Flight Mechanics and Control, University of

Stuttgart, Germany; 3European Space Agency - ESTEC, Netherlands

Back to Overview

Miniaturization and new technology trends

P05 Target Relative Navigation Performance Results from SINPLEX: a Miniaturized NavigationSystem

Steffes, S.1; Theil, S.1; Dumke, M.1; Heise, D.1; Sagliano, M.1; Samaan, M.1; Oosterling, H.2;

Boslooper, E.2; Schulte, J.3; Söderholm, S.3; Skaborn, D.3; Yanson, Y.4; Esposito, M.4; Conticello, S.4;

Visee, R.5; Monna, B.5; Stelwagen, F.5

1DLR, Germany; 2TNO, Netherlands; 3AAC, Sweden; 4Cosine, Netherlands; 5SystematIC, Netherlands

Back to Overview

In-Orbit Experiences

P06 CryoSat-2 In-Orbit AOCS Performance

Barthen, B.1; Duske, N.1; Fornarelli, D.2; Mardle, N.2; Vanschoenbeek, I.1; Parrinello, T.3; Koeble, K.1

1Airbus Defence and Space, Germany; 2European Space Agency, Germany; 3European SpaceAgency, Italy

P07 In-orbit demonstration of a Sun avoidance law

Brethé, D.1; Majal, F.1; Samson, P.1; De la Fontaine, J.2; Raffier, B.3

1Thales Alenia Space - France, France; 2NGC, Canada; 3CNES, France

P08 In-Orbit Results from the Sapphire AOCS System - Space Surveillance using a Low-Cost SmallSatellite

Fingerloos, S1; Holt, T1; Oosthuizen, P1; Leitch, R2

1Surrey Satellite Technology Ltd, United Kingdom; 2MDA Systems Ltd, Canada

Back to Overview

Autonomy and FDIR

P09 A fault tolerant robust AOCS based on 'smart' actuators and sensors Fechtmann, C.Applied Space Technology, Germany

P10 STARTIGER DROPTER PROJECT: Autonomous flight control of a Skycrane-like terrestrial landerdemonstrator

Gu, C1; Gardecki, S2; Cordes, F3; Hormigo, T4; Lutz, T5

1Airbus Defence and Space, France; 2IAII, Poland; 3DFKI, Germany; 4Spin.Works, Portugal; 5AirbusDefence and Space, Germany

Back to Overview

Debris mitigation and removal

P11 Gas Plume Impingement Techniques for Space Debris De-Tumbling Benvenuto, R.; Lavagna, M.Politecnico di Milano, Italy

P12 Propellant sloshing modelling for AOCS design and analysis during satellite de-orbiting 

Hahn, M.1; Cirillo, F.2; Gravemeier, V.1; Wall, W.1

1Technische Universität München, Germany; 2Airbus Defence and Space, Germany

P13 Study of an Optimization T3chnique for a Monte Carlo Collision Risk Assessment of SpaceObjects

Arrufat, T.1; Escobar, D.2; Nejjari, F.1

1UPC, Spain; 2GMV, Spain

P14 Attitude Analysis of a Gossamer Sail De-orbiting Device

Visagie, L1; Lappas, V.J.1; Erb, S.O.2

1University of Surrey, United Kingdom; 2ESA, ESTEC (TEC-ECM), Netherlands

Back to Overview

Advances in Sensors and Actuators

P15 The FGS design for the SVOM Mission

Fan, Xuewu1; Qiu, Yulei2; Wu, Shufan3; Zou, Gangyi1; Chen, Wen3; Yuan, Hao1

1Xi¡¯an Institute of Optics and Precision Mechanics of CAS, China; 2National Astronomical

Observatories of CAS, China; 3Shanghai Engineering Center for Microsatellites of CAS, China

P16 Miniature Control Moment Gyroscope - CMG 4-6S Engineering Model Morand, J.; Crabos, E.; Faucheux, P.Airbus Defence and Space, France

2014-6-5 Final Programme

http://www.congrexprojects.com/2014-events/14a01/scientific-content/final-programme#Current_Missions 13/14

P17 Ground Testing of the GPS Receiver Experiment on SGEO/HAG1

Neumann, N.1; De Bruijn, F.1; Lapanne-Joinville, T.2; Marx, M.2

1OHB-System AG, Germany; 2Airbus Defence and Space, Germany

P18 AOCS Unit Simulation Models

Pattenden, T.1; Pigg, M.1; Dungate, D.1; Bakouche, C.2; Perriault, N.2; Maingam, F.2; Bacchetta, A.3;

Polle, B.4; Theureau, D.4; Girouart, B.5; Carlsson, A.6; Battelino, M.6; Johnsson, M.6; Wallin, R.6;

Prezzavento, A.7; van der Drift, A.1

1Tessella Ltd., United Kingdom; 2Thales Alenia Space, France; 3Thales Alenia Space, Italy; 4Airbus

Defence and Space, France; 5ESA, Netherlands; 6OHB, Sweden; 7Airbus Defence and Space, UnitedKingdom

P19 Altimeter for Planetary Lander

Pinto, C.1; Ortega, G.2; Dubois-Matra, O.2; Mesquita, D.3; Lahtinen, J.4

1EFACEC, Portugal; 2ESA, Netherlands; 3LUSOSPACE, Portugal; 4Harp Technologies, Finland

Back to Overview

Advances in Control and Estimation

P20 An industrial approach for AOCS SW development based on autocoding Devillières, K.; Gendre, D.Airbus Defence and Space, FRANCE

P21 Development of Total Orbital Real-time Attitude control Simulator for Small Satellites

Hoshika, Motoki1; Toraya, Takanori1; Suzaki, Yuta1; Ogawa, Tomoya1; Katayama, Masayuki1;

Mizutamari, Hitoshi1; Aso, Shigeru2; Yasaka, Tetsuo2; Sakurai, Akira2

1Mitsubishi Precision Co.,Ltd, Japan; 2Kyushu University, Japan

Back to Overview

Autonomous Navigation

P22 Realistic Mars environment simulation and impact on the Vision-Based Navigation System forrendez-vous & landing

Chabot, T.1; Vidal, P.1; Jonniaux, G.1; Rebuffat, D.2; Salehi, S.2

1Airbus Defence and Space, France; 2ESA, Netherlands

P23 Vision-based navigation concepts in Mars environment

Cometto, F.1; Lanza, P.1; Christy, J.2; Gil-Fernández, J.3; Hamilton, W.4; Rebuffat, D.5; Salehi, S.6

1Thales Alenia Space ITALIA, ITALY; 2Thales Alenia Space France, France; 3GMV, SPAIN; 4SCISYS,

UNITED KINGDOM; 5ESA/ESTEC, Netherlands; 6Rhea@ESA/ESTEC, Netherlands

P24 Scalable GNC architecture for Moon and Mars landing missions

Oddenino, D.1; Neveu, D.2; Hamel, J. F.2; Carraca Guerreiro, L.3; Mammarella, M.4; Voirin, T.5;

Martinez Barrio, A.5; Simard Bilodeau, V.2; Beaudette, D.2

1Thales Alenia Space Italia, ITALY; 2NGC Aerospace Ltd, CANADA; 3GMV Portugal,

PORTUGAL;4GMV Spain, SPAIN; 5ESA, Netherlands

P25 Validation of Mission Critical Vision-Based Navigation Systems for Planetary Landers, Rovers andIn-Orbit Rendezvous

Parkes, S.1; Dunstan, M.1; Martin, I.1; Rowell, N.1; Gherardi, D.2; Salehi, S.3

1University of Dundee, United Kingdom; 2ESTEC, ESA, Netherlands; 3Rhea System for ESA, ESTEC,Netherlands

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Student Session

P26 Flexible Systems Dynamics for Active Space Debris Removal

Cingoli, A.1; Lavagna, M.1; Benvenuto, R.1; Yabar, C.2; Casasco, M.2

1Politecnico di Milano, Italy; 2ESA-ESTEC, The Netherlands

Back to Overview

Exploration missions

P27 HOMER PROJECT: Development, validation, qualification and flight test results of theautonomous flight control of the test vehicle

Gu, C.1; Vernis, P1; Jourdas, J.F.1; Hachelef, N.1; Heynen, S.1; Poirrier, T.1; Schwientek, A.2; Boudillet,

O1

1Airbus Defence and Space, France; 2Airbus Defence and Space, Germany

P28 HASE: hazard avoidance and detection in low light conditions Kervendal, E.; Kanani, K.; Philippe, C.; Martinez, A.Airbus Defence and Space, France

2014-6-5 Final Programme

http://www.congrexprojects.com/2014-events/14a01/scientific-content/final-programme#Current_Missions 14/14

Future Missions

P29 KaNaRiA - an autonomous asteroid mining mission

Probst, A.1; González Peytavi, G.; Förstner, R.2; Eisfeller, B.

University of the Federal Armed Forces, Munich, Germany; 2University of the Federal Armed ForcesMunich, Germany

Back to Overview

Space Transportation

P30 IXV Worst Case Flying Qualities and Control Testing Haya Ramos, R.; Bonetti, D.; Freixa, J.; Kerr, M.L.; de Zaiacomo, G.; Parigini, C.DEIMOS Space S.L.U., Spain

P31 Guidance Strategies for Orbital Re-Entry of the USV-3 Mission Romagnoli, D.; Morani, G.; Palumbo, R.; Cuciniello, G.; Corraro, F.C.I.R.A. - Italian Aerospace Research Center, Italy

P32 Attitude Control of Launch Vehicle without Roll Control Souza, Carlos H. M.Instituto de Aeronáutica e Espaço, Brazil

Back to Overview