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  • Envision Mission Analysis: from Launch to Low Venus OrbitPablo MUÑOZ, ESA/ESOC, Darmstadt, Germany
    Lorenzo BUCCI, ESA/ESOC, Darmstadt, Germany

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    Pablo MUÑOZ, ESA/ESOC, Darmstadt, Germany
    DESTINY+ Reconfigured Mission Analysis of a Low-Thrust Flyby Cycler Connecting Apophis and PhaethonNaoya OZAKI, JAXA, Kanagawa, Japan
    Hiraiwa NAOKI, JAXA, Kanagawa, Japan
    Christian HOFMANN, JAXA, Kanagawa, Japan
    Takayuki YAMAMOTO, JAXA, Kanagawa, Japan

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    Naoya OZAKI, JAXA, Kanagawa, Japan
    Design of close-proximity orbits about Apophis during  its Earth Close Approach Daniel SCHEERES, University of Colorado Boulder, Boulder, United States
    Hai-Shuo WANG, University of Colorado Boulder, Boulder, United States

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    Daniel SCHEERES, University of Colorado Boulder, Boulder, United States
    Flight Dynamics Operations for the Hera Mission: Preparations for the Binary Asteroid Proximity PhaseFrancesco CASTELLINI, Telespazio Germany GmbH, Darmstadt, Germany
    Bernard GODARD, Telespazio Germany GmbH, Darmstadt, Germany
    Diogene DEI TOS, Terma GmbH, Darmstadt, Germany
    Frank BUDNIK, European Space Agency, Darmstadt, Germany

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    Francesco CASTELLINI, Telespazio Germany GmbH, Darmstadt, Germany
    Constraints on Spacecraft Observations of Apophis through its Earth Close ApproachDaniel J. SCHEERES, UNIVERSITY OF COLORADO BOULDER, Boulder, United States
    Haishuo WANG, UNIVERSITY OF COLORADO BOULDER, Boulder, United States

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    Haishuo WANG, UNIVERSITY OF COLORADO BOULDER, Boulder, United States
    Hera Milani’s Operational Mission Analysis for Didymos binary asteroid characterizationAurélien FELIN, CNES, Toulouse, France
    Julie VERNIERE, CNES, Toulouse, France
    Romain PINEDE, CNES, Toulouse, France
    Jean JAUBERT, CNES, Toulouse, France
    Véronique PIOU, CNES, Toulouse, France
    Sébastien GOULET, CS GROUP, Toulouse, France

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    Aurélien FELIN, CNES, Toulouse, France
    Mission Analysis for RAMSESRuaraidh MACKENZIE, ESA, Darmstadt, Germany
    Ignacio ACEDO ISAC, GMV Gmbh, Darmstadt, Germany
    Davide BASSO, GMV Gmbh, Darmstadt, Germany

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    Ignacio ACEDO ISAC, GMV Gmbh, Darmstadt, Germany
    AEGIS: Italy’s Step Toward the Future of NEA Robotic Exploration – Rendezvous, Landing, and In-Situ AnalysisAlessandro MORSELLI, Nautilus - Navigation in Space Srl, Forlì, Italy
    Luigi COMI, Nautilus - Navigation in Space Srl, Forlì, Italy
    Igor GAI, Nautilus - Navigation in Space Srl, Forlì, Italy
    Alessio QUINCI, Nautilus - Navigation in Space Srl, Forlì, Italy
    Alfredo LOCARINI, Nautilus - Navigation in Space Srl, Forlì, Italy
    Niccolò MICHELOTTI, Politecnico di Milano, Milan, Italy
    Samuele VAGHI, Politecnico di Milano, Milan, Italy
    Fabio FERRARI, Politecnico di Milano, Milan, Italy
    Antonio ABRUSCATO, Tyvak International, Turin, Italy
    Elena VALANT, Tyvak International, Turin, Italy
    Margherita CARDI, Tyvak International, Turin, Italy
    Alessio TAITI, Officina Stellare, Padova, Italy
    Andrea ALBERTI, Officina Stellare, Padova, Italy
    Davide SANTACHIARA, DTM Technologies, Modena, Italy
    Maurizio PAJOLA, INAF - Padova Astronomical Observatory, Padova, Italy
    Alice LUCCHETTI, INAF - Padova Astronomical Observatory, Padova, Italy
    Riccardo LASAGNI MANGHI, Università degli Studi di Bologna, Forlì, Italy
    Giovanni VALENTINI, Agenzia Spaziale Italiana, Rome, Italy
    Alberto BIGAZZI, Agenzia Spaziale Italiana, Rome, Italy
    Marilena AMOROSO, Agenzia Spaziale Italiana, Rome, Italy

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    Alessandro MORSELLI, Nautilus - Navigation in Space Srl, Forlì, Italy
    Feasibility Analysis of GTO Dual-Launch and Indirect Transfer to SEL2 for the Comet Interceptor MissionJuan BAS FERNANDEZ, GMV for ESA-ESOC, Darmstadt, Germany
    Jose Manuel SANCHEZ PEREZ, ESA-ESOC, Darmstadt, Germany
    Ignacio ACEDO ISAC, GMV for ESA-ESOC, Darmstadt, Germany

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    Juan BAS FERNANDEZ, GMV for ESA-ESOC, Darmstadt, Germany
    Statistical Trajectory Optimization Under Uncertainty for Icy MoonExploration with Probability of Impact ConstraintsGabriele NUCCIO,
    Kenshiro OGURI, Purdue University, West Lafayette, IN, United States
    Francesco TOPPUTO, Politecnico di Milano, Milano, Italy

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    Gabriele NUCCIO, Politecnico di Milano, Milano, Italy; Purdue University, West Lafayette, IN, United States
    Harmony and Sentinel-1C/D: an analysis of the convoy safetyJavier SANCHEZ MARTIN, ESA-ESOC, Darmstadt, Germany
    Giuseppe ALBINI, ESA-ESOC, Darmstadt, Germany
    Pedro JURADO, ESA-ESTEC, Noordwijk, Netherlands

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    Javier SANCHEZ MARTIN, ESA-ESOC, Darmstadt, Germany
    Linear Parameter-Varying Control of Spacecraft Relative Motion in Elliptical Orbits via Geometry-Informed ConvexificationTakahiro SASAKI, JAXA, Tsukuba, Japan
    Naomi MURAKAMI, JAXA, Tsukuba, Japan
    Nicola BARESI, University of Surrey, Guildford, United Kingdom
    Finn ANKERSEN, ESA, Noordwijk, Netherlands

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    Takahiro SASAKI, JAXA, Tsukuba, Japan
    Preparation of a first ever in-orbit demonstration of differential lift in INTA's ANSER cluster Constantin TRAUB, Institute of Space Systems (IRS), University of Stuttgart, Stuttgart, Germany
    Fabrizio TURCO, Institute of Space Systems (IRS), University of Stuttgart, Stuttgart, Germany
    Marcos FUENTES-CARILLO, Space Programmes Department. Instituto Nacional de Técnica Aeroespacial (INTA), Torrejón de Ardoz, Spain
    Iván CASTRO-FERNÁNDEZ, Space Programmes Department. Instituto Nacional de Técnica Aeroespacial (INTA), Torrejón de Ardoz, Spain
    César ARZA-GONZÁLEZ, Space Programmes Department. Instituto Nacional de Técnica Aeroespacial (INTA), Torrejón de Ardoz, Spain
    Stefanos FASOULAS, Institute of Space Systems (IRS), University of Stuttgart, Stuttgart, Germany
    Carlos CAMPUZANO-CORRALES, Space Programmes Department. Instituto Nacional de Técnica Aeroespacial (INTA), Torrejón de Ardoz, Spain
    Santiago RODRÍGUEZ-BUSTABAD, Space Programmes Department. Instituto Nacional de Técnica Aeroespacial (INTA), Torrejón de Ardoz, Spain

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    Fabrizio TURCO, Institute of Space Systems (IRS), University of Stuttgart, Stuttgart, Germany
    Physics-Informed Neural Networks for Multi-Impulse Trajectory Generation in Spacecraft Formation ReconfigurationHao GONG, School of Aeronautics and Astronautics, Sun Yat-sen University, Shenzhen, China
    Chenglong XU, School of Aeronautics and Astronautics, Sun Yat-sen University, Shenzhen, China
    Jihe WANG, School of Aeronautics and Astronautics, Sun Yat-sen University, Shenzhen, China

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    Hao GONG, School of Aeronautics and Astronautics, Sun Yat-sen University, Shenzhen, China
    Parameter Space Exploration for Analysis of Motion Synchronization with a Tumbling Space ObjectMatthew HUTTON, European Space Agency (via IMS Space Consultancy GmbH), Darmstadt, Germany
    Arnaud BOUTONNET, European Space Agency, Darmstadt, Germany

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    Matthew HUTTON, European Space Agency (via IMS Space Consultancy GmbH), Darmstadt, Germany
    Distributed Relative Navigation in Spacecraft Swarms via joint RF Ranging and CommunicationFrancesco DE CECIO, Politecnico di Milano, Milan, Italy
    Michèle LAVAGNA, Politecnico di Milano, Milan, Italy
    Enrico BELLONI, Politecnico di Milano, Milan, Italy

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    Enrico BELLONI, Politecnico di Milano, Milan, Italy
    Feasibility analysis of the low-thrust trajectory for the Moon-enabled Sun occultation missionAlesia HERASIMENKA, Surrey Space Centre, University of Surrey, Guildford, United Kingdom
    Nicola BARESI, Surrey Space Centre, University of Surrey, Guildford, United Kingdom
    Lucie GREEN, Mullard Space Science Laboratory, University College London, Dorking, United Kingdom
    Huw MORGAN, Department of Physics, Aberystwyth University, Aberystwyth, United Kingdom

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    Alesia HERASIMENKA, Surrey Space Centre, University of Surrey, Guildford, United Kingdom
    Robust Orbit Insertion Strategies for Low-Energy Lunar TransferKenta OSHIMA, Suwa University of Science, Chino, Japan
    Chit Hong YAM, ispace, inc., Tokyo, Japan

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    Kenta OSHIMA, Suwa University of Science, Chino, Japan
    Earth-Moon Orbit Design for a Rapid-Response Asteroid Interceptor SystemAlessandro MASSINI,
    Noelle Elisabeth MAY, Purdue University, West Lafayette, United States
    Moacir FONSECA BECKER, Purdue University, West Lafayette, United States
    Andrea CAPANNOLO, Purdue University, West Lafayette, United States

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    Alessandro MASSINI, Politecnico di Milano, Milano, Italy; Purdue University, West Lafayette, United States
    Trajectory Design for Multi-Moon Orbiters Using Lobe Dynamics of Resonant ManifoldsYusaku ENDOH, Nihon University, Chiba, Japan
    Kenji UCHIYAMA, Nihon University, Chiba, Japan
    Kai MASUDA, Nihon University, Chiba, Japan

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    Yusaku ENDOH, Nihon University, Chiba, Japan
    Resonances, Invariant Manifolds, and Low-Thrust Lunar Transfers: the Case of ESA's SMART-1Bhanu KUMAR, University of Michigan, Ann Arbor, United States

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    Bhanu KUMAR, University of Michigan, Ann Arbor, United States
    Maneuver design methods in the Didymos binary asteroid system for Juventas and Milani operationsRomain PINÈDE, CNES, TOULOUSE, France
    Julie VERNIÈRE, CNES, TOULOUSE, France
    Aurélien FÉLIN, CNES, TOULOUSE, France
    Véronique PIOU, CNES, TOULOUSE, France
    Alain LAMY, CNES, TOULOUSE, France

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    Romain PINÈDE, CNES, TOULOUSE, France
    Safe Autonomous Guidance Under Uncertainty via Sequential Covariance Steering for Small-Body Proximity Operations Luca FRASSINELLA,
    Kenshiro OGURI, Purdue University, West Lafayette, United States
    Francesco TOPPUTO, Politecnico di Milano, Milan, Italy

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    Luca FRASSINELLA, Politecnico di Milano, Milan, Italy; Purdue University, West Lafayette, United States
    OPERATIONAL MANEUVER TARGETING FRAMEWORK FOR THE EMIRATES MISSION TO THE ASTEROID BELTMohamed KULEIB, Technology Innovation Institute (TII), Abu Dhabi, United Arab Emirates
    Jay MCMAHON, Colorado Center for Astrodynamics Research, University of Colorado, Boulder, United States
    Giovanni FEREOLI, Colorado Center for Astrodynamics Research, University of Colorado, Boulder, United States
    Jeremy KNITTEL, Laboratory for Atmospheric and Space Physics (LASP) at University of Colorado,, Boulder, United States

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    Mohamed KULEIB, Technology Innovation Institute (TII), Abu Dhabi, United Arab Emirates
    A practical guide to implementing generic zero-hold interplanetary trajectory legsDario IZZO, European Space Research and Technology Centre, Noordwijk, Netherlands
    Giacomo ACCIARINI, European Space Research and Technology Centre, Noordwijk, Netherlands
    Laurent BEAUREGARD, European Space Operations Centre, Darmstadt, Germany
    Harry HOLT, European Space Research and Technology Centre, Noordwijk, Netherlands
    Yuri SHIMANE, Samueli School of Engineering at UC Irvine, San Diego, United States

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    Dario IZZO, European Space Research and Technology Centre, Noordwijk, Netherlands
    Long-Term Orbit Evolution of Sentinel-1A: Analysis and Interpretation of In-Flight DataLuigi IMPERI, Thales Alenia Space, Roma, Italy
    Simone PROIETTI, Thales Alenia Space, Roma, Italy
    Andrea PRIROVANO, Thales Alenia Space, Roma, Italy
    Sergio Giuseppe BARRASSO, Thales Alenia Space, Roma, Italy
    Annamaria NICITO, Thales Alenia Space, Roma, Italy

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    Simone PROIETTI, Thales Alenia Space, Roma, Italy
    Low-Thrust Orbit Acquisition for the EUMETSAT EPS-Sterna ConstellationDaniel AGUILAR TABOADA, EUMETSAT, Darmstadt, Germany
    Riccardo TORELLI, EUMETSAT, Darmstadt, Germany

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    Riccardo TORELLI, EUMETSAT, Darmstadt, Germany
    Thruster Performance Estimation via Satellite Model and Telemetry Data Fusion: Application to Sentinel-1 ConstellationSimone PROIETTI, Thales Alenia Space, Roma, Italy
    Luigi IMPERI, Thales Alenia Space, Roma, Italy
    Andrea PIROVANO, Thales Alenia Space, Roma, Italy
    Sergio Giuseppe BARRASSO, Thales Alenia Space, Roma, Italy
    Annamaria NICITO, Thales Alenia Space, Roma, Italy

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    Simone PROIETTI, Thales Alenia Space, Roma, Italy
    Operational Experience of Close Formation Flight at 500 km Altitude during Severe Geomagnetic StormsRalph KAHLE, DLR / GSOC, Oberpfaffenhofen, Germany
    Benjamin SCHLEPP, DLR / GSOC, Oberpfaffenhofen, Germany
    Simon GRUBER, DLR / GSOC, Oberpfaffenhofen, Germany
    Lars SPRENGELMEYER, DLR / GSOC, Oberpfaffenhofen, Germany
    Martin WERMUTH, DLR / GSOC, Oberpfaffenhofen, Germany
    Stefan HACKEL, DLR / GSOC, Oberpfaffenhofen, Germany
    Frederic SCHOUTETENS, DLR / GSOC, Oberpfaffenhofen, Germany

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    Ralph KAHLE, DLR / GSOC, Oberpfaffenhofen, Germany
    Biomass Reference Orbit Generation and Orbit Control André VASCONCELOS, CS Group - Germany GmbH, Darmstadt, Germany
    Pere RAMOS BOSCH, European Space Operations Centre (ESOC), Darmstadt, Germany
    Javier SANCHEZ, European Space Operations Centre (ESOC), Darmstadt, Germany
    Luca GUERRA, CS Group - Germany GmbH, Darmstadt, Germany
    Alessio PELELLA, Terma GmbH, Darmstadt, Germany
    Mick HOFFMANN, European Space Operations Centre (ESOC), Darmstadt, Germany
    Daniel RANUSCHIO, GMV GmbH, Darmstadt, Germany

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    André VASCONCELOS, CS Group - Germany GmbH, Darmstadt, Germany
    NorSat-TD re-entry experiment for semi-controlled re-entry of small satellitesØyvind Bryhn PETTERSEN, Space Norway, Oslo, Norway
    Ivar SPYDEVOLD, Space Norway, Oslo, Norway
    May-Iren ESPELUND, Space Norway, Oslo, Norway
    Toby HARRIS, SpaceROC, Thatcham, United Kingdom

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    Øyvind Bryhn PETTERSEN, Space Norway, Oslo, Norway
    Preparations of Comet Interceptor Navigation to an unknow comet Ignacio ACEDO ISAC, GMV for ESA-ESOC, Darmstadt, Germany
    JOSE MANUEL SANCHEZ PEREZ, ESA-ESOC, Darmstadt, Germany
    Juan BAS FERNANDEZ, GMV for ESA-ESOC, Darmstadt, Germany

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    Ignacio ACEDO ISAC, GMV for ESA-ESOC, Darmstadt, Germany
    Rosetta Earth Swing-by Anomaly Revisited: Assessing Physical Contributions through Orbital Dynamics AnalysisTobias HOFFMANN, Flight Dynamics Division, ESA/ESOC, Darmstadt, Germany
    Frank BUDNIK, Flight Dynamics Division, ESA/ESOC, Darmstadt, Germany

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    Tobias HOFFMANN, Flight Dynamics Division, ESA/ESOC, Darmstadt, Germany
    Interplanetary Orbit Determination Augmented by Beacon Navigation: Application to the EMA MissionLars HINÜBER, Faculty of Aerospace Engineering, Delft University of Technology, Delft, Netherlands
    Mattia PUGLIATTI,
    Dominic DIRKX, Faculty of Aerospace Engineering, Delft University of Technology, Delft, Netherlands
    Jay MCMAHON, Colorado Center for Astrodynamics Research, University of Colorado Boulder, Boulder, United States

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    Lars HINÜBER, Faculty of Aerospace Engineering, Delft University of Technology, Delft, Netherlands
    Covariance Analysis of Quasi-Satellite Orbits around Phobos with Applications to the Japanese Martians Moons eXploration mission (MMX)Nicola BARESI, Surrey Space Centre / University of Surrey, Guildford, United Kingdom
    Edoardo CICCARELLI, Surrey Space Centre / University of Surrey, Guildford, United Kingdom
    Tolgahan TANRIKULU, Surrey Space Centre / University of Surrey, Guildford, United Kingdom
    Mattia PUGLIATTI, University of Colorado Boulder, Boulder, United States

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    Nicola BARESI, Surrey Space Centre / University of Surrey, Guildford, United Kingdom
    Validating Probability-of-Collision Computing Methods Through a Classification-Based Analysis of Assumption FailuresDenis ARZELIER, LAAS-CNRS, Toulouse , France
    Sébastien Nicolas François BELIS, GMV, Ramonville, France
    Adrìan DE ANDRÈS, GMV, Ramonville, France
    Emmanuel DELANDE, CNES, Toulouse, France
    Mioara JOLDES, LAAS-CNRS, Toulouse , France
    Marìa-Luz HERNANDÈS, GMV, Ramonville, France
    Riccardo FASANELLA, LAAS-CNRS, Toulouse , France
    Christophe TAILLAN, CNES, Toulouse, France
    Jérôme THOMASSIN, CNES, Toulouse, France

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    Riccardo FASANELLA, LAAS-CNRS, Toulouse , France
    Combining Differential Algebra and Subset Sampling for Efficient Long-Term Collision Risk AssessmentAndrea ZOLLO, DLR - German Space Operation Center, Munich, Germany
    Annarita TROMBETTA, DLR - German Space Operation Center, Munich, Germany
    Crisitna PARIGINI, University of Auckland - Te Pūnaha Ātea - Space Institute, Auckland, New Zealand
    Roberto ARMELLIN , University of Auckland - Te Pūnaha Ātea - Space Institute, Auckland, New Zealand
    Juan Félix SAN JUAN DÍAZ , University of La Rioja - Scientific Computation & Technological Innovation Center, Logrono, Spain
    Ralph KAHLE, DLR - German Space Operation Center, Munich, Germany

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    Andrea ZOLLO, DLR - German Space Operation Center, Munich, Germany
    Assessing Operational Collision Consequence MetricsMiles LIFSON, The Aerospace Corporation, Arlington, United States
    Kai KINDRED, The Aerospace Corporation, Arlington, United States
    Daniel PACHURA, The Aerospace Corporation, Arlington, United States
    Tim MURPHY, The Aerospace Corporation, Arlington, United States
    Dolan HIGHSMITH, The Aerospace Corporation, Arlington, United States
    Matthew HEJDUK, The Aerospace Corporation, Arlington, United States

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    Miles LIFSON, The Aerospace Corporation, Arlington, United States
    Topology-based Launch Collision Avoidance augmented with Differential EvolutionLuca LEONI,
    Giuseppe DI CAMPLI BAYARD DE VOLO, DLR/GSOC, Weßling, Germany
    Ralph KAHLE, DLR/GSOC, Weßling, Germany

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    Luca LEONI, DLR/GSOC, Weßling, Germany; TU Delft, Delft, Netherlands
    Intelligent Space Object Cataloging: A Deep Learning Framework for Orbit Regime Classification and Track Association of Optical ArcsDingcun CHEN, Nanjing University, Nanjing, China
    Jingshi TANG, Nanjing University, Nanjing, China

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    Dingcun CHEN, Nanjing University, Nanjing, China
    Avoidance maneuvers compatible with formation flying Nicolas KAIKATI, CS-Group, Toulouse, France
    Vincent DEBOUT, CS-Group, Toulouse, France
    Vincent CUCCHIETTI, CS-Group, Toulouse, France
    Christophe TAILLAN, CNES, Toulouse, France
    Jérôme THOMASSIN, CNES, Toulouse, France

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    Nicolas KAIKATI, CS-Group, Toulouse, France
    Virtual Thrust–Based Control Formulation for Multiple Kinetic Impactor Asteroid DeflectionMoacir FONSECA BECKER, Purdue University, West Lafayette, United States
    Karel HERNÁNDEZ BANDRICH, Purdue University, West Lafayette, United States
    Alessandro MASSINI, Politecnico di Milano, Milan, Italy
    Noelle MAY, Purdue University, West Lafayette, United States
    Shivani MANOJ PATWARDHAN, Purdue University, West Lafayette, United States
    Andrea CAPANNOLO, Purdue University, West Lafayette, United States

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    Moacir FONSECA BECKER, Purdue University, West Lafayette, United States
    A Graph Search Approach for Automated Scientific Planetary Moon Tour Design with Mission ConstraintsFrancesco PERSENICO, Politecnico di Milano, Milano, Italy
    Fabrizio MACCARI, Politecnico di Milano, Milano, Italy
    Michèle Roberta LAVAGNA, Politecnico di Milano, Milano, Italy

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    Fabrizio MACCARI, Politecnico di Milano, Milano, Italy
    Nonlinear stochastic trajectory optimizationThomas CALEB, ISAE-SUPAERO, Toulouse, France
    Roberto ARMELLIN, Te Punaha Atea - Space Institute University of Auckland, Auckland, New Zealand
    Stéphanie LIZY-DESTREZ, ISAE-SUPAERO, Toulouse, France

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    Thomas CALEB, ISAE-SUPAERO, Toulouse, France
    ISSFD 2026: Cycler and Self-Cycler Orbits using Solar-SailsHarry HOLT, Advanced Concepts Team, ESA, Leiden, Netherlands
    Dario IZZO, Advanced Concepts Team, ESA, Leiden, Netherlands
    Chit Hong YAM, Mission Design and Operations Group, ispace inc., Tokyo, Japan
    Zhong ZHANG, Department of Aerospace Science and Technology, Politecnico di Milano, Milan, Italy

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    Harry HOLT, Advanced Concepts Team, ESA, Leiden, Netherlands
    AstroNav – A System for Performing Autonomous Navigation on Deep Space Missions  Shyam BHASKARAN, Jet Propulsion Laboratory, Pasadena, United States
    Ted DRAIN, Jet Propulsion Laboratory, Pasadena, United States
    Todd ELY, Jet Propulsion Laboratory, Pasadena, United States
    Declan MAGES, Jet Propulsion Laboratory, Pasadena, United States
    Swati MOHAN, Jet Propulsion Laboratory, Pasadena, United States

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    Shyam BHASKARAN, Jet Propulsion Laboratory, Pasadena, United States
    Autonomous navigation in Low Lunar Orbits using a gravity gradiometerSergio COLL-IBARS, University of Colorado, Boulder, Boulder, United States
    Daniel SCHEERES, University of Colorado, Boulder, Boulder, United States
    Penina AXELRAD, University of Colorado, Boulder, Boulder, United States

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    Sergio COLL-IBARS, University of Colorado, Boulder, Boulder, United States
    Augmented inertial navigation solutions for medium accuracy landing  Luis GOMEZ CASAJUS,
    Marco LOMBARDO, Nautilus - Navigation in Space Srl. , Forlì (FC), Italy
    Marco ZANNONI,
    Edoardo SCARPA, Nautilus - Navigation in Space Srl. , Forlì (FC), Italy
    Federico SCALERA, University of Bologna, Department of Industrial Engineering, Forlì (FC), Italy
    Andrea MAGNANINI, University of Bologna, Department of Industrial Engineering, Forlì (FC), Italy
    Alvaro MARTINEZ BARRIO, ESA/ESTEC, Noordwijk, Netherlands
    Ruaraidh MACKENZIE, ESA/ESOC Darmstadt, Darmstadt, Germany

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    Edoardo SCARPA, Nautilus - Navigation in Space Srl. , Forlì (FC), Italy
    Spacecraft Control in Unknown Gravitational Environments through a Data-Driven Tube MPC SchemeAbhishek MALHOTRA, Purdue University, West Lafayette, United States
    Andrea CAPANNOLO, Purdue University, West Lafayette, United States
    Moacir FONSECA BECKER, Purdue University, West Lafayette, United States

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    Moacir FONSECA BECKER, Purdue University, West Lafayette, United States
    Autonomous GNSS-based Relative Navigation for Distributed Earth Observation Missions using Adaptive Extended Kalman FilterAlessandro MICHELAZZI, Politecnico di Milano, Milan, Italy
    Gabriella GAIAS, Politecnico di Milano, Milan, Italy
    Camilla COLOMBO, Politecnico di Milano, Milan, Italy

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    Alessandro MICHELAZZI, Politecnico di Milano, Milan, Italy
    Uncertainty-Aware Visual Perception for Spacecraft Proximity OperationsMassimiliano BUSSOLINO, Politecnico di Milano, Department of Aerospace Science and Technology, Milan, Italy
    Stefano SILVESTRINI, Politecnico di Milano, Department of Aerospace Science and Technology, Milan, Italy
    Michèle LAVAGNA, Politecnico di Milano, Department of Aerospace Science and Technology, Milan, Italy

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    Massimiliano BUSSOLINO, Politecnico di Milano, Department of Aerospace Science and Technology, Milan, Italy
    TESSERAL-COUPLING EFFECTS ON THE LONG-TERM DYNAMICS OF EXTREMELY LOW LUNAR ORBITSMartin LARA, University of La Rioja, Logroño, Spain

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    Martin LARA, University of La Rioja, Logroño, Spain
    Comprehensive High-Fidelity Analysis of Lunar Frozen OrbitsGiovanni ANESE, CISAS "Giuseppe Colombo", Università degli Studi di Padova, Padova, Italy
    Miguel GAVIRA-ALADRO, Technical University of Madrid (UPM), Madrid, Spain
    Claudio BOMBARDELLI, Technical University of Madrid (UPM), Madrid, Spain

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    Giovanni ANESE, CISAS "Giuseppe Colombo", Università degli Studi di Padova, Padova, Italy
    Lunar exterior mean-motion resonancesAnjali RAWAT, Virginia Tech, Blacksburg, United States
    Bhanu KUMAR, University of Michigan, Ann Arbor, United States
    Aaron J. ROSENGREN, University of California San Diego, La Jolla, United States
    Shane D. ROSS, Virginia Tech, Blacksburg, United States

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    Anjali RAWAT, Virginia Tech, Blacksburg, United States
    Local Orbital Elements Around Periodic OrbitsJoan GIMENO, Universitat de Barcelona, Barcelona, Spain
    Luke PETERSON, University of Texas at Austin, Austin, United States

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    Luke PETERSON, University of Texas at Austin, Austin, United States
    Orbit Determination Strategies for Lunar CubeSats: Application to the VMMO MissionAndrea BELLOME, Indra Space, Rome, Italy
    Ismael EL BAKOURI BEN SIAMAR, Indra Space, Madrid, Spain
    Chiara PILEGGI, Indra Space, Lisbon, Portugal
    David MORANTE, Indra Space, Madrid, Spain
    Nicola BARESI, University of Surrey, Guildford, United Kingdom
    John PAPOUDOS, University of Surrey, Guildford, United Kingdom
    Wojciech KALINOWSKI, University of Surrey, Guildford, United Kingdom
    Alesia HERASIMENKA, University of Surrey, Guildford, United Kingdom
    Roman KRUZELECKY, MPB Communications Inc., Pointe-Claire, Canada

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    Andrea BELLOME, Indra Space, Rome, Italy
    Nonlinear Filtering for Spacecraft-to-Spacecraft Absolute and Relative Tracking on NRHO-QPO Formations in Cislunar SpaceRyan MENGES, University of Colorado Boulder, Boulder, United States
    Daniel SCHEERES, University of Colorado Boulder, Boulder, United States

    person_pin
    Ryan MENGES, University of Colorado Boulder, Boulder, United States
    Autonomous Hybrid State Estimation in the Perturbed Two-Body SystemBenjamin HANSON, University of California San Diego, La Jolla, United States
    Thomas BEWLEY, University of California San Diego, La Jolla, United States
    Aaron ROSENGREN, University of California San Diego, La Jolla, United States

    person_pin
    Benjamin HANSON, University of California San Diego, La Jolla, United States
    Analysis of an unexpected force acting on the SWOT satellite in early operations phaseThibaut DUPUY, CNES, TOULOUSE, France

    person_pin
    Thibaut DUPUY, CNES, TOULOUSE, France
    Estimation of satellite parameters using angle-only measurements for precise orbit predictionEliot STEIN, ONERA, Palaiseau, France
    Lamberto DELL'ELCE, INRIA, Sophia Antipolis, France
    Hanae LABRIJI, ONERA, Palaiseau, France
    Florian THUILLET, ONERA, Toulouse, France

    person_pin
    Eliot STEIN, ONERA, Palaiseau, France
    Orbit determination accuracy in LEO using dedicated optical passive systemsMiguel SANTOS, Neuraspace, Coimbra, Portugal
    Alejandro CANO, Neuraspace, Coimbra, Portugal
    Andrea FIORENTINO, Neuraspace, Coimbra, Portugal
    Rob ARTHUR, Neuraspace, Coimbra, Portugal
    Chiara MANFLETTI, Neuraspace, Coimbra, Portugal

    person_pin
    Miguel SANTOS, Neuraspace, Coimbra, Portugal
    Design and Execution of the CRYO2ICE Manoeuvre Campaign for Arctic ObservationsDavide DI SANTIS, European Space Agency - ESOC, Darmstadt, Germany
    Mick HOFFMANN, European Space Agency - ESOC, Darmstadt, Germany
    Luca Giorgio PAOLETTI, European Space Agency - ESOC, Darmstadt, Germany
    Javier SANCHEZ, European Space Agency - ESOC, Darmstadt, Germany

    person_pin
    Davide DI SANTIS, European Space Agency - ESOC, Darmstadt, Germany
    MicroCarb's journey to orbit: lessons learned from the Delayed Launch and Non-Optimal InjectionNoé CHARPIGNY, CNES, Toulouse, France
    Séverine BELLOIR, CNES, Toulouse, France

    person_pin
    Séverine BELLOIR, CNES, Toulouse, France
    BIOMASS Flight Dynamics Operations from Launch to Commissioning: Performance and Lessons LearnedPere RAMOS BOSCH, European Space Agency (ESA), Darmstadt, Germany
    Libe JAUREGUI, European Space Agency (ESA), Darmstadt, Germany
    André VASCONCELOS, CS Group - Germany GmbH, Darmstadt, Germany
    Susanne KASTEN-COORS, European Space Agency (ESA), Darmstadt, Germany

    person_pin
    Pere RAMOS BOSCH, European Space Agency (ESA), Darmstadt, Germany
    Everything You Always Wanted to Know about the Kinéis maneuver CONOPS :  Electrical Orbit Raising, Station-Keeping, Collision avoidance and DeorbitationJules DAVID, Kinéis, Toulouse, France
    Guillaume AZEMA, Thales Service Numériques, Toulouse, France
    Jesus ESTEBAN DONES, Centre National d'Etudes Spatiales, Toulouse, France
    Etienne MONTAGNON, Centre National d'Etudes Spatiales, Toulouse, France

    person_pin
    Jules DAVID, Kinéis, Toulouse, France
    Robust Guidance for Assisted Natural Reentry with On-Board Drag EstimationDamien COURTEVILLE, ISAE-SUPAERO, Toulouse, France
    Joan Pau SÁNCHEZ, ISAE-SUPAERO, Toulouse, France
    Richard EPENOY, Centre National d'Etudes Spatiales (CNES), Toulouse, France
    Bertrand RAFFIER, Centre National d'Etudes Spatiales (CNES), Toulouse, France
    Quentin HARBULOT, Thales Alenia Space, Cannes, France

    person_pin
    Damien COURTEVILLE, ISAE-SUPAERO, Toulouse, France
    Continuous-Thrust Autonomous Guidance for Constraint-Compliant Proximity Observation of Small Bodies via Control Barrier Functions  Richard EPENOY, Centre National d'Etudes Spatiales (CNES), Toulouse, France

    person_pin
    Richard EPENOY, Centre National d'Etudes Spatiales (CNES), Toulouse, France
    Reachability for Low-Thrust Trajectories via Maximum Initial MassGiacomo ACCIARINI, European Space Agency, Noordwijk, Netherlands
    Dario IZZO, European Space Agency, Noordwijk, Netherlands
    Zhong ZHANG, Politecnico di Milano, Milan, Italy

    person_pin
    Giacomo ACCIARINI, European Space Agency, Noordwijk, Netherlands
    A Semi-Analytical Approach for Operational Orbit Control in Low Earth OrbitsAnna FONTAN, CS Group - Germany GmbH, Darmstadt, Germany
    Klaas VANTOURNHOUT, CS Group - Germany GmbH, Darmstadt, Germany

    person_pin
    Anna FONTAN, CS Group - Germany GmbH, Darmstadt, Germany
    Meteosat Third Generation: Evolution of the Orbit Control Strategy of MTG-I1 and MTG-S1 towards the Co-located ConfigurationFilippo BERTABONI, WGS Workgroup Solutions at EUMETSAT, Darmstadt, Germany
    Stefano PESSINA, EUMETSAT, Darmstadt, Germany
    Miguel Angel MARTIN SERRANO, EUMETSAT, Darmstadt, Germany
    Marco DEL MONTE, Starion Group at EUMETSAT, Darmstadt, Germany

    person_pin
    Filippo BERTABONI, WGS Workgroup Solutions at EUMETSAT, Darmstadt, Germany
    Out-of-Plane Maneuver Strategies for Cross-Track Control in the NanoFF Formation-Flying Mission under Operational ConstraintsDebdeep ROYCHOWDHURY, TU Berlin/EnduroSat, Berlin, Germany
    Fynn BOYER, TU Berlin, Berlin, Germany
    Sascha KAPITOLA, TU Berlin, Berlin, Germany
    Grant REGEN, TU Berlin, Berlin, Germany
    Alan LEGENZA, TU Berlin, Berlin, Germany
    Benjamin PALMER, TU Berlin, Berlin, Germany
    José MANUEL DIEZ, TU Berlin, Berlin, Germany
    Enrico STOLL, TU Berlin, Berlin, Germany

    person_pin
    Grant REGEN, TU Berlin, Berlin, Germany
    High resolution surface model and differential drag as a station-keeping methodGuillaume AZEMA, Thales Service Numériques, Toulouse, France
    Anthony COMBE, Kinéis, Toulouse, France
    Jules DAVID, Kinéis, Toulouse, France

    person_pin
    Guillaume AZEMA, Thales Service Numériques, Toulouse, France
    Minimum-time deorbiting strategy of PLEIADES satellite in case of battery failureNoé CHARPIGNY, CNES, Toulouse, France

    person_pin
    Noé CHARPIGNY, CNES, Toulouse, France
    Geometrical method for optimal GEO-inclined station keepingLaurent BEAUREGARD, Telespazio GmbH, Darmstadt, Germany
    Arnaud BOUTONNET, European Space Agency (ESA), Darmstadt, Germany
    Frederic SCHOUTETENS, German Space Operation Centre (GSOC), DLR, Weßling, Germany
    Simon GRUBER, German Space Operation Centre (GSOC), DLR, Weßling, Germany

    person_pin
    Laurent BEAUREGARD, Telespazio GmbH, Darmstadt, Germany
    Collision Risk Assessment and Monitoring for Electric Orbit Raising – SP-Based Methodology and GTO-to-GEO Case StudyFrederic SCHOUTETENS, German Aerospace Center (DLR), Weßling , Germany
    Lars SPRENGELMEYER, German Aerospace Center (DLR), Weßling , Germany
    Ralph KAHLE, German Aerospace Center (DLR), Weßling , Germany

    person_pin
    Frederic SCHOUTETENS, German Aerospace Center (DLR), Weßling , Germany
    Enhancing Robustness to Operational Contingencies in MEO Electric Orbit Raising through RAAN Management StrategyDavid MORANTE, Indra Space, Madrid, Spain
    Dayana VIERA, Indra Space, Madrid, Spain
    Wail BOUMCHITA, Indra Space, Madrid, Spain
    Riccardo DI CORATO, European Space Agency, Noordwijk, Netherlands
    Rubén CASTRO, European Space Agency, Noordwijk, Netherlands
    Lukas STEINDORF, European Space Agency, Noordwijk, Netherlands
    Claudia IANNONE, Thales Alenia Space Italy, Rome, Italy

    person_pin
    David MORANTE, Indra Space, Madrid, Spain
    VLEO satellite preliminary design: a control-driven approachJean-Marc BIANNIC, ONERA, Toulouse, France
    Mario CASSARO, ONERA, Toulouse, France
    Mathieu ROGNANT, ONERA, Toulouse, France
    Sérgio WAITMAN, ONERA, Toulouse, France
    John Wen-Hao LEE, DSO, Singapore, Singapore
    Merrick Tong Le LING, DSO, Singapore, Singapore
    Andrew Geng Tong NG, DSO, Singapore, Singapore
    Chek Wu TAN, DSO, Singapore, Singapore

    person_pin
    Jean-Marc BIANNIC, ONERA, Toulouse, France
    Robust Performance Analysis of the LISA Attitude Control LoopTommaso CASATI, ONERA, Toulouse, France
    Valentin PREDA, ESA/ESTEC, Noordwijk, Netherlands
    Clément ROOS, ONERA, Toulouse, France
    Jean-Marc BIANNIC, ONERA, Toulouse, France
    Hélène EVAIN, CNES, Toulouse, France

    person_pin
    Jean-Marc BIANNIC, ONERA, Toulouse, France
    Spin Plane Dynamics of Fast Spinning TethersJorge SIMÓN AZNAR, Universidad Carlos III de Madrid, Leganés, Spain
    Gonzalo SÁNCHEZ ARRIAGA, Universidad Carlos III de Madrid, Leganés, Spain
    Behrad VATANKHAHGHADIM, Universidad Carlos III de Madrid, Leganés, Spain

    person_pin
    Jorge SIMÓN AZNAR, Universidad Carlos III de Madrid, Leganés, Spain
    GNC Requirement Analysis of an Active Debris Removal Mission enabled by the Ion Beam Shepherded Concept. The ALBATOR project.  Shrouti DUTTA, Northstar Earth and Space, Luxembourg, Luxembourg
    Priyatharsan RAJASEKAR, Northstar Earth and Space, Luxembourg, Luxembourg
    Manuel SANJURJO-RIVO, Northstar Earth and Space, Luxembourg, Luxembourg

    person_pin
    Shrouti DUTTA, Northstar Earth and Space, Luxembourg, Luxembourg
    High-Fidelity AOCS Simulation Framework for LPV Modeling and Control of Flexible SpacecraftAndrea MARRAZZA, DYCSYT, Toulouse, France
    Ervan KASSARIAN, DYCSYT, Toulouse, France
    Francesco SANFEDINO, Fédération ENAC ISAE-SUPAERO ONERA, Toulouse, France
    Daniel ALAZARD, Fédération ENAC ISAE-SUPAERO ONERA, Toulouse, France

    person_pin
    Andrea MARRAZZA, DYCSYT, Toulouse, France
    State Constraint Analysis for Fuel Optimal Powered Descent GuidanceSamuel HORNUS, Inria, Nancy, France
    Jean-Baptiste CAILLAU, Université Côte d'Azur, Nice, France
    Lamberto DELL'ELCE, Inria, Sophia-Antipolis, France
    Jean-Baptiste POMET, Inria, Sophia-Antipolis, France

    person_pin
    Samuel HORNUS, Inria, Nancy, France
    Auto-Slicing as Post-Processing in Automated Trajectory DesignMax BANNACH, European Space Agency, Noordwijk, Netherlands
    Giacomo ACCIARINI, European Space Agency, Noordwijk, Netherlands
    Laurent BEAUREGARD, European Space Agency, Noordwijk, Netherlands
    Dario IZZO, European Space Agency, Noordwijk, Netherlands

    person_pin
    Max BANNACH, European Space Agency, Noordwijk, Netherlands
    Efficient Nonlinear Uncertainty Quantification for Spaceflight Leveraging Nonlinear ExpansionsEthan BURNETT, University of Texas at Austin, Austin, United States
    Spencer BOONE, ISAE SUPAERO, Toulouse, France

    person_pin
    Ethan BURNETT, University of Texas at Austin, Austin, United States
    Robust and Sustainable End-of-Life by Lunar Impact for Cislunar Periodic Orbits.Louis CARTON, University of California San Diego, San Diego, United States
    Aaron J. ROSENGREN, University of California San Diego, San Diego, United States

    person_pin
    Louis CARTON, University of California San Diego, San Diego, United States
    Cislunar end-of-life strategies based on an aware usage of the key dynamical objectsMathilda BOLIS, Politecnico di Milano, Milano, Italy
    Elisa Maria ALESSI, Istituto di Matematica Applicata e Tecnologie Informatiche “Enrico Magenes”, Consiglio Nazionale delle Ricerche, Milano, Italy
    Joan Pau SANCHEZ CUARTIELLES, Institut Supérieur de l’Aéronautique et de l’Espace (ISAE-SUPAERO), Toulouse, France
    Camilla COLOMBO, Politecnico di Milano, Milano, Italy
    Stéphanie LIZI-DESTREZ, Institut Supérieur de l’Aéronautique et de l’Espace (ISAE-SUPAERO), Toulouse, France

    person_pin
    Mathilda BOLIS, Politecnico di Milano, Milano, Italy
    Satellite Behavior Monitoring For Malicious RPOs PredictionAxel GABLIER, LookUp, Toulouse, France
    Tom SEMBLANET, LookUp, Toulouse, France
    Laurence LORDA, LookUp, Toulouse, France

    person_pin
    Tom SEMBLANET, LookUp, Toulouse, France
    VLEO Satellite Aerodynamics: In-Orbit CharacterisationAndrew NG, DSO National Laboratories, Singapore, Singapore
    Merrick LING , DSO National Laboratories, Singapore, Singapore
    John Wen-Hao LEE, DSO National Laboratories, Singapore, Singapore
    Chek Wu TAN , ST Engineering Satellite Systems, Singapore, Singapore

    person_pin
    Andrew NG, DSO National Laboratories, Singapore, Singapore
    P-01 - IDM-ACS : A new module for calculating disturbance torques and pre-dimensioning reaction wheels and magneto-torquer barsJoël MICHAUD, CNES, Toulouse, France
    Frédérick VIAUD, CNES, Toulouse, France
    Marina TORRES, CNES, Toulouse, France
    Jean-Luc LE GAL, CNES, Toulouse, France
    Maxime SENES, CNES, Toulouse, France

    person_pin
    Maxime SENES, CNES, Toulouse, France
    P-02 - Modelling of attitude profile for CO2M making use of GODOTCristina SANTANA CAMPRUBI, EUMETSAT, Darmstadt, Germany
    Jose Maria DE JUANA GAMO, EUMETSAT, Darmstadt, Germany

    person_pin
    Cristina SANTANA CAMPRUBI, EUMETSAT, Darmstadt, Germany
    P-03 - Dynamically Adaptive Dual Quaternion Control for Spacecraft Proximity Operations via Predictive Bio-Inspired OptimizationJinghan LI, School of Astronautics, Beihang University, Beijing, China
    Peng SHI, School of Astronautics, Beihang University, Beijing, China

    person_pin
    Jinghan LI, School of Astronautics, Beihang University, Beijing, China
    P-04 - Photorealistic Camera Images for the Japanese Martian Moons eXploration Project (MMX): Towards PhobosTolgahan TANRIKULU, Surrey Space Centre, University of Surrey, Guildford, United Kingdom
    Mattia PUGLIATTI, University of Colorado Boulder, Boulder, United States
    Edoardo CICCARELLI, Foundational Space Ltd, London, United Kingdom
    Nicola BARESI, Surrey Space Centre, University of Surrey, Guildford, United Kingdom

    person_pin
    Tolgahan TANRIKULU, Surrey Space Centre, University of Surrey, Guildford, United Kingdom
    P-05 - A Scalable, Modular Flight Dynamics System for Heterogeneous Constellations with Electric PropulsionVincent CUCCHIETTI, CS Group, Toulouse, France
    Guillaume JOLLY, CS Group, Toulouse, France
    Maxime JOURNOT, CS Group, Toulouse, France
    Vincent DEBOUT, CS Group, Toulouse, France

    person_pin
    Vincent CUCCHIETTI, CS Group, Toulouse, France
    P-06 - Enhancing MIRS Science Planning for MMX: A User-Centric Approach with MOPS and PROMISEEric SAWYER, CNES, Toulouse, France

    person_pin
    Eric SAWYER, CNES, Toulouse, France
    P-07 - GRACE-Continuity In-Orbit Science Calibration PlanNadège PIE, Center for Space Research - The University of Texas at Austin, Austin, United States
    Furun WANG, Center for Space Research - The University of Texas at Austin, Austin, United States
    Himanshu SAVE, Center for Space Research - The University of Texas at Austin, Austin, United States
    Chris MCCULLOUGH, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, United States
    David WIESE, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, United States

    person_pin
    Nadège PIE, Center for Space Research - The University of Texas at Austin, Austin, United States
    P-08 -  A Geometric Method to Determine a Long-Term Reference-Eccentricity Trajectory for Orbit-Maintenance PlanningRiccardo MAJER, CS Group, Darmstadt, Germany
    Klaas VANTOURNHOUT, CS Group, Darmstadt, Germany

    person_pin
    Riccardo MAJER, CS Group, Darmstadt, Germany
    P-09 - Orbit Analysis System – Operational Innovation of a Flight Dynamics Tool SuiteMatthew BOURASSA, Calian, Saint-Hubert, Canada
    Bryan COOKE, Calian, Saint-Hubert, Canada
    Cole FRANK, Calian, Saskatoon, Canada
    Greg HAMMEL, Calian, Saint-Hubert, Canada
    Michal JAGNODZINSKI, Calian, Saint-Hubert, Canada
    William OLIVER, Calian, Saskatoon, Canada

    person_pin
    Matthew BOURASSA, Calian, Saint-Hubert, Canada
    P-10 - Low-Thrust Fuel-Optimal Formation Reconfiguration Strategy for Distributed Space-Based Telescopes in Halo Orbits with Homotopic ApproachYihan PENG, Beihang University, Beijing, China
    Peng SHI, Beihang University, Beijing, China
    Shuyi WANG, Beijing Institute of Control Engineering, Beijing, China
    Jiliang SONG, Beijing Institute of Control Engineering, Beijing, China

    person_pin
    Yihan PENG, Beihang University, Beijing, China
    P-11 - Six DoF powered descent guidance based on Image DynamicXi MA, Beihang University, 省/自治区/直辖市, China
    Shengping GONG, Beihang University, 省/自治区/直辖市, China
    Lin CHENG, Beihang University, 省/自治区/直辖市, China

    person_pin
    Xi MA, Beihang University, 省/自治区/直辖市, China
    P-12 - Analytical formulation for minimum time low-thrust phasing of MEO satellites in quasi-circular orbit under platform constraints  Claudia IANNONE, Thales Alenia Space Italy, Rome, Italy
    Wail BOUMCHITA, Deimos Space S.L.U, Tres Cantos, Spain
    Dayana VIERA RODRIGUEZ, Deimos Space S.L.U, Tres Cantos, Spain
    David MORANTE, Deimos Space S.L.U, Tres Cantos, Spain
    Lukas STEINDORF, European Space Agency (ESTEC), Noordwijk, Netherlands
    Rubén CASTRO, European Space Agency (ESTEC), Noordwijk, Netherlands
    Riccardo DI CORATO, European Space Agency (ESTEC), Noordwijk, Netherlands
    Andrea ADRIANI, Thales Alenia Space Italy, Rome, Italy
    Andrea CICI, Thales Alenia Space Italy, Rome, Italy

    person_pin
    Claudia IANNONE, Thales Alenia Space Italy, Rome, Italy
    P-13 - Stochastic Model Predictive Control with Sequential Safety-Map Updates for Autonomous Landing on Unknown TerrainsHosuei OU, The University of Tokyo, Tokyo, Japan
    Naoya OZAKI, Japan Aerospace Exploration Agency, Kanagawa, Japan

    person_pin
    Hosuei OU, The University of Tokyo, Tokyo, Japan
    P-14 - Automated Orbit Control for Copernicus Sentinel-2 Tandem Formation Using EOOC: Concept, Implementation, and In-Flight ResultsDirk KUIJPER, CS Group - Germany GmbH, Darmstadt, Germany
    Anna FONTAN, CS Group - Germany GmbH, Darmstadt, Germany

    person_pin
    Anna FONTAN, CS Group - Germany GmbH, Darmstadt, Germany
    P-15 - Robustness of spacecraft orbits to uncertainties in a triple asteroid systemTomohiro ISHIZUKA, ISAE-SUPAERO, Toulouse, France
    Stéphanie LIZY-DESTREZ, ISAE-SUPAERO, Toulouse, France

    person_pin
    Tomohiro ISHIZUKA, ISAE-SUPAERO, Toulouse, France
    P-16 - Primer Vector-Based Optimization of Multi-Impulse Transfers in the Saturn-Enceladus System for South Pole Plume ExplorationMatteo BEER, SacLAB - ISAE-Supaero, TOULOUSE, France
    Spencer BOONE, SacLAB - ISAE-Supaero, TOULOUSE, France
    Stephanie LIZY-DESTREZ, SacLAB - ISAE-Supaero, TOULOUSE, France
    Paul CAVAILLES, SacLAB - ISAE-Supaero, TOULOUSE, France

    person_pin
    Paul CAVAILLES, SacLAB - ISAE-Supaero, TOULOUSE, France
    P-17 - Efficient Computation and Optimization of the Ground Casualty Risk for Semi-Controlled reentry Damien COURTEVILLE, ISAE-SUPAERO, Toulouse, France
    Augustin DESNOS, ISAE-SUPAERO, Toulouse, France
    Joan Pau SÁNCHEZ, ISAE-SUPAERO, Toulouse, France

    person_pin
    Augustin DESNOS, ISAE-SUPAERO, Toulouse, France
    P-18 - Forward--Backward Indirect Shooting for Low-Thrust Trajectories with Interior EventsZhong ZHANG,
    Jia YANG,
    Dario IZZO,
    Francesco TOPPUTO, Politecnico di Milano, Milano, Italy

    person_pin
    Zhong ZHANG, Politecnico di Milano, Milano, Italy;
    P-19 - On-Board Collision Risk Management for End-of-Mission Satellite De-Orbit ManeuversPaul PINTEAU, ISAE-Supaéro, Toulouse, France
    Thibault GATEAU, ISAE-Supaéro, Toulouse, France
    Jasmine RIMANI, AIKO France, Toulouse, France
    Stéphanie LIZY-DESTREZ, ISAE-Supaéro, Toulouse, France
    Jérôme THOMASSIN, CNES, Toulouse, France

    person_pin
    Paul PINTEAU, ISAE-Supaéro, Toulouse, France
    P-20 - Using Lunar Gravity Assists to Boost Earth Escape for the ESA Comet Interceptor MissionGiovanni GUERRIERO, Institut supérieur de l'aéronautique et de l'espace, Toulouse, France
    Joan-Pau SANCHEZ CUARTIELLES, Institut supérieur de l'aéronautique et de l'espace, Toulouse, France

    person_pin
    Giovanni GUERRIERO, Institut supérieur de l'aéronautique et de l'espace, Toulouse, France
    P-21 - Optimising Transfers from Europe’s Spaceport to the Lunar Gateway using Primer Vector Theory.Marion BURNICHON,
    Lorenzo BUCCI, European Space Agency - ESOC, Darmstadt, Germany
    Carmine GIORDANO, Politecnico di Milano, Milan, Italy
    Francesco TOPPUTO, Politecnico di Milano, Milan, Italy

    person_pin
    Marion BURNICHON, Politecnico di Milano, Milan, Italy; European Space Agency - ESOC, Darmstadt, Germany
    P-22 - Formation Control in CR3BP Using Toroidal State Elements from an Atlas of Invariant ToriPaulo RAMIREZ, Purdue University, West Lafayette, United States
    Andrea CAPANNOLO, Purdue University, West Lafayette, United States

    person_pin
    Paulo RAMIREZ, Purdue University, West Lafayette, United States
    P-23 - Co-Orbital Motion for Enhancing Lunar Navigation ServicesLuis CORMIER, University of Nottingham, Nottingham, United Kingdom
    Nishanth PUSHPARAJ, University of Nottingham, Nottingham, United Kingdom
    Paul BLUNT, University of Nottingham, Nottingham, United Kingdom
    Chantal CAPPELLETTI, University of Nottingham, Nottingham, United Kingdom

    person_pin
    Luis CORMIER, University of Nottingham, Nottingham, United Kingdom
    P-24 - Distributed Convex Guidance Generation for Multi-Agent Mapping around Small BodiesEnrico BELLONI, Politecnico di Milano, Milano, Italy
    Michèle LAVAGNA, Politecnico di Milano, Milano, Italy

    person_pin
    Enrico BELLONI, Politecnico di Milano, Milano, Italy
    P-25 - Science-driven Multi-Flyby Resonant Trajectory for Automated Flyby SelectionFlorian BIBOUD, Vinterstellar AB, Stockholm, Sweden
    Emil VINTERHAV, Vinterstellar AB, Stockholm, Sweden

    person_pin
    Florian BIBOUD, Vinterstellar AB, Stockholm, Sweden
    P-26 - Interplanetary Trajectory Design from a Moon-Grazing Retrograde Periodic Orbit around EarthDario BERRETTI, Politecnico di Milano, Milano, Italy
    Kenta OSHIMA, Suwa University of Science, Chino, Japan

    person_pin
    Dario BERRETTI, Politecnico di Milano, Milano, Italy
    P-27 - Time-Regularized Optimization for Low-Thrust Lunar Gravity Assist Escape TrajectoriesXiaowen LIU, Beihang University, Beijing, China
    Shuyue FU, Beihang University, Beijing, China
    Di WU ,
    Shengping GONG,
    Peng SHI,

    person_pin
    Xiaowen LIU, Beihang University, Beijing, China
    P-28 - Ephemeris transition of Earth-Moon resonant orbits leveraging the bicircular restricted four-body problemShuhao CUI, School of Astronautics, Beihang University, Beijing, China
    Yue WANG,

    person_pin
    Shuhao CUI, School of Astronautics, Beihang University, Beijing, China
    P-29 - AI algorithms for on-board collision avoidance decision-makingOscar GLEDEL, CNES, Toulouse, France
    Noé CHARPIGNY, CNES, Toulouse, France
    Jérôme THOMASSIN, CNES, Toulouse, France

    person_pin
    Oscar GLEDEL, CNES, Toulouse, France
    P-30 - A Feasibility Study on Active Debris Removal by Insertion into Natural De-orbiting CorridorsAlexandre MARCHON, ISAE-SUPAERO, Toulouse, France
    Paul PINTEAU, ISAE-SUPAERO, Toulouse, France
    Stéphanie LIZY-DESTREZ, ISAE-SUPAERO, Toulouse, France

    person_pin
    Alexandre MARCHON, ISAE-SUPAERO, Toulouse, France
    P-31 - Pre-launch post-separation screenings for MTG-S1 and MetOp-SG A1 launchesGiacomo NISI, Terma GmbH at EUMETSAT, Darmstadt, Germany
    Stefano PESSINA, EUMETSAT, Darmstadt, Germany
    Jose Maria DE JUANA GAMO, EUMETSAT, Darmstadt, Germany
    Juan Antonio SANZ CRISTOBAL, CLC Space GmbH at EUMETSAT, Darmstadt, Germany
    Filippo BERTABONI, WGS Workgroup Solutions GmbH at EUMETSAT, Darmstadt, Germany

    person_pin
    Giacomo NISI, Terma GmbH at EUMETSAT, Darmstadt, Germany
    P-32 - Assessing the Collision-Avoidance Capability of Solar Sails in Low Earth OrbitVarun GOTTUMUKKALA, Delft University of Technology, Delft, Netherlands
    Steve GEHLY, Delft University of Technology, Delft, Netherlands
    Jeannette HEILIGERS, Delft University of Technology, Delft, Netherlands

    person_pin
    Varun GOTTUMUKKALA, Delft University of Technology, Delft, Netherlands
    P-33 - Debris mitigation compliance assessments associated with interplanetary return trajectoriesValerio LEVI, GMV GmbH, Darmstadt, Germany
    Marc TORRAS RIBELL, GMV GmbH, Darmstadt, Germany
    Lorenzo PORCELLI, GMV GmbH, Darmstadt, Germany
    Harleen KAUR MANN, GMV GmbH, Darmstadt, Germany
    Alejandro PASTOR RODRÍGUEZ, GMV GmbH, Darmstadt, Germany
    Ignacio ACEDO ISAC,
    Patrik KAERRAENG, HTG – Hyperschall Technologie Göttingen GmbH, Bovenden, Germany
    Dennis WEBER, MAITY Space GmbH, Darmstadt, Germany
    Penghuy SREAN, MAITY Space GmbH, Darmstadt, Germany
    Vitali BRAUN, ESA - ESOC, Darmstadt, Germany
    Stijn LEMMENS, ESA - ESOC, Darmstadt, Germany

    person_pin
    Valerio LEVI, GMV GmbH, Darmstadt, Germany
    P-34 - Cataloging objects from INTELSAT 33E fragmentation using optical sensorLucas MALLACH, CS Group, Toulouse, France
    Raphaël FERME, CS Group, Toulouse, France
    Simon BLEICHER, CS Group, Toulouse, France
    Manuel PAVY,

    person_pin
    Simon BLEICHER, CS Group, Toulouse, France
    P-35 - Extending ESA ARES Collision Avoidance Effort Estimation Support to Custom ConstellationsRiccardo CIPOLLONE, Look Up, TOULOUSE, France
    Tom SEMBLANET, Look Up, TOULOUSE, France
    Mathilde HOLLEY, Look Up, TOULOUSE, France
    Laurence LORDA, Look Up, TOULOUSE, France

    person_pin
    Riccardo CIPOLLONE, Look Up, TOULOUSE, France
    P-36 - Advanced Precise Orbit Determination concepts for LEO Mega-ConstellationsJavier BERZOSA MOLINA, GMV Aerospace and Defence, Tres Cantos, Spain
    Luning BAO CHENG, GMV Aerospace and Defence, Tres Cantos, Spain
    Alejandro SEVILLANO GONZÁLEZ, GMV Aerospace and Defence, Tres Cantos, Spain
    Jaime FERNÁNDEZ SÁNCHEZ, GMV Aerospace and Defence, Tres Cantos, Spain
    Francesco GINI, ESA/ESOC, Darmstdat, Germany
    Jean-Christophe BERTON, ESA/ESOC, Darmstdat, Germany

    person_pin
    Javier BERZOSA MOLINA, GMV Aerospace and Defence, Tres Cantos, Spain
    P-37 - From Space-Based Measurements to Accurate State Vectors: Pipeline Design, Implementation, and Technical ChallengesPaolo GUARDABASSO, ARCA Dynamics, Rome, Italy
    Dario SPILLER, ARCA Dynamics, Rome, Italy

    person_pin
    Paolo GUARDABASSO, ARCA Dynamics, Rome, Italy
    P-38 - Analysis of orbit determination performance for SGDC-1 using multiple tracking stations.Márcia NUNES, Telebras, Brasilia, Brazil
    Rebeca RIBEIRO, Telebras, Brasilia, Brazil

    person_pin
    Rebeca RIBEIRO, Telebras, Brasilia, Brazil
    P-39 - Comparative analysis of synthetic covariance generation methods using ephemeris statisticsJérôme HUI, Aldoria, Paris, France
    Julien SMEJ, Aldoria, Paris, France
    Etienne BERTIN, Aldoria, Paris, France
    Alexis PETIT, Aldoria, Paris, France
    Emmanuel DELANDE, Centre National d’Études Spatiales (CNES), Toulouse, France
    Emeline VALETTE, Centre National d’Études Spatiales (CNES), Toulouse, France
    Christophe TAILLAN, Centre National d’Études Spatiales (CNES), Toulouse, France

    person_pin
    Jérôme HUI, Aldoria, Paris, France
    P-40 - SCARABAEUS: AN OPEN-SOURCE TOOL FOR INTERPLANETARY SPACECRAFT NAVIGATIONJay MCMAHON, University of Colorado Boulder, Boulder, United States
    Giovanni FEREOLI, University of Colorado Boulder, Boulder, United States
    Trevor WOLF, University of Colorado Boulder, Boulder, United States
    Zack ELLIS, University of Colorado Boulder, Boulder, United States
    Bushra ALDHANHANI, Technology Innovation Institute, Abu Dhabi, United Arab Emirates
    Mohamed KULEIB, Technology Innovation Institute, Abu Dhabi, United Arab Emirates
    Wendy FRANK, LASP, Boulder, United States
    Mattia PUGLIATTI, University of Colorado Boulder, Boulder, United States
    Mohamed ALMASHJARI, UAE Space Agency, Abu Dhabi, United Arab Emirates
    Jeremy KNITTEL, LASP, Boulder, United States

    person_pin
    Jay MCMAHON, University of Colorado Boulder, Boulder, United States
    P-41 - ?Analysis of the Error Sources in the SGP4 Analytical Satellite Theory and the Enhancement of Space Situational Awareness Analytical Satellite TheoriesPaul CEFOLA, University at Buffalo, Tisbury, United States
    Juan Felix SAN-JUAN, Scientific Computing & Technological Innovation Center, University of La Rioja, Logroño, La Rioja, Spain
    Miguel ALONSO, Scientific Computing & Technological Innovation Center, University of La Rioja, Logroño, La Rioja, Spain
    Rosario LOPEZ, Scientific Computing & Technological Innovation Center, University of La Rioja, Logroño, La Rioja, Spain
    Ivan PEREZ, Scientific Computing & Technological Innovation Center, University of La Rioja, Logroño, La Rioja, Spain
    Srinivas SETTY, Independent Astrodynamics and Space Systems Consultant, Germany, , Munich, Germany

    person_pin
    Juan Felix SAN-JUAN, Scientific Computing & Technological Innovation Center, University of La Rioja, Logroño, La Rioja, Spain
    P-42 - Positioning accuracy assessment of a lunar polar landerVincenzo MARIANI, Sapienza University of Rome, Rome, Italy
    Fabrizio DE MARCHI, Sapienza University of Rome, Rome, Italy
    Paolo RACIOPPA, Sapienza University of Rome, Rome, Italy
    Luciano IESS, Sapienza University of Rome, Rome, Italy

    person_pin
    Vincenzo MARIANI, Sapienza University of Rome, Rome, Italy
    P-43 - A Dynamic Lagrangian Mascon Framework for Gravity Modeling of Irregular Small BodiesYaqiong WANG, Paris Observatory, Paris, France
    Daniel HESTROFFER, Paris Observatory, Paris, France

    person_pin
    Yaqiong WANG, Paris Observatory, Paris, France
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