IPB

session IPB

Title: Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUM
type: interactive
Room: IP Area (Hall B)

IPC members

Co-Chair: Dr. Diane Davis, NASA, United States;
Co-Chair: Dr. Florian Renk, European Space Agency (ESA), Germany;
Co-Chair: Prof. Kathleen Howell, Purdue University, United States;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
Robust Attitude Control for Space Target Pointing in Proximity Operations	15	confirmed	Mr. Tobia Armando La Marca	Scuola Superiore Meridionale	Italy
Exploiting gauge freedom in KS variables for high-performance numerical orbital propagation	15	confirmed	Mr. Sergio Cuevas del Valle	Universidad Rey Juan Carlos	Spain
Constrained attitude control of spacecraft under angular velocity constraints and input saturation	15	confirmed	Mr. Ming LU	Research Center of Satellite Technology, Harbin Institute of Technology	China
Generalized Precise Orbit Prediction of LEO Satellites via Physics Informed Machine Learning	15	confirmed	Dr. Takashi Maruyama	NEC Laboratories Europe	Germany
Euclid Fine Guidance Sensor: design and ground validation	15	confirmed	Mrs. Chiara Finocchietti	Leonardo S.p.A	Italy
Study on Resonant Flyby Trajectory Design \\ using Symbolic Regression in CRTBP	15	confirmed	Mr. Shota Ito	Tokyo Metropolitan University	Japan
Advanced optimization method for high-thrust and Weak Stability Boundary End-to-End high-fidelity Earth-Moon trajectories with space manoeuvres	15	confirmed	Mr. Andrea D'Ottavio	Thales Alenia Space Italia (TAS-I)	Italy
Controllability of orbiting solar reflectors under structural failures.	15	confirmed	Dr. Iain Moore	University of Glasgow	United Kingdom
Designing cislunar co-orbital transfer networks in the Earth-Moon system	15	confirmed	Mr. Ying Ding	Beijing Institude of technology	China
Defining Admissible Maneuvers and Resulting Reachability Sets in the Three-Body Problem using Hamiltonian Normal Form Methods	15	confirmed	Dr. Puneet Singla	Pennsylvania State University	United States
analysis of multiple gravity-assist opportunities based on feasibility domains	15	confirmed	Ms. Zhiyuan Cao	Beijing Institude of technology	China
Semi-Analytical Approach for Lunar Capture under Solar Gravity Perturbation in the Elliptic Restricted Three-Body Problem	15	confirmed	Mr. Takayuki Shihara	University of Tokyo	Japan
advancing solutions for the three-body problem through physics-informed neural networks	15	confirmed	Mr. Manuel Pereira	Faculdade de Ciências e Tecnologia - UNL	Portugal
Continuous Estimator for Space Logistics Network Optimization with Multiple Vehicles	15	withdrawn	Prof. Liqiang Hou	Shanghai Jiaotong University	China
Reinforcement Learning for Real-Time Low-Thrust Relative Orbital Rendezvous Design	15	confirmed	Mr. Longwei Xu	Harbin Institute of Technology	China
Reachable Set of Invariant Manifold with Low Thrust	15	confirmed	Dr. Yang Wang	Nanjing University	China
Satellite formation control using multi-agent deep reinforcement learning	15	confirmed	Ms. heng jiang	Beihang University	China
Accelerating Mega-Constellation Design: Efficient Visibility Computation and Multi-Shell Optimisation	15	confirmed	Mr. Vassili Tunjov	Delft University of Technology (TU Delft)	The Netherlands
unsaturated maintenance and reconstruction of high specific impulse spacecraft formation	15	confirmed	Dr. Lin Chen	Beihang University (BUAA)	China
Complex analysis of a mission to Venus with gravity assist and resonant orbits under the lander-orbiter constraints	15	confirmed	Mr. Andrey Belyaev	Space Research Institute (IKI), Russian Academy of Sciences (RAS)	Russian Federation
Vigil – Transfer design for the European Space Agency’s Space Weather Mission to the Sun-Earth Libration Point 5	15	confirmed	Dr. Florian Renk	European Space Agency (ESA)	Germany
Robust trajectory design of impulsive multi-flyby trajectories with chance-constraint formulation	15	withdrawn	Dr. Nicola Marmo	Sapienza University of Rome	Italy
Low-Thrust Assisted Periodic Orbits Around Small Bodies via Indirect Optimal Control	15	confirmed	Dr. Shanshan Pan	Kyushu University	Japan
Observability-based orbiter aided cooperative navigation for asteroid landing	15	confirmed	Dr. Wenbo Xiu	Beijing Institude of technology	China
Applying Machine Learning Techniques for Optical Navigation in Lunar Missions	15	confirmed	Dr. Pablo Ghiglino		Switzerland
Design and Optimization of Multi-Rendezvous Maneuvres based on Reinforcement Learning and Convex Optimization	15	confirmed	Mr. Antonio López Rivera	Delft University of Technology	The Netherlands
A robust approach merging deep learning and unscented Kalman for vision based space rendez-vous	15	confirmed	Mr. thomas chambon	IRT Saint Exupéry	France
Synthetic Variable-Baseline Variable-Orientation Stereo Camera System for Relative Navigation in Close Proximity	15	confirmed	Mr. Niccolò Faraco	Politecnico di Milano	Italy
RCDs-based feedback control of a solar sail spacecraft at the Earth-Sun L1 point with dual pointing requirements	15	confirmed	Mr. Hongyi Xie	Politecnico di Milano	Italy
Model Predictive Control Strategy with a Decreasing Horizon Interval for a Reusable Launcher in a Landing Scenario	15	confirmed	Mr. Guillermo Zaragoza Prous	Cranfield University	United Kingdom
Long-Term Station Keeping around Earth-Moon Synodic Resonant Halo Orbits Using Solar Sails in High-Fidelity Dynamics Model	15	confirmed	Dr. Toshihiro Chujo	Tokyo Institute of Technology	Japan
Robust Powered Descent Guidance Using Successive Convexification and Tube Model Predictive Control	15	confirmed	Mr. Duozhi Gao	Harbin Institute of Technology	China
Rapid Convex Guidance for Long-Range Spacecraft Rendezvous	15	withdrawn	Dr. Ethan Burnett	Politecnico di Milano	Italy
An Efficient Optical Navigation Model for Monte-Carlo Feasibility Analysis: Limits of Horizon-Based Cislunar Autonomy	15	confirmed	Ms. Emma Topolcsik	San Diego State University	United States
Descentralized control scheme for small satellite with manipulators	15	withdrawn	Dr. Rolando Cortés Martínez	BTU Cottbus	Germany
Autonomous Fault Management in Attitude Determination and Control Subsystems: Hardware and Processor in the Loop Testing	15	confirmed	Dr. Andrea Colagrossi	Politecnico di Milano	Italy
Optimization of Electrospray Thruster Configuration and Control Allocation for Spacecraft Attitude Control	15	confirmed	Mr. Riccardo Gatti	Politecnico di Torino	Italy
Deep learning based resolution of attitude ambiguities for relative pose estimation of unknown and uncooperative targets	15	confirmed	Mr. Matteo Rosa	Politecnico di Milano	Italy
adaptive correction network incorporating rate gyro weighting for heavy launch vehicle attitude control	15	confirmed	Mr. Xing-yu Jiang	Beihang University (BUAA)	China

session IPB

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