session IP

Title: Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUM
type: interactive
Description: This session offers a unique opportunity to deliver your key messages in an interactive presentation on any of the subjects of Astrodynamics addressed in the classic Sessions. The presentation will be displayed on a digital screen in a dedicated location and available for view by all Congress attendees for the entire Congress week. In addition, one afternoon is dedicated exclusively for the attendees to view the Interactive Presentations, and the author will be assigned a specific ten minute slot to personally present the topic and interact with the attendees present. The Interactive Presentation may take advantage of all electronic display capabilities, such as: PowerPoint charts, embedded hot links, pictures, audio and video clips etc. An award will also be presented to the author of the best Interactive Presentation in the C Category at a special ceremony. An Abstract that follows the standard format must be submitted by the deadline for standard IAC abstracts.
Room: IP Area

IPC members

Co-Chair: Dr. Vladimir Razoumny, RUDN University, Russian Federation;
Co-Chair: Prof. Manoranjan Sinha, Indian Institute of Technology Kharagpur, India;
Co-Chair: Dr. Feng Jinglang, University of Strathclyde, United Kingdom;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
Reinforcement Learning-based Relative Configuration Maintenance for Large-Scale Constellations			Mr. Longwei Xu	Harbin Institute of Technology	China
Real-Time Stochastic Optimal Attitude Stabilization for Autonomous Spacecraft via Sequential Power-Series Approximation		confirmed	Mr. Hengpeng Lun	Beihang University	China
Learning-Based Time-Synchronized Control for Disturbance-Free Dual-Cabin Spacecraft with Obstacle Avoidance		confirmed	Mr. Xiang Guo	Beihang University (BUAA)	China
Hierarchical Sequential Convex Programming for Stochastic Fuel-Optimal Low-Thrust Trajectory Design under Uncertainty		confirmed	Mr. Hengpeng Lun	Beihang University	China
Global Search for Optimal Solar Sail Trajectories Using Diffusion Models		confirmed	Mr. Shizhan Gao	School of Astronautics, Beihang University	China
Frequency-Constrained Predictive Shaping Control for Dumbbell-Shaped Flexible Spacecraft Vibration Suppression		confirmed	Mr. Xinhai Ma	Harbin Institute of Technology	China
Neural Network Assisted Adaptive Covariance Tuning for Quaternion Based CubeSat EKF	10	confirmed	Mr. Karhan Göktuğ Yasar	Turkish-German University	Türkiye
composite anti-disturbance control for energy-efficient operation of very low earth orbit vehicles servo system			Mr. Shaoguang Rong	Beihang University (BUAA)	China
Center Manifold Direction-Field Guidance for In-Family Low-Thrust Reconfiguration of Halo Orbits		confirmed	Mr. Bohao Du	School of Astronautics, Beihang University	China
Automated Gravity-Assist Trajectory Optimization for Uranus Missions from 2026 to 2050			Dr. Nan Zhang	Beihang University (BUAA)	China
An Improved Monte Carlo Tree Search for Autonomous Optimization of Low-Thrust Gravity-Assist Sequences		confirmed	Ms. Yutong Guan	Harbin Institute of Technology	China
Orbit control and de-orbiting using electrodynamic tethers	10	confirmed	Dr. Antonio Prado	National Institute for Space Research - INPE	Brazil
A Digital-Twin and Hardware-in-the-Loop Framework for CubeSat ADCS Verification	10	confirmed	Mr. Ali Elmorshedy	United Arab Emirates University (UAEU)	United Arab Emirates
A Hybrid Approach for Attitude Determination and Sensor Calibration in CubeSats	10	confirmed	Mr. Angelo Espinoza Valles	Samara National Research University (Samara University)	Russian Federation
Design of a Sun Sensor Emulation Board for Flat-Sat HIL Tests	10	confirmed	Mr. Francesco Cataffo	Politecnico di Milano	Italy
Enhanced Geomagnetic Field Measurement-based Autonomous Orbit Determination for Small Satellites in LEO		confirmed	Mr. Filipe Cardoso	University of Brasilia	Brazil
Rotation-Minimizing Tidal-Impedance Relative Dynamics for Near Rectilinear Halo Orbit Proximity Operations: Application to the Lunar Gateway			Mr. Harish Vernekar	University of Arizona	United States
Multi-Formulation Uncertainty-Aware LEO Drag Propagation with First-Exit Risk Metrics		confirmed	Mr. Nijanthan Vasudevan	West Virginia University	United States
hybrid dynamical–statistical orbit determination in the restricted three-body problem under sparse observability for debris monitoring and navigation		confirmed	Dr. Jessica Gyegwe		Nigeria
Improved POD of Sentinel-6a by a high precision thermal radiation pressure model		confirmed	Dr. Benny Rievers	ZARM, University of Bremen	Germany
Uncertainty-Aware Floquet Mode Approach for Stationkeeping of Libration Point Orbits		confirmed	Dr. Xiaoyu Fu	University of Liverpool	United Kingdom
A categorization of J2-problem intermediaries from their efficiency in developing an AI-based LEO propagator		confirmed	Dr. Yuying Liang	Beihang University (BUAA)	China
Adaptive Segmentation Strategies for MCPI in Coupled VLEO Orbit-Attitude Propagation			Mr. Hamza Eren Gunaltay	Surrey Space Centre, University of Surrey	United Kingdom
Artificial Neural Networks for Initial Orbit Determination: A Two-Epoch Approach for LEO		confirmed	Mr. Ömer Utku Örengül	University of Turkish Aeronautical Association	Türkiye
An autonomous ai-driven collision avoidance architecture for multi-object orbital conjunction scenarios		confirmed	Mr. Ali Haydar Kara	Samsun University	Türkiye
research on intelligent orbit generation and classification method for efficient reconstruction of poincaré sections		confirmed	Mr. Xukang Xie	Sun Yat-sen University (Guangzhou)	China
Stability of Averaged Frozen Orbits Around Mercury: Effects of Short-Period Corrections		confirmed	Dr. Josué Cardoso dos Santos	University of Colorado Colorado Springs	United States
Hierarchical Trajectory Planning for Multi-Modal Space Truss Construction Robots		confirmed	Dr. Jianlin Chen	Weiqiao-UCAS (Binzhou) Science and Technology Co., Ltd.	China
Reinforcement learning-based gnc for powered descent and precision landing on mars using ppo and a recurrent linear transformer		confirmed	Mr. Mattas Ten Voorde	Delft University of Technology (TU Delft)	Netherlands (Kingdom of the)
Efficient Planning and Guidance for Constellation Reconfiguration based on J2-Perturbed Lambert Solver		confirmed	Mr. Giulio De Angelis	Sapienza University of Rome	Italy
GNSS-Based Ground-Target Direction Estimation for Accurate Beam Pointing in the OHISAMA Wireless Power Transmission Demonstrator		confirmed	Mr. Simon Maillot	The Graduate Universty for Advanced Studies (SOKENDAI)	Japan
Multi-view ICP-Based Registration for Pose Estimation and 3D Reconstruction of Non-Cooperative Targets		confirmed	Dr. Alessia Nocerino	University of Naples "Federico II"	Italy
Vision-Based Relative Pose Estimation for Non-cooperative Spacecraft via Line-Segment Distributions		confirmed	Mr. Bohyun Chang	Korea Advanced Institute of Science and Technology (KAIST)	Republic of Korea
Model-based design and verification of a CubeSat ADCS with ground target tracking mode for optical communication		confirmed	Dr. Joseph Thompson	University College Dublin (UCD)	Ireland
Passively Safe Hierarchical Framework for Large-Scale Satellite Swarms			Mr. Chenglong Xu	School of aeronautics and astronautics, Sun Yat-Sen University Guangzhou	China
Argon-C: Autonomous Real-Time Spacecraft Guidance via Optimal Neural Collocation — Inspired by the ATHENA Pointing Scenario		confirmed	Mr. Luca Macchiaiolo	OHB System AG-Bremen	Germany
Data-Efficient Generative Learning of Spacecraft Swarm Density Control with Neural ODE and Configuration Invariant		confirmed	Mr. Junfeng Yuan	Beihang University	China
Trajectory Design for Multi-Target L4 Trojan Flybys Using Jovian-system Gravity Assists for Rideshare Probes		confirmed	Mr. Yixuan Wu	Tsinghua University	China
Analysis of Reaction Wheel Configuration and Performance for Small Agile Earth Observation Satellites		confirmed	Mr. Darpanjeet Deka	Sapienza University of Rome	Italy
Agile Nanosatellite Attitude Control with Reaction Wheels and On-Off Thrusters via embedded convex optimization		confirmed	Mr. Franklin Josue Ticona Coaquira	Kyushu Institute of Technology	Japan
Solar gravity perturbations on Enceladus science orbits		confirmed	Mr. Gabriel Richard	ISAE-Supaero University of Toulouse	France
Determining Eclipse Duration for a Venus Orbiter Using a Geometric Shadow Curve Model		confirmed	Dr. Vladislav Zubko	Space Research Institute (IKI), Russian Academy of Sciences (RAS)	Russian Federation
Optimized approach for performance-enhanced satellite attitude control		confirmed	Dr. ELHASSEN BENFRIHA	Agence Spatiale Algérienne (ASAL)	Algeria
Long-Term Orbital Dynamics with a Self-Sustaining Energy Modulation of Solar Sail in Near Earth Space		confirmed	Ms. Xiaohan Jing	National Space Science Center (NSSC), Chinese Academy of Sciences	China
dual-actuator attitude control of flexible satellite using pd with movable mass		confirmed	Dr. jalal eddine benmansour	Agence Spatiale Algérienne (ASAL)	Algeria
Efficient Dynamic Analysis of Tethered Net Capture for Space Debris using Linear Complementarity Problem		confirmed	Mr. Ryotaro Ichimiya	Aoyama Gakuin University	Japan
Integrated Terrain-Relative Navigation and Hazard Detection Framework for Autonomous Lunar Precision Landing		confirmed	Mr. Çağrı ÇIBUK	Isik University	Türkiye
A Scalable Lunar Repeat Ground-Track Constellation for Persistent South Pole Observation		confirmed	Mr. YUHANG YU	Tsinghua University, Beijing	China
RRT-Based Multi-Dimensional Homotopy for Propellantless Solar-Sail Transfer Optimization		confirmed	Mr. Xinliang Liu	Harbin Institute of Technology	China
An improved hybrid CNN-LSTM and pseudospectral method for space shuttle reentry trajectory optimization		confirmed	Mr. Yuanxin Yang	Northwestern Polytechnical University	China
Interplanetary Trajectory Optimization Using Planet-Satellite Consecutive Gravity Assists			Mr. Jialong Song	Tsinghua University	China
Data-Driven Nonlinear Model Predictive Control for Spacecraft Landing with Optimization through Lyapunov-stable Learned Terminal Cost		confirmed	Mr. Hongmai Chen	Beihang University	China

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