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: Dr. Florian Renk, European Space Agency (ESA), Germany;
Co-Chair: Prof. Manoranjan Sinha, Indian Institute of Technology Kharagpur, India;
Co-Chair: Dr. Feng Jinglang, University of Strathclyde, United Kingdom;

papers
Paper title	Presentation status	Speaker	Affiliation	Country
A Fast Evaluation Method for Spacecraft Low-Thrust Collision Avoidance Maneuvers Based on Differential Algebra		Mr. Jikai Wang	School of Astronautics, Beihang University	China
A Non-Contact Liquid Gyroscope Design for Improved Satellite Attitude Control		Mr. Paul Iustin Vartolomei	Politehnica University of Bucharest	Romania
Aerodynamic Analysis for Drag-controlled Collision Avoidance for the M2 CubeSats and the Feasibility of a LEO Space Corridor		Ms. Shathria Ompragash	UNSW Canberra	Australia
AI-Enabled Optical Navigation and Anomaly Detection for a Moon-Orbiting Spacecraft		Mr. Murathan Bakır	Istanbul Technical University	Türkiye
ai-powered procedural terrain generation for realistic martian and lunar rover simulations		Mr. Vishnurat Kadagadakai	Ramaiah Institute of Technology	India
An analytical geometric approach for determining satellite occultation events	confirmed	Dr. Vladislav Zubko	Space Research Institute (IKI), Russian Academy of Sciences (RAS)	Russian Federation
attitude guidance for arbitrary imaging missions of earth observation satellites		Mr. Jeonghoon Hyun	Korea Aerospace Research Institute (KARI)	Korea, Republic of
bio-inspired ai for autonomous spacecraft swarm coordination		Mr. Vishnurat Kadagadakai	Ramaiah Institute of Technology	India
Comparative Study of Spacecraft Trajectory Simulation Tools		Mr. Oluwatosin Kolade	Obafemi Awolowo University	Nigeria
Development of Launch Vehicle Flight Simulation Software to verify Guidance and Control for HILS(hardware-in-the-loop simulation) Testing		Mr. Yong Kyu Park	Korea Aerospace Research Institute (KARI)	Korea, Republic of
ROBUST TRAJECTORY OPTIMIZATION SOFTWARE USING DIFFERENTIAL DYNAMIC PROGRAMMING		Mr. Shun Kodama	Research Institute of Systems Planning, Inc. / ISP	Japan
Diffusion Enhanced Model Predictive Control for Autonomous Spacecraft Rendezvous and Docking with Obstacle Avoidance		Mr. Biyue Pan	Beihang University (BUAA)	China
Dual quaternion-based kinematic control of space manipulators: from theory to experimental validation		Mr. Hadi Jahanshahi	York University	Canada
Efficient Design for Optimal Finite-Thrust Transfer Using Sequential Convex Programing		Mr. Hailiao Wang	Beihang University (BUAA)	China
Enhancing Path Planning for High-Altitude Balloon Missions: Strategies for Improved Trajectory Accuracy and Payload Recovery		Mr. Adam Brogan	University of Glasgow	United Kingdom
intelligent spacecraft avoidance maneuver strategies for an uncertain number of threat targets		Dr. Wang zhengtao	Harbin Institute of Technology	China
MONET: an industry-oriented software suite for mission analysis		Mr. Simone Proietti	Thales Alenia Space	Italy
Open-Source High-Fidelity Orbit Estimation for Planetary Science and Space Situational Awareness Using the Tudat Software		Mr. Luigi Gisolfi	Delft University of Technology	The Netherlands
Adaptive Guidance with Real-Time Performance Compensation for Mars Ascent Vehicles under Local Degradation		Mr. Bohao Du	School of Astronautics, Beihang University	China
Optimizing Low-Thrust Trajectories for Sustainable Lunar Missions in Cislunar-Space		Mr. Samarth Badgujar	University of Padova - DII	Italy
Orbit determination of constellation satellites with maneuvers based on sparse optical data		Dr. Shengxian Yu	Purple Mountain Observatory (PMO)	China
Orbit-Phasing Based Transfer Trajectory to Inclined Heliocentric Orbit around Sun-Earth L4		Mr. Gunhee Yi	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
Performance Analysis and Design Framework for Earth Observation Small-Satellite Constellations		Mr. Jaeyoul Ko	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
Robust TLE Outlier Detection Algorithm with Manoeuvre Detection Capabilities		Mr. Louis Bruninx	Delft University of Technology	Belgium
Design of Safe Transfer Trajectory between Quasi-Satellite Orbits		Dr. Yusuke Oki	Japan Aerospace Exploration Agency (JAXA)	Japan
SPACECRAFT CONTROL IN CONSTRAINED ENVIRONMENTS: BARRIER LYAPUNOV FUNCTION-BASED RENDEZVOUS AND DOCKING WITH HYBRID ACTUATOR ASSEMBLY		Ms. Tanya Krishna Kumar	Indian Institute of Technology Kanpur	India
Stochastic Trajectory Optimization for Satellite Swarm Reconfiguration via Convex Optimization		Dr. LIXIANG WANG	Research Center of Satellite Technology, Harbin Institute of Technology	China
The self-gravitating ring in the N-body problem		Ms. Rosaura Patricia Delgado Ortiz	Altum Principia	Mexico
TRAJECTORY OPTIMIZATION FOR MULTIPLE ROUND-TRIP TRANSFERS BETWEEN LEO AND DRO IN AIRLINE FLIGHT MODE		Ms. Qingqing Li	Tsinghua University	China
Wide Field-of-View RF Monitoring for Enhanced Orbit Determination of Uncorrelated Tracks		Dr. Ryan Nosrati		Australia
Applications of Space Tethers in Orbital Manoeuvres		Dr. Vladimir Razoumny	RUDN University	Russian Federation
Assessing orbital lifetime stability around Mercury: Implications for the BepiColombo Mission		Dr. Josué Cardoso dos Santos	University of Colorado Colorado Springs	United States
Chandrayaan Lunar Connectivity: A scalable Earth-Moon communication constellation leveraging India’s Chandrayaan-2 Orbiter		Ms. Savri Gandhi	Georgia Institute of Technology	United States
Dynamic Modeling and Dual-Cabin Coordinated Attitude Adjustment of High-Precision Disturbance-Free Payload Spacecraft		Mr. Hanzhou Wang	Beihang University (BUAA)	China
Graphical Solution to Kepler's Time Equation		Mr. Jeremy Partington		Australia
verified computation of ocean tide perturbations		Dr. Stefano Casotto	University of Padua	Italy
Feedback Landing Guidance for Reusable Launch Vehicle in Atmosphere based on Homing Guidance		Mr. Hyeonjae Kim	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
Novel Eclipse-Avoidance Strategy for Solar Electric Propulsion Spacecraft		Mr. Nicholas Nurre	Auburn University	United States
Multi-Objective Optimization of Lunar Navigation Satellite System using Genetic Algorithm		Mr. Rameez Ahmed Malik	University of New South Wales	Australia
Orbit Maintenance Strategy Integrated with Power Management for Ultra-low Earth Orbit Satellites		Ms. Jixin Ding	School of Astronautics, Beihang University	China
Safety Enhanced Optimal Learning for Solar Sail Spacecraft Earth-to-Mars Transfers		Dr. Lin Cheng	Beihang University (BUAA)	China
non-gaussian chance-constrained trajectory for spacecraft rendezvous and docking using gaussian mixtures		Ms. Wenjie Su	Beihang University	China
Safe Reinforcement Learning for Autonomous Rendezvous and Proximity Operations: Balancing Safety and Performance in CubeSat Docking Missions		Mr. Simone Rotondi	Sapienza University of Rome	Italy
onboard low-thrust spacecraft collision avoidance strategy design and optimization	confirmed	Dr. Yanjun YU	Harbin Institute of Technology	China
Low-Thrust Trajectory Design with Power Constraints and Attitude Dynamics Integration		Mr. Gianni Pecora	Universidad Carlos III de Madrid	Spain
Minimum Fuel Indirect Optimal Control Transfers Across Multiple Regimes in the Earth-Moon System		Dr. Mihir Vedantam	The University of Texas at Austin	United States
Dimensionality reduction in angles-only\\ optimal orbit determination		Mr. Edgar Kirchner	Technische Universität München	Germany
Low-Cost rendezvous and phasing with the Lunar Gateway leveraging quasi-periodic tori		Mr. Matteo Santacesaria	Politecnico di Milano	Italy
Transformer for Orbit Propagation with Application to Precise Repeat-Track Orbit Design		Mr. Zhe Xu		China
Low-thrust Minimum-time Orbital Transfer using Picard-Chebyshev Homotopy Method		Mr. Syed Shan Ali Shah	School of Astronautics,Northwestern Polytechnical University	China

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