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 (Hall B)

IPC members

Co-Chair: Dr. Diane Davis, National Aeronautics and Space Administration (NASA), Johnson Space Center, United States;
Co-Chair: Dr. Florian Renk, European Space Agency (ESA), Germany;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
Advanced attitude determination and control testing in a modular solution	10	confirmed	Mr. Riccardo Spartà	Politecnico di Torino	Italy
A Novel Approach for Autonomous Spacecraft Recovery to Sun Pointing Orientation	10	confirmed	Mrs. KanuPriya Govila	Indian Space Research Organization (ISRO)	India
Attitude and bias estimation of the agile satellite with high dynamic performance based on L1-TSAKF	10	confirmed	Mr. Ziran Liu	Research Center of Satellite Technology, Harbin Institute of Technology	China
Coupled rendezvous and docking maneuver control of spacecraft using fast fixed-time sliding mode controller	10	confirmed	Mr. Rakesh Kumar Sahoo	Indian Institute of Technology Kharagpur	India
DESIGN, TEST, AND VERIFICATION OF A REACTION WHEEL FOR CUBESATS	10	confirmed	Mr. Zayed Alkatheeri	Khalifa University of Science and Technology (KUST)	United Arab Emirates
Simulation of the attitude pointing performance of CubeSats for optical communications	10	withdrawn	Ms. Elisa Garbagnati	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
Applying Fictitious Reference Iterative Tuning to Quaternion Feedback and Quantitative Evaluation	10	confirmed	Mr. Ozeki Yusaku	Tokyo Institute of Technology	Japan
In-Orbit Allan Variance for Gyroscope Noise Characterization in Earth Observation Satellites	10	confirmed	Mr. Tomás Ignacio Burroni	Satellogic	Spain
Methodology and Dedicated Software Development to Provide Passive Magnetic Attitude Control for CubeSats	10	confirmed	Ms. Tirza Ohana Berger de Souza	Samara National Research University (Samara University)	Russian Federation
Spacecraft dynamic window attitude planning method for planetary approach detection	10	confirmed	Mr. CongCong Luo	Beijing Institude of technology	China
Chaotic behavior of high and eccentric Earth orbits---The case of ESA's Integral space observatory	10	confirmed	Dr. Juan Félix San-Juan	Universidad de La Rioja	Spain
Ionospheric Plasma Drag on Small Satellites in Low-Earth Orbit	10	confirmed	Dr. Simone Di Fede	Nanyang Technological University	Singapore, Republic of
Long-term orbital dynamics surrounding an eccentric binary asteroid system by triple averaging	10	withdrawn	Mr. Yongjie Chen	School of Astronautics, Beihang University	China
On the refinement of low-energy Earth–Moon transfer families into an ephemeris model	10	confirmed	Mr. Claudio Toquinho Campana	Politecnico di Milano	Italy
Orbit determination for X-ray pulsar navigation with the aid of artificial neural networks	10	confirmed	Ms. Sui Chen	Politecnico di Milano	Italy
Restricted Four Body Problem Chaotic Analysis of Phase Space Structures for Natural Multi-Moon Transfers	10	withdrawn	Mr. Suryansh Aryan	Virginia Tech	United States
Safe Short-Term Loitering in Gateway's Near Rectilinear Halo Orbit	10	confirmed	Mr. Matthew Bolliger	Advanced Space	United States
Design of periodic orbit inclined to the sun line around an asteroid with imperfectly reflecting solar sail	10	confirmed	Ms. Moe Yasuda	Tokyo Institute of Technology	Japan
Exploring new periodic orbits for the n-body problem	10	confirmed	Ms. Margaux Introna	University of Trento, Department of Physics, National PhD in Space Science and Technology	Italy
Long-term evolution of orbits in cislunar space: characterisation and stability analysis	10	confirmed	Ms. Mathilda Bolis	Politecnico di Milano	Italy
Numerical Continuation and Stationkeeping of Quasi-Periodic Quasi-Satellite Orbits around Phobos	10	confirmed	Dr. Xiaoyu Fu	University of Liverpool	United Kingdom
Transfer to asteroids during close encounter using finite-time Lyapunov exponent fields	10	confirmed	Mr. Tianji Chen	Beihang University	China
An Orbital Game Control Algorithm for On-Board Application by Behaviour Cloning	10	confirmed	Dr. Simeng Huang	Tsinghua University	China
Automated Computation of Optimal Spiral Trajectories in the Circular Restricted Three-Body Problem	10	confirmed	Mr. Grant Hecht	University at Buffalo	United States
enhanced convex optimization strategies in 6-dof non-coplanar orbital maneuver trajectory design	10	confirmed	Mr. Haobo Kang	Research Center of Satellite Technology, Harbin Institute of Technology	China
Global Trajectory Optimization with Alphazero: A Novel Approach Applied to the GTOC 11 Challenge	10	confirmed	Mr. Andrea Forestieri	Politecnico di Torino	Italy
Impulsive station-keeping of frozen orbits around planetary moons using manifolds of averaged dynamics	10	withdrawn	Mr. Yongjie Chen	School of Astronautics, Beihang University	China
Non-Smooth Deviation Evolution Analysis in Cislunar Midcourse Correction Trajectory Under Maneuver Execution Threshold	10	confirmed	Dr. Zeyue Li	National University of Defense Technology	China
Optimal low-thrust trajectory approximation via singular perturbation theory	10	confirmed	Mr. Danilo Zona	Università del Salento	Italy
Regularization and a hybrid pseudospectral, shape-based solver for low-thrust optimal control	10	confirmed	Mr. Sergio Cuevas del Valle	Universidad Rey Juan Carlos	Spain
Robustness Assessment of Asteroid Approach Trajectory Regarding Thruster Failures and Missed Maneuvers	10	confirmed	Mr. Paul Pinteau	ISAE - Institut Supérieur de l'Aéronautique et de l'Espace	France
Systematic Analysis of Cislunar Escape Opportunities for Exploration and Planetary Defence Missions	10	confirmed	Dr. Andrea Pasquale	GMV GmbH	Germany
Trajectory Design of NRHO Transfer with Continuous Launch Window for Logistics Resupply Mission to Gateway	10	confirmed	Mr. Junji Kikuchi	Japan Aerospace Exploration Agency (JAXA)	Japan
Trajectory Optimization for Jovian Moon Exploration using Single and Multi-Objective Beam Search	10	confirmed	Mr. Andrea Marrazza	ISAE - Institut Supérieur de l'Aéronautique et de l'Espace	France
Advances in Koopman Operator Methods for Astrodynamics Applications	10	confirmed	Mr. Oluwatosin Kolade	Obafemi Awolowo University	Nigeria
AI-Enhanced Visualization and Control of Swarm Satellites Utilizing Geomagnetic Actuators	10	confirmed	Ms. Tanya Krishna Kumar	Indian Institute of Technology Kanpur	India
Characterization of Orbits in Cislunar Space for Space Traffic Management	10	confirmed	Mr. Sourav Ghosh	Space Generation Advisory Council (SGAC)	India
Drag Coupling of Attitude and Orbital Dynamics for LEO Satellites.	10	confirmed	Mr. Thomas McIlwraith	University of Strathclyde	United Kingdom
Exploring stable and chaotic regions to design a space mission around a body with a large crater	10	confirmed	Prof. Silvia Giuliatti Winter	São Paulo State University - Universidade Estadual Paulista (UNESP)	Brazil
Lunar Constellation Deployment Techniques Leveraging Natural Perturbations	10	confirmed	Dr. Andrea Pasquale	GMV GmbH	Germany
Optimal Control of Spacecraft with an Air-Breathing Electric Propulsion in Ultra-Low Orbits	10	confirmed	Dr. Egor Loktionov	Bauman Moscow State Technical University	Russian Federation
Optimal Far-Range Rendezvous Trajectory Design of Low-Thrust Electric Propulsion Spacecraft using Deep Reinforcement Learning	10	confirmed	Mr. Arya Das	Indian Institute of Technology Kanpur	India
A Polynomial-Based Differential Dynamic Programming Optimisation Method for Space Trajectory Design	10	confirmed	Mr. Thomas Caleb	ISAE-Supaero University of Toulouse	France
Analysis of Transfer Trajectory from NRHO to Lunar Orbit of Various Inclination for Gateway Release Mission	10	confirmed	Mr. Junji Kikuchi	Japan Aerospace Exploration Agency (JAXA)	Japan
General Approach to Solve Low-Thrust Multi-Target Space Logistics Problems	10	confirmed	Mr. Riccardo Apa	Politecnico di Torino	Italy
Inspection of Space Rider with a 12U CubeSat: Ensuring Safety and Efficiency	10	confirmed	Mr. Luca Bartolucci	Politecnico di Torino	Italy
Mission Feasibility for Interstellar Object Exploration through Utilization of Advanced Propulsion Technologies	10	confirmed	Prof. Jekanthan Thangavelautham	University of Arizona	United States
Multi-target space mission sequence optimization with deep reinforcement learning	10	confirmed	Mr. Edward Tomanek-Volynets	University of Glasgow	United Kingdom
Rassvet-1 Tech Demo Mission for Broadband Internet Constellation: On-Orbit Results and Lessons Learned	10	confirmed	Ms. Irina Ponomareva		Russian Federation
Attitude-trajectory coupling adaptive control for flexible landing on small celestial body	10	confirmed	Ms. Bingjie Lu	Beijing Institude of technology	China
Onboard Perception-based Autonomous Visual Navigation around Small Celestial Bodies	10	confirmed	Dr. Avijit Banerjee	Luleå University of Technology	Sweden
Performance Assessment of Crater-Based Navigation for Autonomous Moon Landing	10	withdrawn	Mr. Jean-Francois Hamel	NGC Aerospace Ltd.	Canada
Feasibility Study of an All-Electric Rendezvous Mission in GEO Orbit	10	confirmed	Mrs. Damiana Losa	Thales Alenia Space	France
CNN-based Visual Navigation: Optimization Strategies for Monocular Pose Estimation in Proximity Operations	10	confirmed	Mrs. Lucrezia Lovaglio	Politecnico di Torino	Italy
Orbit-attitude coupled guidance and control for constrained trajectory generation and tracking during final approach to non-cooperative spacecraft	10	confirmed	Mr. Agostino Madonna	University of Naples "Federico II"	Italy
Optimization-based actuator management for hybrid control allocation	10	confirmed	Mr. Jesús Ramírez	SENER Aeroespacial	Spain
Approximate Analytical Solution to Spacecraft Optimal Docking Using Koopman Operator Theory	10	confirmed	Mr. Zhan Feng	School of Astronautics, Beihang University	China
Optical and Radio Data Fusion for Spacecraft Navigation and Geophysical Investigations	10	confirmed	Ms. Martina Ciambellini	Sapienza University of Rome	Italy
LSTM-based Fast Predictive Guidance for Autonomous Safe Docking with Path and Control Constraints	10	confirmed	Mr. Kumud Darshan Yadav	University of Seville	Spain

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