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
- 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;
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 |
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Simulation of the attitude pointing performance of CubeSats for optical communications | 10 | withdrawn | Ms.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 | Reflex Aerospace | Germany |
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 |
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 |
10 | confirmed | Ms. Moe Yasuda | Tokyo Institute of Technology | Japan | |
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 | 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 |
10 | withdrawn | Mr. Yongjie Chen | School of Astronautics, Beihang University | China | |
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 |
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 |
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. Samarth Badgujar | Jain University | 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 |
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 |
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 | Ms. Serena Campioli | Politecnico di Torino | Italy |
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 |
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 |
10 | confirmed | Mr. Antonio D'Ortona | Politecnico di Torino | Italy | |
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 |