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.
Date: 2022-09-21
Time: 13:30
Room: IP Area

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;
Co-Chair: Mr. Vincent Martinot, Thales Alenia Space France, France;
Co-Chair: Prof. Stéphanie Lizy-Destrez, Institut Supérieur de l'Aéronautique et de l'Espace (ISAE), France;
Co-Chair: Dr. Elena Fantino, Khalifa University of Science and Technology (KUST), United Arab Emirates;
Co-Chair: Prof. Hanspeter Schaub, Colorado Center for Astrodynamics Research, University of Colorado, United States;
Co-Chair: Prof. Erick Lansard, Satellite Research Center, Nanyang Technological University (NTU), Singapore, Republic of;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
Multiple Input Multiple Output Adaptive Controllers for a Titan Rover Concept	10	confirmed	Mr. Andrés Jiménez Mora	Instituto Tecnológico de Costa Rica (TEC)	Costa Rica
Design and Implementation of a Multi-Mission Torque Model Simulator for Earth Satellites	10	confirmed	Ms. Fatima Alnaqbi	Khalifa University of Science and Technology (KUST)	United Arab Emirates
Model Predictive Spacecraft Attitude Control with Physics-Inspired Neural Dynamics Learning	10	withdrawn	Mr. Jiangliang Fu	Shanghai Jiao Tong University	China
Distributed Guidance for Flexible Spacecraft Landing on Asteroid	10	confirmed	Ms. Chengyu Zhang	Beijing Institute of Technology (BIT)	China
A preliminary investigation of aerogravity assist missions to Ceres and other asteroids using various trajectory paths	10		Ms. Divinaa Burder	Lockheed Martin (Space Systems Company)	United States
Application of singular perturbation theory to space flight dynamics problems	10	confirmed	Prof. Giulio Avanzini	Università del Salento	Italy
dynamics in the vicinity of the stable halo orbits	10	confirmed	Mr. David Lujan	University of Colorado Boulder	United States
A variant of the Kármán line theory facilitating the identification of a precise altitude boundary	10	confirmed	Mr. Nicolas Bérend	ONERA - The French Aerospace Lab	France
A Survey of Longitudinal-Shift Maneuvers Performed by Geosynchronous (GEO) Satellites from 2010 to 2021	10	confirmed	Mr. Thomas G. Roberts	Massachusetts Institute of Technology (MIT)	United States
Automatic multi-gravity assist trajectory design with modified Tisserand Graphs exploration	10	confirmed	Mr. Hadrien AFSA	Cranfield University	France
design for earth-mars cycler trajectories based on aero assisted orbital transfer	10	confirmed	Mr. Shijie Sun	Science and Technology on Space Physics Laboratory	China
On the approximation of gravitational field of a dynamically symmetric rigid body by two balls	10	confirmed	Prof. Alexander Burov	A.A.Dorodnicyn Computing Centre, FRC Computer Science and Control, Russian Academy of Sciences & Higner School of Economics	Russian Federation
Novel Gear based Actuation Mechanism for Spacecraft’s Attitude Control	10	confirmed	Mr. Priyank Dubey	Indian Institute of Technology	India
Optimal Control of J2 formations subject to drag using MPC	10	confirmed	Mr. Karthick Dharmarajan	University of Rome “La Sapienza”	Italy
machine learning based orbit prediction	10	confirmed	Mr. Filipe Senra	University of Beira Interior	Portugal
ienai GO: a free tool for concurrent mission design and optimization with on-board electric propulsion	10	confirmed	Mr. Francisco de Borja De Saavedra	IENAI SPACE	Spain
TudatPy - a versatile open-source astrodynamics software package for space education	10	confirmed	Mr. Filippo Oggionni		Italy
Modelling and simulation of an on-orbit experiment for testing a novel engine technology	10	confirmed	Ms. Martina Rusconi	Politecnico di Milano	Italy
Optimization of chaser trajectory for active debris removal missions	10	confirmed	Prof. Giulio Avanzini	Università del Salento	Italy
Escape Trajectories from Earth-Moon and Sun-Earth Quasi Periodic Orbits with Electric Propulsion	10	withdrawn	Mr. Luigi Mascolo	Politecnico di Torino	Italy
On optimal three-impulse Earth-Moon transfers in a four-body model	10	confirmed	Ms. Shanshan Pan	Nanjing University	China
Three DoF Testbed for CubeSat ADCS Verification and test	10	withdrawn	Mr. Amir Hosein Bahrami	Amirkabir University of Technology	Iran
study of orbital mechanics parameter using Laplace transform.	10	confirmed	Mr. Bhavesh Dadhich	University of Southern California	United States
Online Learning & Optimization for Autonomous Space Servicing Missions	10	withdrawn	Dr. Omer Burak Iskender	Nanyang Technological University	Singapore, Republic of
Design and Implementation of an FPGA based Control Moment Gyro controller	10	withdrawn	Mrs. Aswathy Krishnan	Indian Space Research Organization (ISRO)	India
Processing of Altimetric Data for Precise Orbit Determination	10	confirmed	Mr. Edoardo Del Vecchio	Sapienza University of Rome	Italy
Real-time Optimal Control of a 6-DOF State-Constrained Close-Proximity Rendezvous Mission	10	confirmed	Mr. Akan Selim	ROKETSAN Roket Sanayi ve Ticaret A.S.	Türkiye
A survey of the Magnetic Dipole Moment Determination Methods applied on CubeSats and Nanosatellites	10	confirmed	Dr. Abdelmadjid Lassakeur	Agence Spatiale Algérienne (ASAL)	Algeria
Singularity-Free Hybrid Control for Autonomous Berthing of Two Spacecrafts	10	confirmed	Ms. Tanya Krishna Kumar	Indian Institute of Technology Kanpur	India
Initial Guesses for Cislunar Low-Thrust Transfers	10	confirmed	Mr. Markus Grass	Institute of Space Systems, University of Stuttgart	Germany
Stabilization of Space-advertisement Satellite Formation	10	confirmed	Mr. Kenta Nakajima	Kyushu University	Japan
Application of Reflective Control Devices for Position and Attitude Control of Spacecraft	10	withdrawn	Mr. Alejandro Cabrales Hernandez	Massachusetts Institute of Technology (MIT)	United States
Low-cost Manufacturing and Testing of Attitude Control Systems for CubeSats	10	confirmed	Mr. Charles Lee	UBC Orbit	Canada
optimal launch windows for artemis III and beyond leveraging contour maps	10	confirmed	Dr. Rohan Sood	The University of Alabama	United States
Hybrid Multi-Algorithmic Attitude Determination and Control Architecture	10	confirmed	Ms. Cansu Yildirim	Middle East Technical University	Türkiye
Families of Displaced non-Keplerian Polar Orbits for Space-Based Solar Energy Applications	10	confirmed	Dr. Onur Çelik	University of Glasgow	United Kingdom
Grid search for spatial axi-symmetric horseshoe orbits in restricted three body problem	10	confirmed	Mr. Saleem Yousuf	Central University of Rajasthan	India
Mapping long-term natural orbits about Titania, a satellite of Uranus	10	confirmed	Prof.Dr. Silvia Maria Giuliatti Winter	UNESP - Univ Estadual Paulista	Brazil
Development of a Control Moment Gyro Controller for spacecrafts	10	withdrawn	Mrs. Aswathy Krishnan	Indian Space Research Organization (ISRO)	India
Closed-Loop Minimum-Jerk Explicit Guidance for Powered Descent Phase of Soft landing on Mars Accounting for surface wind	10	withdrawn	Dr. Parvathi S P	Indian Institute of Science	India
Data-Driven Guidance for Asteroid Landing Based on Real-Time Dynamic Mode Decomposition	10	confirmed	Mr. Taiga Kajikawa	Kyushu University	Japan
The thrust vector control optimization of the air-breathing electric propulsion to maintain spacecraft in ultra-low orbits	10	confirmed	Dr. Egor Loktionov	Bauman Moscow State Technical University	Russian Federation
Optimization of impulsive low-energy trajectories to the Earth-Moon L2 halo orbit	10	confirmed	Mr. Rui Zhou	Moscow Aviation Institute (National Research Institute, MAI)	Russian Federation
physical cross-sectional area modeling of complex structural spacecraft for long-term precision orbit determination	10	confirmed	Dr. Yang Cheng		China
Optimal Trade-Off between Solar Energy and Control Input while Rendezvous and Docking of a CubeSat with a Rotating Target Spacecraft	10	confirmed	Mr. Priyank Dubey	Indian Institute of Technology	India
A Framework for Deriving and Validating the Multibody Equations of Motion of Micro-Launchers	10	confirmed	Mr. Victor Covasan	International Space University (ISU)	Portugal
Bald Eagle Search Optimization based Bioinspired Spacecraft Rendezvous- Docking and Space Debris Mitigation	10	confirmed	Mr. Arya Das	Indian Institute of Technology Kanpur	India
A Transport Theorem for the Inertia Tensor for Simplified Spacecraft Dynamics Development	10	confirmed	Dr. Jordan Maxwell		United States
N-Body Problem in Non-Inertial Reference Frame. Application to Full Two-Body Stability Problem	10	confirmed	Prof. Daniel Condurache	Technical University of Iasi	Romania
Accessible and Retrievable Asteroids considering Lunar and Solar Gravity Assists	10	confirmed	Dr. Hongru Chen	Kyushu University	Japan

session IP

Paper title

Mode

Presentation status

Speaker

Affiliation

Country