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  • C1
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  • 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