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  • session IP

    Title

    Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUM

    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

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Advanced attitude determination and control testing in a modular solution

    10

    confirmed

    Mr. Riccardo Spartà

    Politecnico di Torino

    Italy

    2

    A Novel Approach for Autonomous Spacecraft Recovery to Sun Pointing Orientation

    10

    confirmed

    Mrs. KanuPriya Govila

    Indian Space Research Organization (ISRO)

    India

    3

    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

    4

    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

    5

    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

    6

    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

    7

    Applying Fictitious Reference Iterative Tuning to Quaternion Feedback and Quantitative Evaluation

    10

    confirmed

    Mr. Ozeki Yusaku

    Tokyo Institute of Technology

    Japan

    8

    In-Orbit Allan Variance for Gyroscope Noise Characterization in Earth Observation Satellites

    10

    confirmed

    Mr. Tomás Ignacio Burroni

    Satellogic

    Spain

    9

    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

    10

    Spacecraft dynamic window attitude planning method for planetary approach detection

    10

    confirmed

    Mr. CongCong Luo

    Beijing Institude of technology

    China

    11

    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

    12

    Ionospheric Plasma Drag on Small Satellites in Low-Earth Orbit

    10

    confirmed

    Dr. Simone Di Fede

    Nanyang Technological University

    Singapore, Republic of

    13

    Long-term orbital dynamics surrounding an eccentric binary asteroid system by triple averaging

    10

    confirmed

    Mr. Yongjie Chen

    School of Astronautics, Beihang University

    China

    14

    On the refinement of low-energy Earth–Moon transfer families into an ephemeris model

    10

    confirmed

    Mr. Claudio Toquinho Campana

    Politecnico di Milano

    Italy

    15

    Orbit determination for X-ray pulsar navigation with the aid of artificial neural networks

    10

    confirmed

    Ms. Sui Chen

    Politecnico di Milano

    Italy

    16

    Restricted Four Body Problem Chaotic Analysis of Phase Space Structures for Natural Multi-Moon Transfers

    10

    withdrawn

    Mr. Suryansh Aryan

    Virginia Tech

    United States

    17

    Safe Short-Term Loitering in Gateway's Near Rectilinear Halo Orbit

    10

    confirmed

    Mr. Matthew Bolliger

    Advanced Space

    United States

    18

    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

    19

    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

    20

    Long-term evolution of orbits in cislunar space: characterisation and stability analysis

    10

    confirmed

    Ms. Mathilda Bolis

    Politecnico di Milano

    Italy

    21

    Numerical Continuation and Stationkeeping of Quasi-Periodic Quasi-Satellite Orbits around Phobos

    10

    confirmed

    Dr. Xiaoyu Fu

    University of Liverpool

    United Kingdom

    22

    Transfer to asteroids during close encounter using finite-time Lyapunov exponent fields

    10

    confirmed

    Mr. Tianji Chen

    Beihang University

    China

    23

    An Orbital Game Control Algorithm for On-Board Application by Behaviour Cloning

    10

    withdrawn

    Dr. Simeng Huang

    Tsinghua University

    China

    24

    Automated Computation of Optimal Spiral Trajectories in the Circular Restricted Three-Body Problem

    10

    confirmed

    Mr. Grant Hecht

    University at Buffalo

    United States

    25

    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

    26

    Global Trajectory Optimization with Alphazero: A Novel Approach Applied to the GTOC 11 Challenge

    10

    confirmed

    Mr. Andrea Forestieri

    Politecnico di Torino

    Italy

    27

    Impulsive station-keeping of frozen orbits around planetary moons using manifolds of averaged dynamics

    10

    confirmed

    Mr. Yongjie Chen

    School of Astronautics, Beihang University

    China

    28

    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

    29

    Optimal low-thrust trajectory approximation via singular perturbation theory

    10

    confirmed

    Mr. Danilo Zona

    Università del Salento

    Italy

    30

    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

    31

    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

    32

    Systematic Analysis of Cislunar Escape Opportunities for Exploration and Planetary Defence Missions

    10

    confirmed

    Dr. Andrea Pasquale

    Deimos Space SLU

    Germany

    33

    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

    34

    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

    35

    Advances in Koopman Operator Methods for Astrodynamics Applications

    10

    confirmed

    Mr. Oluwatosin Kolade

    Obafemi Awolowo University

    Nigeria

    36

    AI-Enhanced Visualization and Control of Swarm Satellites Utilizing Geomagnetic Actuators

    10

    confirmed

    Ms. Tanya Krishna Kumar

    Indian Institute of Technology Kanpur

    India

    37

    Characterization of Orbits in Cislunar Space for Space Traffic Management

    10

    confirmed

    Mr. Sourav Ghosh

    Space Generation Advisory Council (SGAC)

    India

    38

    Drag Coupling of Attitude and Orbital Dynamics for LEO Satellites.

    10

    confirmed

    Mr. Thomas McIlwraith

    University of Strathclyde

    United Kingdom

    39

    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

    40

    Lunar Constellation Deployment Techniques Leveraging Natural Perturbations

    10

    confirmed

    Dr. Lorenzo Bucci

    Deimos Space SLU

    Germany

    41

    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

    42

    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

    43

    A Polynomial-Based Differential Dynamic Programming Optimisation Method for Space Trajectory Design

    10

    confirmed

    Mr. Thomas Caleb

    ISAE-Supaero University of Toulouse

    France

    44

    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

    45

    General Approach to Solve Low-Thrust Multi-Target Space Logistics Problems

    10

    confirmed

    Mr. Riccardo Apa

    Politecnico di Torino

    Italy

    46

    Inspection of Space Rider with a 12U CubeSat: Ensuring Safety and Efficiency

    10

    confirmed

    Mr. Luca Bartolucci

    Politecnico di Torino

    Italy

    47

    Mission Feasibility for Interstellar Object Exploration through Utilization of Advanced Propulsion Technologies

    10

    confirmed

    Prof. Jekanthan Thangavelautham

    University of Arizona

    United States

    48

    Multi-target space mission sequence optimization with deep reinforcement learning

    10

    confirmed

    Mr. Edward Tomanek-Volynets

    University of Glasgow

    United Kingdom

    49

    Rassvet-1 Tech Demo Mission for Broadband Internet Constellation: On-Orbit Results and Lessons Learned

    10

    confirmed

    Ms. Irina Ponomareva

    Russian Federation

    50

    Attitude-trajectory coupling adaptive control for flexible landing on small celestial body

    10

    confirmed

    Ms. Bingjie Lu

    Beijing Institude of technology

    China

    51

    Onboard Perception-based Autonomous Visual Navigation around Small Celestial Bodies

    10

    confirmed

    Dr. Avijit Banerjee

    Luleå University of Technology

    Sweden

    52

    Performance Assessment of Crater-Based Navigation for Autonomous Moon Landing

    10

    withdrawn

    Mr. Jean-Francois Hamel

    NGC Aerospace Ltd.

    Canada

    53

    Feasibility Study of an All-Electric Rendezvous Mission in GEO Orbit

    10

    confirmed

    Mrs. Damiana Losa

    Thales Alenia Space

    France

    54

    CNN-based Visual Navigation: Optimization Strategies for Monocular Pose Estimation in Proximity Operations

    10

    confirmed

    Mrs. Lucrezia Lovaglio

    Politecnico di Torino

    Italy

    55

    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

    56

    Optimization-based actuator management for hybrid control allocation

    10

    confirmed

    Mr. Jesús Ramírez

    SENER Aeroespacial

    Spain

    57

    Approximate Analytical Solution to Spacecraft Optimal Docking Using Koopman Operator Theory

    10

    confirmed

    Mr. Zhan Feng

    School of Astronautics, Beihang University

    China

    58

    Optical and Radio Data Fusion for Spacecraft Navigation and Geophysical Investigations

    10

    confirmed

    Dr. Martina Ciambellini

    Sapienza University of Rome

    Italy

    59

    LSTM-based Fast Predictive Guidance for Autonomous Safe Docking with Path and Control Constraints

    10

    confirmed

    Mr. Kumud Darshan Yadav

    University of Seville

    Spain