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  • IAC-23
  • C1
  • IP
  • 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.

    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

    Dynamic analysis of mechanical motion of a variable-mass rocket system

    10

    confirmed

    Prof.Dr. Valeh Bakhshali

    Azerbaijan Technical University

    Azerbaijan

    Dynamic modelling and drag-free control system design for the space-borne gravitational wave detector in the port-Hamiltonian framework

    10

    withdrawn

    Mr. Haojun Ma

    National Space Science Center, Chinese Academy of Sciences;University of Chinese Academy of Sciences

    China

    Desensitized Ensemble Guidance

    10

    confirmed

    Prof. Ismail Bayezit

    Istanbul Technical University

    Türkiye

    Machine Learning Based Guidance for Optimal Spacecraft De-Orbiting

    10

    confirmed

    Ms. Emanuela Gaglio

    Scuola Superiore Meridionale

    Italy

    optimization of low-energy trajectories to the Earth-Moon L2 halo orbit with finite thrust via parameter continuation method

    10

    withdrawn

    Mr. Rui Zhou

    Moscow Aviation Institute (National Research University, MAI)

    Russian Federation

    Comparison of Non-Linear Heuristic Control and Linear Time-Varying Optimal Control Design for 3-axes Attitude Control of a Microsatellite

    10

    confirmed

    Ms. Neha Chohan

    ReOrbit

    Finland

    Closed-loop guidance for interplanetary CubeSats with indirect methods

    10

    confirmed

    Mrs. Alessandra Mannocchi

    Politecnico di Milano

    Italy

    Robust low-thrust gravity-assist trajectory optimization

    10

    confirmed

    Mr. Jin Cheng Hu

    Nanjing University of Aeronautics and Astronautics

    China

    Optimal Tuning of the Nanosatellite Attitude Controller Using TRIAD-Aided Kalman Filter and Particle Swarm Optimization

    10

    confirmed

    Prof.Dr. Chingiz Hajiyev

    Istanbul Technical University

    Türkiye

    THE EXTENDED WAHBA’S PROBLEM IN DUAL AND MULTIDUAL QUATERNIONS

    10

    confirmed

    Prof. Daniel Condurache

    Technical University of Iasi

    Romania

    Approximation for gravitational field of a small celestial body by a triple of uniform balls

    10

    confirmed

    Prof. Anna Guerman

    Centre for Mechanical and Aerospace Science and Technologies (C-MAST)

    Portugal

    Multiple Fly-By Low Thrust Trajectory Design Using Finite Fourier Series Shape-Based Approach

    10

    withdrawn

    Ms. Dhanisha Sateesh

    Space Generation Advisory Council (SGAC)

    India

    Trajectory Planning and Execution in a Hyper Redundant Continuum Manipulator for Satellite Docking

    10

    confirmed

    Mr. Ayush Ranjan

    Indian Institute of Technology Kanpur

    India

    Optimal control of the thrust vector of a spacecraft with an air-breathing electric propulsion

    10

    confirmed

    Prof. Alexander S. Filatyev

    Lomonosov Moscow State University

    Russian Federation

    Fuel-Minimum Fuel-Average Control Algorithm for Large Constellation Configuration Maintenance Based on Perturbation Compensation Method

    10

    Dr. Simeng Huang

    China

    Minimum-Propellant Direct, Assisted, and Slingshot Return Trajectories from Mars, Jupiter, and their moons

    10

    confirmed

    Mr. Alessio Patti

    Politecnico di Torino

    Italy

    Attitude determination and control system design for a 3U CubeSat to monitor forward light scattering over Earth horizon

    10

    confirmed

    Mr. Mehmet Esit

    Kyushu Institute of Technology

    Japan

    Overcoming Challenges: Achieving Formation Flying for SIGNIT with Limited Space Situational Awareness and Propulsion Systems

    10

    withdrawn

    Mr. Eric Bertels

    ISIS - Innovative Solutions In Space B.V.

    The Netherlands

    Guidance, Navigation and Control for the autonomous rendezvous and docking of cooperative targets

    10

    withdrawn

    Mr. Alvaro Martinez

    SENER Aeroespacial

    Spain

    Three-body Moon-Mars transfer with revisited weak stability boundary concept and aerobraking capture

    10

    confirmed

    Mr. Gabriele Mocciola

    Politecnico di Torino

    Italy

    Intelligent Integrated Navigation of Solar System Boundary Exploration Cruise Phase Based on Q-Learning Extended Kalman Filter

    10

    confirmed

    Mr. Hui Wang

    School of aeronautics and astronautics, Sun Yat-Sen University Guangzhou

    China

    Robust Attitude Control Using Electrospray Thruster

    10

    Mr. Gianni Pecora

    Politecnico di Torino

    Italy

    Variable-Performance Electrospray Maneuvers Optimization

    10

    Mr. Giuseppe Di Pasquale

    IENAI SPACE

    Spain

    using the dzhanibekov effect to generate angular acceleration for hardware correcting maneuvers

    10

    withdrawn

    Mr. Johannes Ihle

    NTNU

    Norway

    Attitude and orbit control of a geostationary satellite during North-South Station keeping

    10

    withdrawn

    Dr. ELHASSEN BENFRIHA

    Agence Spatiale Algérienne (ASAL)

    Algeria

    Time-delay flight control of small-scale vertical take-off and vertical landing demonstrator using a mini gas turbine engine

    10

    confirmed

    Mr. Minwoo Kim

    Korea Aerospace University

    Korea, Republic of

    Design of transfer trajectories from cislunar orbits to the retrograde Geo-Synchronous Orbit

    10

    confirmed

    Mr. Yuchen He

    Beihang University

    China