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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

    2019-10-24

    Time

    13:15

    Room

    IP Area

    IPC members
    • Co-Chair: Prof. Anna Guerman, Centre for Mechanical and Aerospace Science and Technologies (C-MAST), Portugal;

    • Co-Chair: Prof. Daniel Scheeres, Colorado Center for Astrodynamics Research, University of Colorado, United States;

    papers

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    Precise power descent control of single gimballed thruster moon Lander.

    confirmed

    Mr. Rolando Cortés

    CINVESTAV

    Mexico

    capability analysis for manipulator-actuated integrated translational and rotational control strategy of spacecraft

    withdrawn

    Dr. Feng Zhang

    China Academy of Launch Vehicle Technology(CALT)

    China

    multiple entry trajectory scenarios for returning from the moon: advantages and disadvantages

    confirmed

    Dr. Dmitriy Grishko

    Bauman Moscow State Technical University

    Russian Federation

    Reinforcement Learning for Spacecraft Attitude Control

    confirmed

    Mr. FNU Vedant

    University of Illinois

    United States

    The High Performance Satellite Dynamics Simulator (HPS): A Modular MATLAB/Simulink-Based Simulation Library for GNC Systems Development

    confirmed

    Mr. René Schwarz

    German Aerospace Center (DLR)

    Germany

    Investigating Un-Stability Phenomena and Chaotic Behavior in Deflection of Potential Hazardous Asteroid

    withdrawn

    Mr. Javad Shams

    K. N. Toosi University of Technology

    Iran

    ESA F-Class Comet Interceptor: A first close-up study of a dynamically “new” object

    confirmed

    Dr. Joan Pau Sanchez Cuartielles

    Cranfield University

    United Kingdom

    Research on the dynamic liquid equilibrium position and the composite equivalent mechanical model of large-amplitude liquid sloshing

    withdrawn

    Dr. Nan Miao

    Zhengzhou University of Aeronautics

    China

    Building Inclinated and Excentric High Earth Orbits Through Small Perturbations: A Four-body Dynamics Exploration

    withdrawn

    Prof. Elbert E.N. Macau

    Instituto Nacional de Pesquisas Espaciais (INPE)

    Brazil

    CMOS Based High Accuracy Miniaturized Digital Sun Sensor with Optimized Error Compensation on SONATE

    confirmed

    Mr. Tom Baumann

    University of Würzburg

    Germany

    Hayabusa2 operational design and evaluation of MINERVAII-1A/B rovers deployment

    confirmed

    Mr. Kent Yoshikawa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    Vibration suppression during capture of a spinning satellite using input shaping method based on NTSM control

    no-show

    Mr. Wenzheng Zhang

    Shanghai Institute of Spaceflight Control Technology

    China

    Rendezvous with Spinning Target in Elliptical Orbit by Model Predictive Control

    confirmed

    Prof. Zheng Hong Zhu

    York University

    Canada

    Modeling and Simulation of Post-Impact Dynamics Intended for Real-Time Implementation on Spacecraft Robotic Servicing and Assembly Missions

    confirmed

    Mr. Anthony Wolosik

    Naval Research Laboratory

    United States

    Qualitative and quantitative characterisation of solutions for the low thrust transfer GTO to GEO

    confirmed

    Mr. Juan Carlos Bastante

    OHB System AG-Bremen

    Germany

    Development of a Hardware-In-the-Loop attitude control simulator for EIRSAT-1, a magnetically actuated 2U CubeSat

    confirmed

    Mr. Joseph Thompson

    Student

    Ireland

    neuroevolutionary hebbian-learning for interplanetary trajectory design

    withdrawn

    Mr. Abishek Navukkarasan

    AgniKul Cosmos

    India

    Developing Robust Rendezvous and Proximity Operations Control using Generative-Adversarial Machine Learning

    withdrawn

    Dr. Lorraine Weis

    L-3 Communications

    United States

    The lifetime of dust particles in the Pluto system

    confirmed

    Prof.Dr. Silvia Maria Giuliatti Winter

    UNESP - Univ Estadual Paulista

    Brazil