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  • C2
  • 4
  • session 4

    Title

    Space Structures Control, Dynamics and Microdynamics

    Description

    The topics to be addressed include dynamics analysis and testing, modal identification, landing and impact dynamics, pyro-shock, test facilities, vibration suppression techniques, damping, micro-dynamics, in-orbit dynamic environment, wave structural propagation, excitation sources and in-orbit dynamic testing. Attention will be paid to dynamics modelling and control of robotic and mechatronic systems (e.g. manipulators for the servicing and/or assembly of space structures, pointing mechanisms, etc).

    Date

    2024-10-16

    Time

    10:15

    Room

    Orange Hall 1

    IPC members
    • Co-Chair: Dr. Federica Angeletti, University of Rome “La Sapienza”, Italy;

    • Co-Chair: Dr. Élcio Jeronimo de Oliveira, Associazione Italiana di Aeronautica e Astronautica (AIDAA), Brazil;

    • Rapporteur: Prof. Harijono Djojodihardjo, Bandung Institut of Tecnology, Indonesia;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Space Circuitry Tunable Mass Damper design parameters sensitivity analysis

    10

    confirmed

    Mr. MANUELE LAURENZI

    University of L'Aquila

    Italy

    2

    10:25

    On the Impact of Gravity During the Micro-Vibration Characterization of Reaction-Wheels: An Experimental Assessment

    10

    confirmed

    Mr. Matias Bestard Körner

    German Aerospace Center (DLR)

    Germany

    3

    10:35

    Multibody simulations and impact tests of a docking system for small satellites

    10

    confirmed

    Ms. Martina Imperatrice

    CISAS – “G. Colombo” Center of Studies and Activities for Space

    Italy

    4

    10:45

    Design and analysis of multiple competing "Inertial Morphing" control schemes for autonomous spinning spacecraft, enabling attitude acrobatics with aimed agility

    10

    confirmed

    Prof. Pavel M. Trivailo

    RMIT University, Australia

    Australia

    5

    10:55

    modeling and control of an earth observation satellite equipped with a spinning flexible antenna

    10

    confirmed

    Mr. David Paolo Madonna

    Sapienza University of Rome

    Italy

    6

    11:05

    Machine Learning for Path Planning of Space Robots RVD/B orbital Operations

    10

    confirmed

    Prof. Ijar Da Fonseca

    ITA-DCTA

    Brazil

    7

    11:15

    MetOp-SG MicroWave Imager instrument Microvibration Campaign

    10

    Mr. Claudio Maini

    OHB Italia SpA

    Italy

    8

    11:25

    Simulation and experimental investigation of CALLISTO's landing leg deployment dynamics

    10

    confirmed

    Mr. Anton Schneider

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    9

    11:35

    Design, validation and production of small-size rover elastic wheels: a solution to plastic deformations

    10

    confirmed

    Mr. Mattia Trentini

    Politecnico di Torino

    Italy

    10

    11:45

    Nash Equilibrium-Based Vibration Control for Large Flexible Space Structures Using Distributed Control Moment Gyroscopes

    10

    confirmed

    Mr. TingXiang Zhang

    Beijing Institute of Technology

    China

    11

    11:55

    Using genetic algorithm to characterize dynamic joint parameters of SSRMS

    10

    confirmed

    Ms. Sarah Halabieh

    MDA

    Canada

    12

    12:05

    Characterization of a Novel Micro-Vibration Mitigation Developed for An Experimental Life Sciences Cube Used at the International Space Station

    10

    confirmed

    Mr. Saban Otenkaya

    TUBITAK Uzay, Space Technologies Research Institute

    Türkiye

    *

    Contact and impact dynamics between a space flexible net and an inflatable boom

    10

    confirmed

    Prof. Chao Xu

    Northwestern Polytechnical University

    China

    *

    Investigating shock propagation through composite structures

    10

    confirmed

    Ms. Ada Ranieri

    Politecnico di Bari

    Italy

    *

    Proposal of an assemblable Geostationary megastructure for payload hosting

    10

    withdrawn

    Mr. Hemanth Alapati

    ISAE-Superaero University of Toulouse

    France

    *

    Structural Dynamics of Super Large Plate-Like Gyroelastic Spacecraft with Concentrated Mass Modeling

    10

    confirmed

    Mr. Jingyu Guo

    Harbin Institute of Technology

    China