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  • session 2

    Title

    Space Structures II Development and Verification (Orbital deployable and dimensionally stable structures, including mechanical and robotic systems and subsystems)

    Description

    The topics to be addressed within this session concern all aspects of deployable and dimensionally stable structures e.g. reflectors, telescopes, antennas etc. It includes structural design, analysis and verification, shape control and thermal distortion as well as evaluation of analysis versus test results, of both on-ground and in-orbit testing. Furthermore, related mechanical, thermal and robotic systems and subsystems/mechanisms will be covered.

    Date

    2024-10-15

    Time

    10:15

    Room

    Orange Hall 1

    IPC members
    • Co-Chair: Prof. Paolo Gasbarri, University of Rome “La Sapienza”, Italy;

    • Co-Chair: Prof. Pavel Trivailo, RMIT University (Royal Melbourne Institute of Technology), Australia;

    • Rapporteur: Prof. Jiawen Qiu, China;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    design and optimize of soft robotic manipulator based on cable-driven bellows structure

    12

    confirmed

    Mr. Rui Lin

    Beihang University (BUAA)

    China

    2

    10:27

    A multi-objective optimization approach to design bistable collapsible tubular mast

    12

    confirmed

    Ms. Flavia Palmeri

    Sapienza University of Rome

    Italy

    3

    10:39

    Membrane Reflectarray Antenna Design Deployed on Small Satellites Using Composite Booms

    12

    confirmed

    Prof. Hiraku Sakamoto

    Tokyo Institute of Technology

    Japan

    4

    10:51

    Implicit vs explicit nonlinear dynamics for the unfolding of deployable space structures using advanced one-dimensional finite elemets

    12

    confirmed

    Dr. Riccardo Augello

    Politecnico di Torino

    Italy

    5

    11:03

    Dynamic Modeling and Analysis of Deployable Telescope Tubular Mast (TTM) in Spacecraft Systems Using Hybrid Coordinate and Kane's Methods

    12

    confirmed

    Ms. Tongtong Sun

    Northwestern Polytechnical University

    China

    6

    11:15

    Failure onset evaluation of Deployable Rolled-Up Composite Synthetic Aperture Radar (DERAC-SAR) Antenna via global/local approach

    12

    confirmed

    Prof. Alfonso Pagani

    Associazione Italiana di Aeronautica e Astronautica (AIDAA)

    Italy

    7

    11:27

    Actively Controlled Deployable Polymer Reflectors for Small Satellite Applications

    12

    confirmed

    Mr. Carl Johan Nielsen

    Université Libre de Bruxelles

    Belgium

    8

    11:39

    Deployment and Reachability Analysis of Tendon-actuated Structural Modules for an In-Space Assembled Segmented Reflector

    12

    confirmed

    Mr. Nate Osikowicz

    Pennsylvania State University

    United States

    9

    11:51

    A comprehensive error analysis of high-precision docking process for micro satellite

    12

    confirmed

    Mr. Bo Zhang

    Shanghai Engineering Center for Microsatellite

    China

    10

    12:03

    Deployment Mechanism Design for Atmospheric Reentry Protection Systems

    12

    confirmed

    Mr. Pedro Alves

    University of Brasilia

    Brazil

    11

    12:15

    New Configuration Optimization Algorithm for Reconfiguration Space Manipulator Based on Generalized Flexibility Index

    10

    confirmed

    Mr. Ying Tian

    Beihang University

    China

    12

    12:25

    Co-design Robots and Structures Framework for Automated Construction of Modular Space Platforms

    12

    confirmed

    Dr. Mathieu Rognant

    Office National d’Etudes et de Recherches Aérospatiales (ONERA)

    France

    13*

    12:37

    A deployable and retractable inflatable link for a space robotic manipulator

    12

    confirmed

    Dr. Pierpaolo Palmieri

    Politecnico di Torino

    Italy

    14*

    12:37

    Feasibility Evaluation of the Scissor Petal Reflector Concept

    12

    confirmed

    Mr. Hiroaki Matsubara

    National Defense Academy of Japan

    Japan

    15*

    12:37

    Deployable Origami-inspired Structures for Future Space Applications: Lessons Learned from Zero-G Flight Experiment and New Developments

    12

    confirmed

    Mr. Augustin Gallois

    ISAE - Institut Supérieur de l'Aéronautique et de l'Espace

    France