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  • IAC-21
  • C2
  • 9
  • session 9

    Title

    Smart Materials and Adaptive Structures

    type

    oral

    Description

    The focus of the session will be on application of smart materials to spacecraft and launch vehicle systems, novel sensor and actuator concepts and new concepts for multi-functional and intelligent structural systems. Also included in the session will be new control methods for vibration suppression and shape control using adaptive structures as well as comparisons of predicted performance with data from ground and in-orbit testing.

    Date

    2021-10-29

    Time

    13:30

    Room

    Rais Al Khaimah

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

    • Co-Chair: Dr. Hiroshi Furuya, Japan;

    • Rapporteur: Prof. Paolo Gaudenzi, Sapienza University of Rome, Italy;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    2

    13:30

    Numerical modelling and experiments of a vibration suppression solution via Offset Piezoelectric Stack Actuators for space structures

    10

    confirmed

    Dr. Federica Angeletti

    University of Rome “La Sapienza”

    Italy

    4

    13:40

    Utilization of shape memory alloys for multi-purpose deployable solar panels

    10

    confirmed

    Mr. Kaushik Aryan

    R V College of Engineering, Bengaluru

    India

    6

    13:50

    Passive Vibration Suppression of Solar Array by Using Hyperelastic Shape Memory Alloy

    10

    confirmed

    Mr. Yeon Hyeok Park

    Chosun University

    Korea, Republic of

    1001

    14:00

    Battery-Less Soft Sensor of Spacecraft Vibration with Advanced Piezoelectric Energy Harvester

    10

    confirmed

    Mr. Yushin HARA

    Tohoku University

    Japan

    1003

    14:10

    environmental analysis and optimisation of an in-orbit shape memory alloy deployment mechanism

    10

    confirmed

    Mr. Chris Wright

    University of the West of England (UWE)

    United Kingdom

    1005

    14:20

    Computational Aerothermoelastic Analysis of a Human Crew Entry Vehicle in Earth-Mars atmospheres

    10

    withdrawn

    Mr. Rohan Chandra

    University of Petroleum and Energy Studies

    India

    1007

    14:30

    Passive Self-Healing Dielectric Elastomer Sensors for Structural Health Monitoring of Inflatable Space Structures

    10

    withdrawn

    Mr. Scott Bender

    Embry-Riddle Aeronautical University

    United States

    1008

    14:40

    Design and analysis of a shape-changing dual-bell rocket nozzle.

    10

    withdrawn

    Ms. Khanak Saxena

    SRM Institute of Science and Technology

    India

    1009

    14:50

    Smart Manufacturing in the space industry. A Cyber-Physical System architecture and its implementation to a MAIT process for mega constellations of satellites

    10

    confirmed

    Prof. Paolo Gaudenzi

    Sapienza University of Rome

    Italy

    1010

    15:00

    model predictive control for switching vibration suppression using future trajectory

    10

    confirmed

    Prof. Kanjuro MAKIHARA

    Tohoku University

    Japan

    1011

    15:10

    Development of a novel wire-woven tire for exploration rover using superelastic shape memory alloy wires

    10

    withdrawn

    Dr. Tiegang Chen

    Beihang University (BUAA)

    China

    1012

    15:20

    A novel space bearings unloading mechanism using screw pairs and shape memory alloys

    10

    withdrawn

    Dr. Zhang Yuhang

    Beihang University (BUAA)

    China