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  • session 3

    Title

    Space Structures - Dynamics and Microdynamics

    type

    oral

    Description

    The topics to be addressed include dynamics analysis and testing, modal identification, landing and impact dynamics, pyroshock, test facilities, vibration suppression techniques, damping, micro-dynamics, in-orbit dynamic environment, wave structural propagation, excitation sources and in-orbit dynamic testing.

    Date

    2015-10-13

    Time

    14:45

    Room

    Oranim 1 (ICC, lower level)

    IPC members
    • Co-Chair: Dr. Peter M. Bainum, Howard University, United States;

    • Co-Chair: Prof. Ijar Da Fonseca, ITA-DCTA, Brazil;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Vibration Control Analysis and Genetic Algorithm Optimization of a Piezoelectric Elements bonded Structure Subject to Impact

    12'

    confirmed

    Prof. Harijono Djojodihardjo

    Indonesia

    2

    Innovative viscoelastic damper selection strategy based on DMA and mini-shaker tests for spacecraft applications

    12'

    confirmed

    Mr. Benjamin Kawak

    Surrey Space Centre - University of Surrey

    United Kingdom

    3

    The study of pointing accracy evaluation method for High precise observation satellite

    12'

    confirmed

    Mr. Osamu Takahara

    Mitsubishi Electric Corporation

    Japan

    4

    Development of an efficient analyser for micro-vibration disturbances emanating from spinning actuators

    12'

    no-show

    Ms. Adelia Drego

    Royal Inst. of Technology (KTH)

    Sweden

    5

    Study the influence of wind on the dynamics of angular motion the landing vehicle with an inflatable braking device on the final phase of trajectory

    12'

    confirmed

    Dr. Vsevolod Koryanov

    Bauman Moscow State Technical University

    Russian Federation

    6

    Dynamic Modelling and Control of a Flexible Spacecraft with Fuel Slosh

    12'

    confirmed

    Prof. Paolo Gasbarri

    Università di Roma "La Sapienza"

    Italy

    7

    Attitude Dynamics and Control of a Spacecraft like a Robotic Manipulator when Implementing on-orbit servicing

    12'

    confirmed

    Dr. Ijar M. Da Fonseca

    ITA-DCTA

    Brazil

    8

    Influence analysis of the impacts and frictions of the joints of the vibration isolation platform for control moment gyroscope

    12'

    withdrawn

    Mr. Zixi Guo

    Beijing Institute of technology(BIT)

    China

    9

    DAMPING MEASUREMENT AND DEFORMATION VALIDATION OF FLEXIBLE, HIGH AREA-TO-MASS RATIO DEBRIS MODEL

    12'

    confirmed

    Mr. Sittiporn Channumsin

    School of Engineering, University of Glasgow

    United Kingdom

    10

    Thrust Degradation Effect Research on Non-ideal Configuration of Solar Sail Based on Time-Variant Solar Pressure Model

    12'

    confirmed

    Dr. Chen Yang

    Qian Xuesen Laboratory of Space Technology

    China

    11

    hybrid-trajectory based augmented adaptive control of free-floating flexible space manipulator

    12'

    confirmed

    Dr. xiaoyan yu

    Fuzhou University

    China

    12

    METHODS AND MODELS IN DYNAMICS OF STABILIZATION, ORIENTATION AND NAVIGATION SYSTEMS

    12'

    confirmed

    Prof. Lyudmila Kuzmina

    Kazan National Research Technical University

    Russian Federation

    dynamic singular modeling, robust sliding mode fuzzy control and double elastic vibration active suppression of free-floating flexible-joint and flexible-link space robot with bounded torques

    MERGED 27888

    withdrawn

    Dr. Limin Xie

    Fujian Agriculture and Forestry University

    China