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  • D1
  • IP
  • session IP

    Title

    Interactive Presentations

    Date

    2015-10-14

    Time

    13:15

    IPC members
    • Coordinator: Dr. Reinhold Bertrand, European Space Agency (ESA), Germany;

    • Coordinator: Ms. Jill Prince, National Aeronautics and Space Administration (NASA), United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Coloring the future - an innovative approach for dealing with "doomsday" NEOs

    withdrawn

    Mr. Meidad Pariente

    SPACECIALIST, Effective Space Solutions

    Israel

    2

    Platform Robustness for Unknown Space Missions

    withdrawn

    Dr. Otavio Luiz Bogossian

    Brazilian National Institute for Space Research - INPE

    Brazil

    3

    Integrated Control/Structure Design Method for Future Large Flexible Spacecraft

    withdrawn

    Mr. Jose Alvaro PEREZ GONZALEZ

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

    France

    4

    Research on the Concept, Mechanism and Modeling of Space Soft Capture Technique in the Area of On-orbit Servicing

    confirmed

    Dr. Fan Yang

    Academy of Equipment

    China

    5

    adaptive fault tolerant servo scheme for launch vehicle control actuation system

    withdrawn

    Mr. Baby Sebastian

    Indian Space Research Organization (ISRO)

    India

    6

    indirect adaptive fuzzy H-infinite control of the free-floating space robot system with flexible joints

    withdrawn

    Ms. Lijiao Zhang

    Fuzhou University

    China

    7

    Decentralized Adaptive Neural Network Stabilization Control and Vibration Suppression of Flexible Robot Manipulator during Capture a Target

    withdrawn

    Dr. Jing Cheng

    Fuzhou University

    China

    8

    investigation on decontamination design and control system for spacecraft

    confirmed

    Dr. Kouan Hao

    Aerospace System Engineering Shanghai, China

    China

    9

    the methodology of time-efficient estimation of flying vehicle’s characteristics at the stage of draft design using the multi-disciplinary software

    confirmed

    Mr. Dmitriy Grishko

    Bauman Moscow State Technical University

    Russian Federation

    10

    A multiform data syncretized display system based on Virtools

    Dr. Jingqi Cai

    China Academy of Launch Vehicle Technology(CALT)

    China

    11

    REACTIONLESS WORKSPACE OF A MULTI-DEGREES-OF-FREEDOM SPACE MANIPULATOR

    confirmed

    Dr. Silvio Cocuzza

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

    Italy

    12

    SPACE MANIPULATOR DESIGN FOR A HIGH PERFORMANCE REACTION CONTROL

    Dr. Silvio Cocuzza

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

    Italy

    13

    analysis and comparison of different formal methods on the static behavior for fault-tolerant systems

    withdrawn

    Mr. Zheng WANG

    Zhejiang University

    China

    14

    Fragility Index as a Technical Performance Measure (TPM) during a System Life Cycle: A Case Study on its Application to Monolithic and Fractionated Spacecraft.

    withdrawn

    Mr. Antonio Pugliese

    Stevens Institute of Technology

    United States

    15

    Vision-based lunar virtual surface generation using Shape-from-shading method

    confirmed

    Ms. Yun-young Kim

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    16

    A proposal for updating the Brazilian Data Collecting System

    confirmed

    Prof. Geilson Loureiro

    Instituto Nacional de Pesquisas Espaciais (INPE)

    Brazil

    17

    A Systems Engineering approach for accommodating disruptive space technologies

    withdrawn

    Mr. Tiago Henrique Matos de Carvalho

    Cranfield University

    United Kingdom

    18

    Decoupling gross motion and vibration of free-floating space robots in frequency and time domain

    Mr. Teng Zhang

    College of Astronautics, Northwestern Polytechnical University

    China

    19

    Mission Design “Satellite LIBERTAD 2”

    confirmed

    Dr. Jorge Soliz

    Sergio Arboleda University

    Colombia

    20

    Optimum Open-Loop Actuator Design of High Stability Pointing Mechanisms for High Precision Remote Sensing Satellites

    confirmed

    Dr. Rui Li

    Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)

    China

    21

    A Reliable Multicore Processor Design for Space Applications

    confirmed

    Mr. Cao Hui

    Xi'an Microelectronics Technology Institute

    China

    22

    Platform Robustness for Unknown Space Missions

    withdrawn

    Dr. Otavio Luiz Bogossian

    Brazilian National Institute for Space Research - INPE

    Brazil