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  • session 1

    Title

    Attitude Dynamics (1)

    Description

    This theme discusses advances in spacecraft attitude dynamics and control, as well as design, testing and performance of attitude sensors and actuators. This theme also covers dynamics and control of multiple interconnected rigid and flexible bodies, including tethered systems, and in-orbit assembly.

    Date

    2013-09-23

    Time

    15:15

    Room

    306A

    IPC members
    • Chairman: Prof. Gianmarco Radice, University of Glasgow, United Kingdom;

    • Chairman: Prof.Dr. Kazuya Yoshida, Tohoku University, Japan;

    • Rapporteur: Dr. Simei Ji, Beijing Institute of Technology, China;

    papers

    Order

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    confirmed

    15'

    Maximum-Likelihood Estimation Optimizer for Constrained, Time-Optimal Satellite Reorientation

    Prof. Robert G. Melton

    The Pennsylvania State University

    United States

    2

    confirmed

    15'

    Drag-Free and Attitude Control for Chinese Planning ASTROD-I Mission

    Ms. Yan Wei

    Beihang University

    China

    3

    confirmed

    15'

    Passive aerostability for drag sails

    Mr. Andrew Wolahan

    Cranfield University

    The Netherlands

    4

    confirmed

    15'

    BRITE-Constellation: On-Orbit Attitude Performance of a Nanosatellite Telescope

    Mr. Bryan Johnston-Lemke

    Space Flight Laboratory, University of Toronto

    Canada

    5

    15'

    Dynamic Decoupling of Slosh Motion in Thrusting Spacecraft with Multiple Large Liquid Stores

    Prof. Jay Kang

    Korea Aerospace University

    Korea, Republic of

    6

    confirmed

    15'

    UNIFORM ROTATIONS OF A TWO-BODY TETHERED SYSTEM IN AN ELLIPTIC ORBIT

    Prof. Anna Guerman

    Centre for Mechanical and Aerospace Science and Technologies (C-MAST)

    Portugal

    7

    confirmed

    15'

    Hybrid Position/Force Control of Large Space manipulators

    Dr. Dongming Ge

    China Academy of Space Technology (CAST)

    China

    8

    confirmed

    15'

    Design of spherical solar sails for spacecraft attitude maneuvers

    Mr. Fedorenko Alexey

    Moscow Institute of Electronics and Mathematics of National Research University Higher School of Economics (MIEM NRU HSE)

    Russian Federation

    9

    confirmed

    15'

    Magnetic Attitude Control of a Two Body System in Drag Balance Instrument Implementation

    Prof. Fabio Santoni

    University of Rome “La Sapienza”

    Italy

    10

    confirmed

    15'

    Discovering Razi acceleration via the theory of derivative kinematics and its application to the dynamic analysis of spacecraft systems

    Mr. Ahmad Salahuddin Mohd Harithuddin

    RMIT University (Royal Melbourne Institute of Technology)

    Australia

    11

    confirmed

    15'

    finite-time continuous sliding mode magneto coulombic attitude control

    Dr. Manoranjan Sinha

    IIIT Kharagpur

    India

    12

    confirmed

    15'

    A Nadir-Pointing Magnetic Attitude Control System for TigriSat nanosatellite

    Mr. Paride Testani

    Scuola Ingegneria Aerospaziale

    Italy

    13

    confirmed

    15'

    Statistical research of the nanosatellite relative motion after separation from the rocket carrier upper stage

    Prof. Igor V. Belokonov

    Russian Federation