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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

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:15

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

    15'

    confirmed

    Prof. Robert G. Melton

    The Pennsylvania State University

    United States

    2

    15:30

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

    15'

    confirmed

    Ms. Yan Wei

    Beihang University

    China

    3

    15:45

    Passive aerostability for drag sails

    15'

    confirmed

    Mr. Andrew Wolahan

    Cranfield University

    The Netherlands

    4

    16:00

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

    15'

    confirmed

    Mr. Bryan Johnston-Lemke

    Space Flight Laboratory, University of Toronto

    Canada

    5

    16:15

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

    15'

    Prof. Jay Kang

    Korea Aerospace University

    Korea, Republic of

    6

    16:30

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

    15'

    confirmed

    Prof. Anna Guerman

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

    Portugal

    7

    16:45

    Hybrid Position/Force Control of Large Space manipulators

    15'

    confirmed

    Dr. Dongming Ge

    China Academy of Space Technology (CAST)

    China

    8

    17:00

    Design of spherical solar sails for spacecraft attitude maneuvers

    15'

    confirmed

    Mr. Fedorenko Alexey

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

    Russian Federation

    9

    17:15

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

    15'

    confirmed

    Prof. Fabio Santoni

    University of Rome “La Sapienza”

    Italy

    10

    17:30

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

    15'

    confirmed

    Mr. Ahmad Salahuddin Mohd Harithuddin

    RMIT University (Royal Melbourne Institute of Technology)

    Australia

    11

    17:45

    finite-time continuous sliding mode magneto coulombic attitude control

    15'

    confirmed

    Dr. Manoranjan Sinha

    IIIT Kharagpur

    India

    12

    18:00

    A Nadir-Pointing Magnetic Attitude Control System for TigriSat nanosatellite

    15'

    confirmed

    Mr. Paride Testani

    Scuola Ingegneria Aerospaziale

    Italy

    13

    18:15

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

    15'

    confirmed

    Prof. Igor V. Belokonov

    Russian Federation