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  • session 5

    Title

    Attitude Dynamics (1)

    type

    oral

    Description

    This theme discusses advances in spacecraft attitude dynamics and control, as well as design, testing and performance of novel 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

    2015-10-14

    Time

    14:45

    Room

    Teddy B (ICC, lower level)

    IPC members
    • Co-Chair: Prof. Mikhail Ovchinnikov, Keldysh Institute of Applied Mathematics, RAS, Russian Federation;

    • Co-Chair: Mrs. Amalia Ercoli Finzi, Politecnico di Milano, Italy;

    • Rapporteur: Dr. Hao-Chi Chang, tiSPACE Inc., Unknown;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Natural periodic orbit-attitude behaviors for rigid bodies in three-body periodic orbits

    15'

    confirmed

    Mr. Davide Guzzetti

    Purdue University

    United States

    2

    Attitude estimation and control design for single steerable single wing satellite

    15'

    confirmed

    Dr. Hao-Chi Chang

    National Space Organization

    Taiwan, China

    3

    An efficient momentum dumping method through an alternative sun pointing strategy for small Near Equatorial Orbit satellite

    15'

    confirmed

    Mr. Mihindukulasooriya Sheral Crescent Tissera

    Nanyang Technological University

    Singapore, Republic of

    4

    robust optimal sun-pointing control of a large solar power satellite

    15'

    withdrawn

    Prof. Gianmarco Radice

    University of Glasgow

    United Kingdom

    5

    Nonlinear H-inf via Modified Rodrigues Parameters for Attitude Control in the Reuse of Retired Spacecraft Antenna

    15'

    confirmed

    Mr. Xiaoyu Lang

    Research Center of Satellite Technology, Harbin Institute of Technology

    China

    6

    Attitude determination for the Unisat-6 microsatellite

    15'

    confirmed

    Prof. Simone Battistini

    Universidade de Brasília

    Brazil

    7

    On the rotational Cucker-Smale model: optimal formation configuration and adaptive gains design

    15'

    confirmed

    Mr. Fabrizio Paita

    Universitat Politecnica de Catalunya (UPC)

    Spain

    8

    multi-pendulum modeling of propellant sloshing via parameter optimization

    15'

    no-show

    Mr. dong-yeon lee

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    9

    coupled attitude-orbit dynamic modeling of high area-to-mass spacecraft and significance analysis of perturbation factors

    15'

    confirmed

    Ms. Qiao Qiao

    National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University

    China

    10

    Determining High Rate Angular Velocity from Star Tracker Measurements

    15'

    confirmed

    Prof. Fabio Curti

    Sapienza - University of Rome

    Italy

    11

    Adaptive Attitude Control for Spacecraft with Unknown Dead-Zone of Thruster

    15'

    no-show

    Mr. LI DONGBAI

    Research Center of Satellite Technology, Harbin Institute of Technology

    China