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  • session 2

    Title

    Attitude Dynamics (2)

    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

    2023-10-04

    Time

    10:15

    Room

    BCC B4

    IPC members
    • Co-Chair: Prof. Toshio Kamiya, Meisei University, Japan;

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

    • Rapporteur: Bang Hyochoong, Korea Advanced Institute of Science and Technology (KAIST), Korea, Republic of;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    KEYNOTE: "Breakwell Lecture" - Small Satellites Dynamics and Control: Retrospect and Future

    30

    confirmed

    Prof. Mikhail Ovchinnikov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    2

    10:45

    Attitude control and trajectory planning of a space manipulator system using Kane’s formulation

    15

    confirmed

    Mr. David Paolo Madonna

    Sapienza University of Rome

    Italy

    3

    11:00

    Attitude control using Iterative Learning Control considering orbital motion of NRHO

    15

    confirmed

    Mr. Yuta Hayashi

    Kyushu University

    Japan

    4

    11:15

    HERMES ADCS: from system design to pre-flight verification and testing

    15

    confirmed

    Dr. Andrea Colagrossi

    Politecnico di Milano

    Italy

    5

    11:30

    Adaptive kernel Kalman filter on Lie groups for attitude estimation of nanosatellites

    15

    withdrawn

    Mr. Joe Gibbs

    School of Engineering, University of Glasgow

    United Kingdom

    6

    11:45

    Large-Angle Attitude Maneuver of Variable-Shape Spacecraft with Nonlinear Model Predictive Control

    15

    confirmed

    Mr. Haruta Miki

    Tokyo Institute of Technology

    Japan

    7

    12:00

    Online Estimation of Unknown Parameters for Flexible Spacecraft subject to Measurements Noise

    15

    confirmed

    Mr. Nicolo Woodward

    Embry-Riddle Aeronautical University

    United States

    8

    12:15

    synthesis of program angular motion regimes for the magnetic attitude control system of spacecraft

    15

    confirmed

    Ms. Anna Okhitina

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    9

    12:30

    Kernel Management strategy for Reaction wheel optimal speed control for spacecrafts for enhanced pointing accuracy and agility

    15

    confirmed

    Mrs. Pratibha Srivastava

    U R RAO SATELLITE CENTRE (URSC)

    India