• Home
  • IAF Digital Library
  • Public Website
  • My papers
  • Home
  • event
  • IAC-22
  • C1
  • 1
  • session 1

    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

    2022-09-18

    Time

    15:15

    Room

    S05

    IPC members
    • Co-Chair: Prof. Giovanni B. Palmerini, Sapienza University of Rome, Italy;

    • Co-Chair: Prof. Robert G. Melton, Pennsylvania State University, United States;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:15

    Design, realization and characterization of a free-floating platform for flexible satellite control experiments

    15

    confirmed

    Dr. Marco Sabatini

    Sapienza University of Rome

    Italy

    2

    15:30

    Reinforcement Learning for Attitude Control of a Spacecraft with Flexible Appendages

    15

    confirmed

    Mr. Ahmed Mahfouz

    University of Luxembourg

    Luxembourg

    3

    15:45

    reaction wheel unloading using external torque for variable shape spacecraft

    15

    confirmed

    Mr. Yuki Amaki

    Tokyo Institute of Technology

    Japan

    4

    16:00

    Fuzzy-Logic-Based Integrated Orbit-Attitude-Vibration Prescribed-Time Control for Large-Scale Flexible Spacecraft

    15

    confirmed

    Dr. Chuang Liu

    Northwestern Polytechnical University

    China

    5

    16:15

    Online policy iteration ADP-based control of post-capture combined spacecraft without inertia identifications

    15

    confirmed

    Mrs. Jingyi Liu

    Delft University of Technology (TU Delft)

    The Netherlands

    6

    16:30

    Attitude control of satellites with flexible appendages using inverse simulation

    15

    confirmed

    Mr. Robert Gordon

    University of Glasgow

    United Kingdom

    7

    16:45

    Time-Optimal Attitude Controller Design for Precision Pointing of an Agile Spacecraft using Deep Reinforcement Learning

    15

    confirmed

    Dr. Vinod Kumar

    Indian Space Research Organization (ISRO)

    India

    8

    17:00

    Invariant Sigma-Point Kalman Filtering on SO(3) for Attitude Estimation of a 3U CubeSat

    15

    confirmed

    Mr. Joe Gibbs

    School of Engineering, University of Glasgow

    United Kingdom

    9

    17:15

    Simultaneous Orbit-Attitude Control of Formation Flying Solar Sails around Sun-Earth L2 Using Reflectivity Modulation

    15

    confirmed

    Mr. Keisuke Sugiura

    Aoyama Gakuin University

    Japan

    10

    17:30

    Attitude Determination and Control System of the Student Small Satellite (SSS): An International Hands-On Satellite Project Among Asia Pacific Universities

    15

    confirmed

    Ms. Niki Sajjad

    K. N. Toosi University of Technology

    Iran