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  • session 4

    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

    2018-10-03

    Time

    09:45

    Room

    CCB Borgward

    IPC members
    • Co-Chair: Dr. James O'Donnell, National Aeronautics and Space Administration (NASA), Goddard Space Flight Center, United States;

    • Co-Chair: Prof. Gianmarco Radice, Singapore, Republic of;

    • Rapporteur: Dr. Shinji Hokamoto, Kyushu University, Japan;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    High stability and Pointing performance AOCS for the ECULID Mission

    15

    confirmed

    Mr. Alfredo Agenjo

    SENER

    Spain

    2

    10:00

    Investigation of Redundancy Strategies in Fluid-Dynamic Attitude Control

    15

    confirmed

    Mr. Johannes Ferdinand Fürstenau

    Technische Universität Berlin

    Germany

    3

    10:15

    Closed-Chain Forward Dynamics Modeling of a Four-Panel Folding Spacecraft Structure

    15

    confirmed

    Ms. JoAnna Fulton

    University of Colorado Boulder

    United States

    4

    10:30

    Optimal Control of Spacecraft Attitude Motion using Port-Hamiltonian Systems

    15

    confirmed

    Mr. Sakamoto Tomoya

    Kyushu University

    Japan

    5

    10:45

    Minimum-Error Single-Axis Pointing for an Underactuated Spacecraft in the Presence of a Residual Angular Momentum

    15

    confirmed

    Prof. Giulio Avanzini

    Università del Salento

    Italy

    6

    11:00

    Base Attitude Stabilization of Space Robot with Guaranteed Prescribed Performance

    15

    confirmed

    Dr. Mingming Wang

    National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University

    China

    7

    11:15

    Lyapunov control for attitude maneuvers with restricted areas

    15

    confirmed

    Mr. Yaroslav Mashtakov

    Keldysh Institute of Applied Mathematics of RAS

    Russian Federation

    8

    11:30

    Attitude dynamics of an electric sail model with a realistic shape

    15

    confirmed

    Mr. Marco Bassetto

    University of Pisa

    Italy

    9

    11:45

    performance analysis of an attitude control system\\ for small satellites

    15

    confirmed

    Mr. Matteo Dentis

    Politecnico di Torino

    Italy

    10

    12:00

    Nonlinear Observer for Attitude Estimation and Rate Gyro Calibration

    15

    confirmed

    Dr. Sérgio Brás

    HE Space

    The Netherlands

    11

    12:15

    Synergetic approach in attitude control of very flexible satellites by means of thrusters and PZT devices

    15

    confirmed

    Dr. Marco Sabatini

    Sapienza University of Rome

    Italy

    12

    12:30

    Landmark Acquisition and Tracking Using Variable Speed Control Moment Gyros

    15

    withdrawn

    Mr. Abhilash Mony

    Vikram Sarabhai Space Centre (VSSC)

    India