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  • session 6

    Title

    Attitude Dynamics (2)

    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

    2019-10-24

    Time

    09:45

    Room

    150A

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

    • Co-Chair: Prof. Paolo Teofilatto, Sapienza University of Rome, Italy;

    • Rapporteur: Dr. Toshio Kamiya, NEC Corporation, Japan;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    Euclid Dark Universe Mission – High stability and pointing performance control

    15

    confirmed

    Mr. Raúl Sánchez Maestro

    SENER Ingenieria y Sistemas, S.A.

    Spain

    2

    10:00

    Analytic Spacecraft Attitude and Rate Estimation Performance During Attitude Sensor Outages

    15

    confirmed

    Dr. Joseph Galante

    NASA Goddard Space Flight Center Greenbelt MD 20771

    United States

    3

    10:15

    On the management of the satellite angular momentum taking advantage of external torques

    15

    confirmed

    Mr. Ivan Sumelzo Martinez

    Thales Alenia Space France

    France

    4

    10:30

    Attitude Control for the LUMIO CubeSat in Deep Space

    15

    confirmed

    Mr. Álvaro Romero-Calvo

    Politecnico di Milano

    Italy

    5

    10:45

    Experimentation of Nonlinear Spacecraft Attitude Motion Control via Successive Linearization Based Model Predictive Control

    15

    confirmed

    Mr. Burak Omer Iskender

    Nanyang Technological University

    Singapore, Republic of

    6

    11:00

    Attitude Guidance and Control for Rapid Deorbit of Space Debris by Aerodynamic Drag

    15

    confirmed

    Dr. Takahiro Sasaki

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    7

    11:15

    A Three-Axis Fluid-Dynamic Attitude Control Experiment for SALSAT

    15

    confirmed

    Mr. Daniel Noack

    Technische Universität Berlin

    Germany

    8

    11:30

    Analyzing the Stabilization of a Tumbling Satellite using Finite Element Methods

    15

    confirmed

    Mr. Ryotaro SAKAMOTO

    University of Colorado Boulder

    United States

    9

    11:45

    Coordinated Attitude Determination and Control in a Swarm of CubeSats

    15

    confirmed

    Mr. Ahmed Mahfouz

    Skolkovo Institute of Science and Technology

    Russian Federation

    10

    12:00

    ZERO PROPRLLANT MANEUVER PATH PLANNING OF SPACE SATTION UNDER MULTIPLE CONSTRAINTS

    15

    confirmed

    Mr. Zhuo Wang

    Beijing Institute of Technology

    China

    11

    12:15

    Angular rate determination using star sensors and novel algorithms based on geometrical investigations

    15

    confirmed

    Dr. Dario Spiller

    Sapienza University of Rome

    Italy

    12

    12:30

    Sliding Mode Techniques for Precise Attitude Control

    15

    confirmed

    Dr. Matteo Dentis

    Politecnico di Torino

    Italy