• Home
  • IAF Digital Library
  • Public Website
  • My papers
  • Home
  • event
  • IAC-16
  • C1
  • 8
  • session 8

    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

    2016-09-30

    Time

    09:45

    Room

    Salon Jalisco E6

    IPC members
    • Co-Chair: Dr. Hao-Chi Chang, tiSPACE Inc., Unknown;

    • 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

    Inverse Dynamics Particle Swarm Optimization applied to constrained minimum-time maneuvers using reaction wheels

    15'

    confirmed

    Mr. Dario Spiller

    Sapienza University of Rome

    Italy

    2

    Concept Design for a Satellite with Micro Vibration Isolator

    15'

    confirmed

    Mr. Takuma Shibata

    The Graduate Universty for Advanced Studies[SOKENDAI]

    Japan

    3

    torque distribution algorithm for effective use of reaction wheels torque and angular momentum

    15'

    confirmed

    Mr. Mikihiro Sugita

    Mitsubishi Electric Corporation

    Japan

    4

    Using Aerodynamic Torques to Aid Detumbling into an Aerostable State

    15'

    confirmed

    Mr. Zhou Hao

    The University of Manchester

    United Kingdom

    5

    An attitude determination and control system for a nano-satellite alternative launch platform

    15'

    confirmed

    Prof. Simone Battistini

    Universidade de Brasília

    Brazil

    6

    analysis and design of logical differential control law

    15'

    confirmed

    Mr. XinXin Yu

    Beijing Institute of Control Engineering(BICE), China Academy of Space Technology(CAST)

    China

    7

    Stability Analysis of 3-axis Attitude Control System of Single Wing Satellite

    15'

    confirmed

    Dr. Hao-Chi Chang

    National Space Organization

    Taiwan, China

    8

    Simple Adaptive Control of a Satellite with Large Flexible Appendages

    15'

    confirmed

    Dr. Derek Gransden

    Delft University of Technology (TU Delft)

    The Netherlands

    9

    numerical evaluation of on-orbit attitude behavior for microsatellites with variable shape function

    15'

    confirmed

    Mr. Kyosuke Tawara

    Tokyo Institute of Technology

    Japan

    10

    ACS Feed-Forward for Manipulator Control During Coupled Satellite Detumbling

    15'

    withdrawn

    Mr. Barrett Dillow

    University of Maryland, College Park

    United States

    11

    Chaotic motions of tethered satellites with low thrust

    15'

    confirmed

    Prof. Vladimir S. Aslanov

    Samara National Research University (Samara University)

    Russian Federation

    12

    Constraint Force Algorithm for Dynamics Modeling of Flexible Multibody Spacecraft

    15'

    confirmed

    Ms. LI Haiyan

    China

    13

    Dynamics and Underactuated Robust Control of Rigid-flexible Coupling Tethered System for Space Deorbit

    15'

    withdrawn

    Dr. Liang Sun

    Beihang University

    China