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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

    2017-09-26

    Time

    09:45

    Room

    Hall A

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

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

    • Rapporteur: Dr. Hao-Chi Chang, tiSPACE Inc., Unknown;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    robust collocated sun-pointing control of a large solar power satellite

    15

    withdrawn

    Dr. Shunan Wu

    Dalian University of Technology (DUT)

    China

    2

    10:00

    Particle Swarm/Differential Evolution Optimizer for Constrained Slew Maneuvers

    15

    confirmed

    Prof. Robert G. Melton

    Pennsylvania State University

    United States

    3

    10:15

    Usage of solar and gravitational torques for reaction wheels desaturation

    15

    confirmed

    Mr. Yaroslav Mashtakov

    Keldysh Institute of Applied Mathematics of RAS

    Russian Federation

    4

    10:30

    Kinematic Steering Enabling Speed-Constrained Three-Axes Attitude Control

    15

    confirmed

    Prof. Hanspeter Schaub

    Colorado Center for Astrodynamics Research, University of Colorado

    United States

    5

    10:45

    Adaptive Spacecraft Attitude Control with Incremental Approximate Dynamic Programming

    15

    confirmed

    Ms. Ye Zhou

    Delft University of Technology (TU Delft)

    The Netherlands

    6

    11:00

    vision-based attitude determination system for small satellites using unscented kalman filter

    15

    confirmed

    Mr. Dagvasumberel Amartuvshin

    Kyushu Institute of Technology

    Japan

    7

    11:15

    PID Controller Optimization for Android-Powered Nanosatellites Using Jacobian-Based Scaling

    15

    confirmed

    Mr. Mohammad Alsharif

    University of Bremen

    Germany

    8

    11:30

    On Orbit Servicing GNC through a dual quaternion approach

    15

    confirmed

    Mr. Aureliano Rivolta

    Politecnico di Milano

    Italy

    9

    11:45

    Spacecraft attitude control system based on Total Energy Control Approach.

    15

    confirmed

    Mr. Rolando Cortés

    CINVESTAV

    Mexico

    10

    12:00

    A comprehensive study on magnetic actuator design for CubeSat missions.

    15

    confirmed

    Ms. Anja Kohfeldt

    Technische Universität Berlin

    Germany

    11

    12:15

    Attitude Control of a 3U CubeSat Equipped with a Large Loop Antenna

    15

    confirmed

    Ms. Hasnaa Khalifi

    University of Florida

    United States

    12

    12:30

    analysis of the attitude motion and structural vibration coupling for solar power satellite

    15

    confirmed

    Dr. Shunan Wu

    Dalian University of Technology (DUT)

    China