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  • session 3

    Title

    Guidance, Navigation and Control (1)

    Description

    The emphasis of this theme is on the studies and application related to the guidance, navigation and control of Earth-orbiting and interplanetary spacecraft and rockets, including formation flying, rendezvous and docking.

    Date

    2013-09-24

    Time

    14:45

    Room

    306A

    IPC members
    • Chairman: Dr. Fuyuto Terui, Japan Aerospace Exploration Agency (JAXA), Japan;

    • Chairman: Dr. Bernard Lübke-Ossenbeck, OHB System AG-Bremen, Germany;

    • Rapporteur: Prof. Paolo Teofilatto, Sapienza University of Rome, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Guidance, Navigation, and Control System Performance During the Landsat Data Continuity Mission Launch and Commissioning

    15'

    withdrawn

    Dr. James O'Donnell

    National Aeronautics and Space Administration (NASA), Goddard Space Flight Center

    United States

    2

    Phase space and orbit relative motion between high area-to-mass ratio spacecraft

    15'

    withdrawn

    Dr. Camilla Colombo

    University of Southampton

    Italy

    3

    A Linear Constant Gain Controller based on Integrated Guidance and Control for the re-entry phase of a manned space mission

    15'

    confirmed

    Mr. Pitchaimani M

    ISTRAC/ISRO

    India

    4

    Innovative Mars EDL GNC technologies for future China Mars exploration

    15'

    confirmed

    Prof. Shuang Li

    Nanjing University of Aeronautics and Astronautics

    China

    5

    Inter-satellite Orientation Observation and Long-term Autonomous Orbit Determination for Constellation

    15'

    confirmed

    Mr. Fei Han

    Shanghai Key Laboratory of Aerospace Intelligent Control Technology

    China

    6

    A Mixed Kalman/H-infinity Filtering Approach for Augmented Proportional Navigation Guidance

    15'

    confirmed

    Prof. Adrian-Mihail Stoica

    University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space

    Romania

    7

    Attitude Control of Spacecraft using Optimal Nonlinear Control SDRE and Theta-D

    15'

    confirmed

    Prof. M. Navabi

    Iran

    8

    application of plural momentum exchange impact dampers to landing gear systems

    15'

    confirmed

    Mr. Tsubasa Watanabe

    Nagoya University

    Japan

    9

    Optimal guidance for soft landing on irregular-shaped asteroids using sliding-mode control

    15'

    confirmed

    Mr. Hongwei YANG

    Tsinghua University

    China

    10

    On the Cucker-Smale flocking model applied to a formation moving in a central force-field

    15'

    confirmed

    Mr. Fabrizio Paita

    Universitat Politecnica de Catalunya (UPC)

    Spain

    11

    An Exploration of Numerical Methods for Low-Thrust Trajectory Optimization in N-Body Models

    15'

    confirmed

    Prof. Franco Bernelli-Zazzera

    Politecnico di Milano

    Italy

    12

    Visual Navigation Performance for precise Lunar Landing: Status of a Technological Breakthrough

    15'

    withdrawn

    Mr. Giovanni Orlando

    EADS Astrium Space Transportation GmbH

    Germany

    13

    The Shenzhou Manned Spacecraft Rendezvous and Docking Guidance, Navigation and Control Design

    15'

    confirmed

    Prof.Dr. Hu Jun

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

    China