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  • session 9

    Title

    Guidance, Navigation and Control - Part 3

    type

    oral

    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 rendezvous and docking.

    Date

    2011-10-07

    Time

    14:00

    Room

    TS-04

    IPC members
    • Chairman: Prof. Weihua Zhang, National University of Defense Technology, China;

    • Chairman: Prof. Saburo Matunaga, Tokyo Institute of Technology, Japan;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Guidance, Navigation, and Control System Design of HTV and Evaluation of On-orbit Results

    15

    confirmed

    Dr. Shoji Yoshikawa

    Mitsubishi Electric Corporation

    Japan

    2

    Rendezvous Technique of HTV and Evaluation of On-orbit Results

    15

    confirmed

    Dr. Shoji Yoshikawa

    Mitsubishi Electric Corporation

    Japan

    3

    An On-Orbit Mass Properties Identification Algorithm for Large Space Structures

    15

    confirmed

    Ms. Ling Jiang

    Beihang University

    China

    4

    Spacecraft Actuator Alignment Determination through Null Motion Excitation

    15

    confirmed

    Dr. Frederick Leve

    Air Force Research Laboratory (AFRL)

    United States

    5

    Global and local optimization approaches for launch vehicles ascent trajectory design

    15

    confirmed

    Ms. Annalisa Riccardi

    University of Bremen

    Germany

    6

    A Novel Navigation Solution of Reusable Launch Vehicle Based on Multi-Source Geospatial Information Fusion

    15

    no-show

    Dr. Nie Qi

    Beijing Aerospace Automatic Control Institute

    China

    7

    A Novel Approach to Hybrid Propulsion Transfers

    15

    confirmed

    Mr. Steven Owens

    Advanced Space Concept Laboratory, University of Strathclyde

    United Kingdom

    8

    Mathematical model for attitude control of small satellites using rotation angles

    15

    confirmed

    Prof. Teodor-Viorel Chelaru

    University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space

    Romania

    9

    In-Orbit Identification of Moment of Inertia Matrix for High Pointing Satellites

    15

    confirmed

    Mr. Bharadwaj K.M.

    Indian Space Research Organization (ISRO)

    India

    10

    Neural Network Based Predictor-Corrector Entry Guidance for High Lifting Vehicles

    15

    withdrawn

    Mr. Mingliang Xu

    National University of Defense Technology

    China

    11

    Derivation of a Complete Set of Equations of Motion for Coupled Slosh-Vehicle Dynamics

    15

    confirmed

    Dr. Mohammad Ebrahimi

    Aerospace Research Institute

    Iran