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  • 6
  • session 6

    Title

    Guidance, Navigation, and Control (2)

    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

    2010-09-30

    Time

    10:15

    Room

    North Hall

    IPC members
    • Chairman: Mr. Jean-Paul Berthias, Centre National d'Etudes Spatiales (CNES), France;

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

    • Rapporteur: Mrs Benedicte Escudier, Institut Supérieur de l'Aéronautique et de l'Espace (ISAE), France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Trajectory Reconstruction of Hayabusa's Atmospheric Reentry

    15

    confirmed

    Mr. Michael Shoemaker

    Kyushu University

    Japan

    2

    Precise Modeling of Solar Radiation and Thermal Accelerations on Rosetta

    15

    confirmed

    Dr. Takahiro Kato

    Kyushu University

    Germany

    3

    Requirements and Design Study of the HTV Recovery Trajectory

    15

    confirmed

    Mr. Keiichi Wada

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    estimation of solar radiation pressure force for solar sail navigation

    15

    confirmed

    Mr. Tomohiro Yamaguchi

    The Graduate University of Advanced Studies

    Japan

    5

    Proximity Navigation for Asteroid Mission using CCD Imager

    15

    confirmed

    Dr. Kikuko Miyata

    NESTRA

    Japan

    6

    Evaluation and Findings of HTV-1 Trajectory and the Planning Operation

    15

    confirmed

    Mr. Keiichi Wada

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    7

    DEIMOS PRECISION LANDER GUIDANCE, NAVIGATION AND CONTROL DESIGN

    15

    confirmed

    Mr. James Kaidy

    The John Hopkins University Applied Physics Laboratory

    United States

    8

    Reducing uncertainties effects for Air-Launch Systems

    15

    withdrawn

    Mr. Luigi Ridolfi

    Scuola di Ingegneria Aerospaziale

    Italy

    9

    Design of a robust control law for the VEGA launcher ballistic phase

    15

    confirmed

    Ms. Monica Valli

    Politecnico di Milano

    Italy

    10

    Adaptive Guidance Law for Trajectory Control of a Reusable Launch Vehicle during Air-Breathing Ascent Phase

    15

    Dr. Venkitakrishnan Brinda

    Indian Space Research Organization (ISRO)

    India

    11

    Fault Detection and Isolation for Satellite using the IMM-UKF Algorithm

    15

    confirmed

    Dr. Jonghee Bae

    Seoul National University

    Korea, Republic of

    12

    Vision Based Navigation for Autonomous Pinpoint Lunar Landing

    15

    Mr. junhua feng

    Harbin Institute of Technology

    China