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  • session 3

    Title

    Guidance, Navigation & Control (1)

    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 formation flying, rendezvous and docking.

    Date

    2017-09-26

    Time

    14:45

    Room

    Hall A

    IPC members
    • Co-Chair: Prof. Yong Chun Xie, Beijing Institute of Control Engineering, China Academy of Space Technology (CAST), China;

    • Rapporteur: Prof. Fuyuto Terui, Kanagawa Institute of Technology, Japan;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Semi-autonomous attitude guidance using relative navigation based on Line of Sight measurements – AIM scenario

    15

    confirmed

    Mr. Andrea Pellacani

    G.M.V. Space and Defence, S.A.

    Spain

    3

    Monocular vision based simultaneous localization and mapping for close proximity navigation near an asteroid

    15

    confirmed

    Mr. Arunkumar Rathinam

    University of New South Wales

    Australia

    4

    Accurate penetrator for the in-situ astrobiological exploration of Europa

    15

    confirmed

    Mr. Konstantinos Konstantinidis

    Universität der Bundeswehr München

    Germany

    5

    Monocular and LIDAR based determination of shape, relative attitude and position of a non-cooperative, unknown satellite

    15

    confirmed

    Mr. Renato Volpe

    University of Rome "La Sapienza"

    Italy

    7

    vision-based state estimation of an uncooperative space object

    15

    confirmed

    Mr. Vincenzo Pesce

    Politecnico di Milano

    Italy

    8

    a robust path-tracking guidance considering uncertainty for mars atmospheric entry

    15

    confirmed

    Dr. Zhengshi Yu

    School of Aerospace Engineering, Beijing Institute of Technology

    China

    9

    Development and Validation of GNC Functional Modes for Asteroids Sample Return Mission in the frame of the European Commission H2020 NEOShield-2 Project

    15

    confirmed

    Mr. Matteo Suatoni

    G.M.V. Space and Defence, S.A.

    Spain

    11

    Attainable Landing Area Computation of Lunar Landers with Pseudo-Spectral and Polynomial based Guidance Methods

    15

    confirmed

    Mr. Mohammad Alsharif

    University of Bremen

    Germany