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  • session 9

    Title

    Orbital Dynamics (2)

    Description

    This theme discusses advances in the knowledge of natural motions of objects in orbit around the Earth, planets, minor bodies, Lagrangian points and more generally orbital dynamics of spacecraft in the Solar System. It also covers advances in orbit determination.

    Date

    2013-09-27

    Time

    13:30

    Room

    306A

    IPC members
    • Chairman: Prof. Othon Winter, UNESP - Univ Estadual Paulista, Brazil;

    • Chairman: Prof. Josep J. Masdemont, Universitat Politecnica de Catalunya (UPC), Spain;

    • Rapporteur: Dr. Shoji Yoshikawa, Mitsubishi Electric Corporation, Japan;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    out-of-plane extension of resonant encounters for escape and capture

    15'

    confirmed

    Dr. Elisa Maria Alessi

    IFAC-CNR

    Italy

    2

    A New Strategy of Designing Low-Thrust Trajectories in Alternate Rotational Coordinates

    15'

    confirmed

    Dr. Junichiro Kawaguchi

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    3

    Dynamics of a Spacecraft in the Vicinity of Binary Asteroids

    15'

    confirmed

    Ms. Pamela Woo

    McGill University

    Canada

    4

    Orbit Dynamics in the Vicinity of Contact Binary Asteroids

    15'

    confirmed

    Ms. Feng Jinglang

    Delft University of Technology (TU Delft), The Netherlands

    The Netherlands

    5

    Linear stability of the relative equilibria of a spacecraft around an asteroid

    15'

    confirmed

    Dr. Yue Wang

    Beihang University

    Israel

    6

    Applications of SRP dominated highly non-Keplerian trajectories around minor bodies

    15'

    confirmed

    Dr. Daniel Garcia Yarnoz

    Advanced Space Concept Laboratory, University of Strathclyde

    United Kingdom

    7

    Combined Orbit Determination for CE-2 and Toutatis Based on Optical Imaging Data at Fly-by

    15'

    confirmed

    Dr. Songjie HU

    1)Science and Technology on Aerospace Flight Dynamics Laboratory, China,2)Beijing Aerospace Control Center, China

    China

    8

    A simulation tool for Space Situational Awareness: Near Earth Objects

    15'

    confirmed

    Ms. Maria Piera Padula

    Politecnico di Milano

    Italy

    9

    Switch Points for Highly Eccentric Orbits: Modelling the Occurrences of Sign Changes in the Rate of Change of the Eccentricity

    15'

    confirmed

    Mr. Matthew Bourassa

    Carleton Univeristy

    Canada

    10

    Adaptive structures for spacecraft orbit control

    15'

    confirmed

    Ms. Stefania Soldini

    University of Southampton

    United Kingdom

    11

    Numerical Approximation of Invariant Manifolds in the Restricted Three-Body Problem

    15'

    confirmed

    Dr. Francesco Topputo

    Politecnico di Milano

    Italy

    12

    The Farside Explorer: Mission Analysis - Design and computation of a Quasi Ballistic transfer trajectory to the far side of the Moon

    15'

    withdrawn

    Mr. Andrea Campa

    ISAE - Institut Supérieur de l'Aéronautique et de l'Espace

    Italy