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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

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    confirmed

    15'

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

    Dr. Elisa Maria Alessi

    IFAC-CNR

    Italy

    2

    confirmed

    15'

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

    Dr. Junichiro Kawaguchi

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    3

    confirmed

    15'

    Dynamics of a Spacecraft in the Vicinity of Binary Asteroids

    Ms. Pamela Woo

    McGill University

    Canada

    4

    confirmed

    15'

    Orbit Dynamics in the Vicinity of Contact Binary Asteroids

    Ms. Feng Jinglang

    Delft University of Technology (TU Delft), The Netherlands

    The Netherlands

    5

    confirmed

    15'

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

    Dr. Yue Wang

    Beihang University

    Israel

    6

    confirmed

    15'

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

    Dr. Daniel Garcia Yarnoz

    Advanced Space Concept Laboratory, University of Strathclyde

    United Kingdom

    7

    confirmed

    15'

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

    Dr. Songjie HU

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

    China

    8

    confirmed

    15'

    A simulation tool for Space Situational Awareness: Near Earth Objects

    Ms. Maria Piera Padula

    Politecnico di Milano

    Italy

    9

    confirmed

    15'

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

    Mr. Matthew Bourassa

    Carleton Univeristy

    Canada

    10

    confirmed

    15'

    Adaptive structures for spacecraft orbit control

    Ms. Stefania Soldini

    University of Southampton

    United Kingdom

    11

    confirmed

    15'

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

    Dr. Francesco Topputo

    Politecnico di Milano

    Italy

    12

    withdrawn

    15'

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

    Mr. Andrea Campa

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

    Italy