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  • session 7

    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 natural orbital dynamics of spacecraft in the Solar System. It also covers advances in orbit determination.

    Date

    2016-09-29

    Time

    14:45

    Room

    Salon Jalisco E6

    IPC members
    • Co-Chair: Prof. Josep J. Masdemont, Universitat Politecnica de Catalunya (UPC), Spain;

    • Co-Chair: Dr. Antonio Almeida Prado, INPE, Brazil;

    • Rapporteur: Mr. Laureano Cangahuala, Jet Propulsion Laboratory, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    De-Orbiting and Re-entry Analysis with Generalised Intrusive Polynomial Expansions

    15'

    confirmed

    Dr. Massimiliano Vasile

    University of Strathclyde

    United Kingdom

    2

    Computation of periodic orbits in multi-body models using Cell Mapping

    15'

    withdrawn

    Ms. Dayung Koh

    University of Southern California

    United States

    3

    Mission analysis for a space weather monitoring system near the Sun-Earth L1 and L5 libration points

    15'

    confirmed

    Dr. Aurelie Heritier

    Deimos Space UK Ltd

    United Kingdom

    4

    Quasi-periodic Invariant Tori of Time-periodic Dynamical Systems: Applications to Small Body Exploration

    15'

    confirmed

    Mr. Nicola Baresi

    Colorado Center for Astrodynamics Research, University of Colorado

    United States

    5

    Modelling and Stability Analysis of Generic Non-Keplerian Elliptic Orbits for Solar Sails with Reflection Control Devices

    15'

    withdrawn

    Mr. Jianlin Chen

    National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University

    China

    5

    Modelling and Stability Analysis of Generic Non-Keplerian Elliptic Orbits for Solar Sails with Reflection Control Devices

    15'

    confirmed

    Mr. Hongwen Zhang

    National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an

    China

    6

    the calculation features of flyby maneuvers of a space vehicle sequentially taking the objects of large-size space debris to low disposal orbits

    15'

    confirmed

    Mr. Dmitriy Grishko

    Bauman Moscow State Technical University

    Russian Federation

    7

    The Consequences of Stiffness in Numerical Solutions of Astrodynamics Problems

    15'

    withdrawn

    Dr. David Finkleman

    International Academy of Astronautics

    United States

    8

    The effect of solar radiation pressure on Solar orbiter Gravity Assist Maneuvers

    15'

    Mr. Dusan Marceta

    University of Belgrade, Faculty of Mathematics

    Serbia

    9

    periodic orbits design based on the center manifold theory in the circular restricted three-body problem

    15'

    confirmed

    Mr. Yuki Akiyama

    Kyushu University

    Japan

    10

    Periodic and quasi-periodic motions for a Solar sail in the Earth-Moon system

    15'

    confirmed

    Mr. Marc Jorba-Cuscó

    University of Barcelona

    Spain

    11

    Solar reflectors about the Sun-Earth artificial collinear equilibrium points

    15'

    confirmed

    Dr. Francisco Salazar

    Universidade Estadual Paulista - Grupo de Dinâmica Orbital

    Brazil

    12

    Analysis of ballistic capture dynamics with a semianalytical approach

    15'

    withdrawn

    Mr. Diogene Alessandro Dei Tos

    Politecnico di Milano

    Italy