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  • session 6

    Title

    Orbital Dynamics (1)

    type

    oral

    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

    09:45

    Room

    Salon Jalisco E6

    IPC members
    • Co-Chair: Prof. Daniel Scheeres, Colorado Center for Astrodynamics Research, University of Colorado, United States;

    • Co-Chair: Prof. Filippo Graziani, G.A.U.S.S. Srl, Italy;

    • Rapporteur: Prof. Gerard Gomez, University of Barcelona, Spain;

    • Rapporteur: Dr. Simei Ji, Beijing Institute of Technology, China;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Preliminary Results on the Dynamics of Large and Flexible Space Structures in Halo Orbits

    15'

    confirmed

    Mr. Andrea Colagrossi

    Politecnico di Milano

    Italy

    2

    DYNAMICS OF SPACECRAFT ORBITAL MOTION AROUND ASTEROID APOPHIS

    15'

    confirmed

    Ms. Anqi Lang

    N.E. Bauman Moscow State Technology University

    Russian Federation

    3

    Long-Term Orbit Propagation Using Symplectic Integration Algorithms

    15'

    confirmed

    Prof. David B. Spencer

    Pennsylvania State University

    United States

    4

    transfers between libration point orbits using lunar gravity assist

    15'

    confirmed

    Dr. Rui Zhong

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    5

    Influence of tether deployment on the atmospheric stage of tether-assisted payload return mission from elliptical orbit

    15'

    confirmed

    Dr. Alexander Ledkov

    Samara National Research University (Samara University)

    Russian Federation

    6

    An Accurate and Robust Method for Interplanetary Orbit Design

    15'

    confirmed

    Dr. An-Ming Wu

    National Space Organization

    Taiwan, China

    7

    Orbital dynamics of a solar sail accelerated by thermal desorption of coatings

    15'

    confirmed

    Prof. Roman Ya. Kezerashvili

    New York City College of Technology, The City University of New York

    United States

    8

    Effectiveness of KS elements in orbit prediction using Earth's Gravity, Drag and Solar Radiation Pressure

    15'

    Dr. Xavier James Raj

    Indian Space Research Organization (ISRO)

    India

    9

    Using Equinoctial Orbital Elements and Quasi-average Element Method to Construct Analytical Solutions for Geostationary Satellite

    15'

    confirmed

    Mr. Bin Liu

    Nanjing University

    China

    10

    artificial satellites orbiting planetary satellites: critical inclination and helio-synchronous orbits

    15'

    confirmed

    Prof. Rodolpho V. Moraes

    Federal University of São Paulo (UNIFESP)

    Brazil

    11

    Analysis of the influence of area-to-mass ratio error on the orbital motion of a solar power satellite

    15'

    confirmed

    Prof. Gianmarco Radice

    University of Glasgow

    United Kingdom

    12

    A heuristic strategy to compute ensembles of trajectories for 3D low-cost Earth-Moon transfers

    15'

    confirmed

    Dr. Priscilla Sousa Silva

    Instituto Tecnológico de Aeronáutica (ITA)

    Brazil

    13

    Solar radiation pressure assisted transfers between lissajous orbits of the Sun-Earth system

    15'

    confirmed

    Dr. Stefania Soldini

    JAXA

    Japan