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  • session 3

    Title

    Orbital Dynamics - Part 1

    type

    oral

    Description

    This theme discusses advances in orbital dynamics, orbit determination, and orbit control. It includes orbital dynamics associated with constellations and formation flying.

    Date

    2011-10-04

    Time

    15:00

    Room

    TS-04

    IPC members
    • Chairman: Prof. Jeng-Shing (Rock) Chern, International Academy of Astronautics (IAA), Canada;

    • Chairman: Prof. Filippo Graziani, G.A.U.S.S. Srl, Italy;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Effect of a drag force due to absorption of solar radiation on solar sail orbital dynamics

    15

    confirmed

    Prof. Roman Ya. Kezerashvili

    New York City College of Technology

    United States

    2

    Analytical Solutions of the Relative Motion About a Keplerian Elliptic Orbit

    15

    confirmed

    Prof. Gerard Gomez

    University of Barcelona

    Spain

    3

    Post-aerocapture orbit selection and maintenance for the Aerofast mission to Mars

    15

    confirmed

    Dr. Mauro Pontani

    Sapienza University of Rome

    Italy

    4

    An Extended Discussion on the DoubleStar Orbits

    15

    confirmed

    Dr. Jingshi Tang

    Nanjing University

    China

    5

    Station keeping of a solar sail in the solar system

    15

    confirmed

    Dr. Ariadna Farrés

    Université de Bourgogne

    Spain

    6

    India's first MARS Mission Orbit Determination System

    15

    withdrawn

    Dr. Narayanasetti Venkata Vighnesam

    Indian Space Research Organization (ISRO)

    India

    7

    Optimal Impulsive Orbital Maneuver between Noncoplanar Noncoaxial orbits with or without Time constraint

    15

    confirmed

    Prof. M. Navabi

    Shahid Beheshti University

    Iran

    8

    Natural Periodic Relative Orbit Solving using Fourier Series

    15

    confirmed

    Dr. Jing Cao

    College of Astronautics, Northwestern Polytechnical University

    China

    9

    Long-term evolution of Galileo operational orbits by canonical perturbation theory

    15

    confirmed

    Dr. Paul Cefola

    University at Buffalo

    United States

    10

    Simulation of Orbit and Guidance Design for TSLV

    15

    confirmed

    Prof. Rock Jeng-Shing Chern

    University of Science & Technology

    Canada

    11

    Stability analysis of a highly eccentric orbit around Mars

    15

    confirmed

    Mrs. Bannihatti Parameshwarappa Dakshayani

    ISRO Satellite Centre (ISAC)

    India

    12

    Mars-Phobos low energy transfer in the restricted three body problem

    15

    withdrawn

    Dr. Dong Qiao

    Beijing Institute of Technology

    China