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  • session 1

    Title

    Orbital Dynamics

    Description

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

    Date

    2010-09-27

    Time

    15:15

    Room

    North Hall

    IPC members
    • Chairman: Prof. Rock Jeng-Shing Chern, Ryerson University, Canada;

    • Chairman: Prof. Paolo Teofilatto, Sapienza University of Rome, Italy;

    • Rapporteur: Prof. Othon Winter, UNESP - Univ Estadual Paulista, Brazil;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    analytic expansions of luni-solar gravity perturbations along rotating axes for trajectory optimization: part2: the multipliers system and simulations

    15

    confirmed

    Dr. jean kechichian

    The Aerospace Corporation

    United States

    2

    New Numerical Methods for Determining Periodic Orbits in the Circular Restricted Three-Body Problem

    15

    confirmed

    Dr. Mauro Pontani

    Sapienza University of Rome

    Italy

    3

    extension of low thrust propulsion to the coplanar circular restricted four body problem with applications to future trojan asteroids missions

    15

    confirmed

    Dr. marta ceccaroni

    University of Strathclyde

    Italy

    4

    On the low-energy transfers between icy moons of Jupiter

    15

    Dr. Elena Fantino

    Universitat Politecnica de Catalunya (UPC)

    Spain

    5

    Electric ?V in Solar Electric Propulsion (SEP) and Flyby for Near-Earth-Objects

    15

    confirmed

    Dr. Denilson Paulo Souza dos Santos

    INPE

    Brazil

    6

    Short-Period Ballistic Out-of-Ecliptic Trajectories via Multiple Venus & Earth Swing-bys and VEGA-driven Multiple Earth Swing-bys

    15

    confirmed

    Dr. Junichiro Kawaguchi

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    7

    Trajectory Evolution in Multi-Body Regimes with Applications in the Saturnian System

    15

    confirmed

    Ms. Diane Davis

    Purdue University

    United States

    8

    accuracy analysis of orbit determination and prediction for low orbit lunar satellites

    15

    confirmed

    Prof. Jiasong Wang

    State Key Lab of Astrodynamics

    China

    9

    Coulomb testbed force model verification for charged relative motion experiments

    15

    confirmed

    Mr. Carl Seubert

    Colorado Center for Astrodynamics Research, University of Colorado

    United States

    10

    Orbit Perturbations and Eccentricity Vector Control in Low-Altitude Moon Orbits

    15

    withdrawn

    Mr. Slim Locoche

    EADS Astrium

    France

    11

    How to Establish and Keep Orthogonal Constellation by Two Orbiters Under Perturbation

    15

    confirmed

    Dr. Naoko Ogawa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    12

    Spacecraft Rendezvous Through Motion Camouflage

    15

    Ms. Tao Yang

    China