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  • session 5

    Title

    Mission and Constellation Design

    Description

    This session deals with mission, constellation and formation flying with emphasis on studies and experiences related to current and future projects while taking into account mission constraints and implementation problems.

    Date

    2009-10-14

    Time

    15:00

    Room

    Technical Session #7

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

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

    • Rapporteur: Prof. Eberhard Gill, Delft University of Technology, The Netherlands;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Methodology and Results of Analysis of Zenit, Cyclone Launch Vehicles Orbital Injection Accuracy

    15'

    Mr. Alexander Novikov

    Yuzhnoye State Design Office

    Ukraine

    2

    Moon swingby at realization of trajectories of interplanetary flight

    15'

    Prof. Mikhail S. Konstantinov

    Moscow Aviation Institute

    Russian Federation

    4

    Advanced Modeling of Optimal Low-Thrust Lunar Pole-Sitter Trajectories

    15'

    Dr. Daniel Grebow

    Jet Propulsion Laboratory - California Institute of Technology

    United States

    5

    Low-cost Asteroid Mission Opportunities using Venus Gravity Assist

    15'

    Dr. Kikuko Miyata

    NESTRA

    Japan

    6

    Jupiter Ganymade Orbiter: Design of the pseudo-orbit near Callisto

    15'

    Mr. Johannes Schoenmaekers

    European Space Operations Centre

    Germany

    7

    Numerical Study on Low Cost Connections between the Sun-Earth Libration Point 2 and the Earth-Moon Libration Point 2 Regions for Satellite Servicing

    15'

    Dr. Florian Renk

    European Space Agency (ESA)

    Germany

    8

    Reconfiguration of Spacecraft Formations in the Vicinity of Libration Points

    15'

    Dr. Laura Garcia-Taberner

    Universitat de Girona

    Spain

    9

    Agent-Based Modeling Techniques for Control of Satellite Formations in Multi-Body Regimes

    15'

    Ms. Lindsay Millard

    Purdue University

    United States

    11

    Proportional Guidance Law for Far Range Rendezvous

    15'

    Mr. Jiu-ren Li

    National University of Defense Technology

    China

    Methodology and Results of Analysis of Zenit, Cyclone Launch Vehicles Orbital Injection Accuracy

    Mr. A.V. Novikov

    Yuzhnoye State Design Office

    Ukraine