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  • session 1

    Title

    Optimization

    Description

    Optimization of trajectories including launch, orbital transfer, rendez-vous, atmospheric reentry, manoeuvring and station keeping will be covered in this session.

    Date

    2009-10-12

    Time

    15:00

    Room

    Technical Session #7

    IPC members
    • Chairman: Mr. David C. Folta, National Aeronautics and Space Administration (NASA), Goddard Space Flight Center, United States;

    • Chairman: Prof. Mauricio Moshe Guelman, Asher Space Research Institute, Technion, I.I.T., Israel;

    • Rapporteur: Mr. Nicolas Bérend, ONERA - The French Aerospace Lab, France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Optimization of Low-Energy Resonant Hopping Transfers between Planetary Moons

    15'

    Dr. Gregory Lantoine

    Jet Propulsion Laboratory

    United States

    2

    Through Optimization of Branching Injection Trajectories by the Pontryagin Maximum Principle using Stochastic Models

    15'

    Dr. Olga Yanova

    Central AeroHydrodynamic Institute (TsAGI)

    Russian Federation

    3

    MGA trajectory planning with an ACO-inspired algorithm

    15'

    Dr. Matteo Ceriotti

    University of Glasgow

    United Kingdom

    4

    Optimal Earth-to-Moon trajectories with combined impulse/low thrusters

    15'

    Dr. Donghun Lee

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    6

    Optimal interception of optimally evasive spacecraft

    15'

    Dr. Mauro Pontani

    Sapienza University of Rome

    Italy

    7

    GRAVITY-ASSISTED MANEUVERS APPLIED IN THE MULTIOBJECTIVE OPTIMIZATION OF INTERPLANETARY TRAJECTORIES

    15'

    Dr. Evandro Marconi Rocco

    National Institute for Space Research - INPE

    Brazil

    8

    Multi-object and multi-constraint trajectory optimization for hypersonic reentry gliding vehicle

    15'

    Dr. chen xiaoqing

    China

    9

    A New Optimized Approach for Ballistic Capture to the Moon utilizing Low Thrust Propulsion

    15'

    Dr. Junichiro Kawaguchi

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    10

    direct trajetory optimization of a soft lunar landing considering a landing site

    15'

    Mr. Bong-Gyun Park

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of