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  • session 9

    Title

    Mission Design, Operations and Optimization (2)

    Description

    This theme covers design, operations and optimization of earth-orbiting and interplanetary missions, with emphasis on studies and experiences related to current and future missions.

    Date

    2010-10-01

    Time

    14:00

    Room

    North Hall

    IPC members
    • Chairman: Prof. Eberhard Gill, Delft University of Technology, The Netherlands;

    • Chairman: Prof. Michèle Lavagna, Politecnico di Milano, Italy;

    • Rapporteur: Prof. Kathleen Howell, Purdue University, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Invariant-Manifold, Low-Thrust Transfers to Low Mars Orbits

    15

    confirmed

    Dr. Giorgio Mingotti

    University of Strathclyde

    United Kingdom

    2

    Proposed End-of-Mission for the Cassini Spacecraft: Inner D Ring Ballistic Saturn Impact

    15

    confirmed

    Mr. Brent Buffington

    National Aeronautics and Space Administration (NASA), Jet Propulsion Laboratory

    United States

    3

    Strategy to achieve gravitational capture at Callisto

    15

    confirmed

    Dr. Elisa Maria Alessi

    IFAC-CNR

    Italy

    4

    Orbital Transfer Design between Libration Points around Jovian Satellites

    15

    confirmed

    Mr. Keita Tanaka

    University of Tokyo

    Japan

    5

    Optimised design of a mission to multiple Trojan asteroids fly-bies

    15

    confirmed

    Mr. denis CARBONNE

    Centre National d'Etudes Spatiales (CNES)

    France

    6

    Mission Designs for Solar Probe Plus Enabling Launch Every Year From 2015 Through 2018

    15

    withdrawn

    Dr. Yanping Guo

    The John Hopkins University Applied Physics Laboratory

    United States

    7

    finite-thrust optimization of interplanetary transfers of space vehicle with bimodal nuclear thermal propulsion

    15

    confirmed

    Dr. Oleksii Kharytonov

    Taras Shevchenko National University

    Ukraine

    8

    Incremental Solution of LTMGA Transfers Transcribed with an Advanced Shaping Approach

    15

    confirmed

    Dr. Massimiliano Vasile

    University of Strathclyde

    United Kingdom

    9

    Applications of Multi-Body Dynamical Environments: The ARTEMIS Transfer Trajectory Design

    15

    confirmed

    Mr. David C. Folta

    National Aeronautics and Space Administration (NASA), Goddard Space Flight Center

    United States

    10

    Particle Swarm Optimization Applied to Orbital Transfers

    15

    confirmed

    Dr. Mauro Pontani

    Sapienza University of Rome

    Italy

    11

    a study of the transfer trajectories to halo orbits using stable manifolds considering launch conditions

    15

    confirmed

    Dr. Masaki Nakamiya

    ISAS/JAXA

    Japan

    12

    Deterministic Method for Space Trajectory Design with Mission Margin Constraints

    15

    confirmed

    Dr. Joris Olympio

    European Space Agency (ESA)

    The Netherlands