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  • session 5

    Title

    Mission Design, Operations and Optimisation (2)

    Description

    The theme covers design, operations and optimisation of Earth-orbiting and interplanetary missions, with emphasis on studies and experiences related to current and future missions.

    Date

    2012-10-03

    Time

    15:15

    Room

    TS01 (Sala Aldebaran, Hall 1)

    IPC members
    • Chairman: Dr. David Spencer, The Aerospace Corporation, United States;

    • Chairman: Prof. Yury Razoumny, Peoples's Friendship University of Russia (RUDN), Russian Federation;

    • Rapporteur: Mr. Johannes Schoenmaekers, European Space Operations Centre, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Design of trajectories for continuous polar Earth observation in the Earth-Moon system

    15'

    confirmed

    Dr. Matteo Ceriotti

    University of Glasgow

    United Kingdom

    2

    Innovative method of constellation design to enable new arising applications based on space-airborne bistatic SAR

    15'

    confirmed

    Dr. Maria Daniela Graziano

    CO.RI.S.T.A./Second University of Naples

    Italy

    3

    Optimization of Satellite Constellation Reconfiguration Maneuvers

    15'

    confirmed

    Mr. Leonid Appel

    Technion, I.I.T.

    Israel

    4

    A predictive guidance scheme for soft landing of a lunar module

    15'

    confirmed

    Mr. Nitin Ghatpande

    Indian Space Research Organization (ISRO)

    India

    5

    An extension and numerical analysis of the hohmann spiral transfer

    15'

    confirmed

    Mr. Steven Owens

    Advanced Space Concept Laboratory, University of Strathclyde

    United Kingdom

    6

    MESSENGER at Mercury: From Orbit Insertion to First Extended Mission

    15'

    confirmed

    Mr. James V. McAdams

    Johns Hopkins University Applied Physics Laboratory

    United States

    7

    Orbit selection criteria for optical dual-use earth observation satellites

    15'

    confirmed

    Mr. Alessio Di Salvo

    NEXT Ingegneria dei Sistemi S.p.A.

    Italy

    8

    Optimal Trajectory Design for the Lunar Vertical Landing

    15'

    confirmed

    Dr. Dong-Hyun Cho

    KARI

    Korea, Republic of

    9

    Optimal Long-duration Low-thrust Transfers Between Libration Point Orbits

    15'

    confirmed

    Dr. Richard Epenoy

    Centre National d'Etudes Spatiales (CNES)

    France

    10

    Optimal Spacecraft Trajectories for Flight to Asteroid Apophis with Low Thrust

    15'

    confirmed

    Prof. Vyacheslav V. Ivashkin

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    11

    A novel approach to the generation of multiple gravity assist trajectories

    15'

    withdrawn

    Dr. Elena Fantino

    Universitat Politecnica de Catalunya (UPC)

    Spain

    12

    Low energy trajectory optimization for CE-2’s extended mission after 2012

    15'

    confirmed

    Dr. Mingtao Li

    National Space Science Center (NSSC), Chinese Academy of Sciences

    China

    13

    Gravitational Capture Opportunities for Asteroid Retrieval Missions

    15'

    confirmed

    Dr. Joan Pau Sanchez Cuartielles

    Advanced Space Concept Laboratory, University of Strathclyde

    United Kingdom