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  • C1
  • 8
  • session 8

    Title

    Mission Design, Operations and Optimization (1)

    Description

    The 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

    2014-10-03

    Time

    09:45

    Room

    801A

    IPC members
    • Co-Chair: Prof. Kathleen Howell, Purdue University, United States;

    • Co-Chair: Mr. Vincent Martinot, Thales Alenia Space France, France;

    • Rapporteur: Prof. Filippo Graziani, G.A.U.S.S. Srl, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Bi-objective optimization of a multiple-target active debris removal mission

    15'

    confirmed

    Mr. Nicolas Bérend

    Office National d’Etudes et de Recherches Aérospatiales (ONERA)

    France

    2

    A method for fast, accurate and robust computation of low-thrust transfers between LEO orbits

    15'

    confirmed

    Dr. JORDI FONTDECABA BAIG

    Thales Alenia Space France

    France

    3

    mission design and analysis for irnss-1a

    15'

    no-show

    Mr. Satyendra Singh

    ISRO Satellite Centre (ISAC)

    India

    4

    new technology for the optimization of satellite maneuvers between near-circular orbits for the purposes of various space missions

    15'

    withdrawn

    Mr. Chernov Nikita

    Keldysh Institute of Applied Mathematics of RAS

    Russian Federation

    5

    Variable Specific Impulse Low-thrust Low Thrust Trajectory Optimization Using Homotopic Approach

    15'

    confirmed

    Mr. Junfeng Li

    State Key Laboratory of Astronautic Dynamics (ADL), affiliated to Xi’an Satellite Control Center, Xi’an

    China

    6

    A homotopy-based method for optimization of hybrid high-low thrust trajectories

    15'

    confirmed

    Mr. Nicola Sullo

    University of Glasgow

    United Kingdom

    7

    Application of a Multi-Objective Evolutionary Algorithm to the Spacecraft Stationkeeping Problem

    15'

    confirmed

    Prof. David B. Spencer

    Pennsylvania State University

    United States

    8

    triangular formation flying under the elliptic restricted three-body problem formulation

    15'

    confirmed

    Mr. Fabio Ferrari

    Politecnico di Milano

    Italy

    9

    A survey of different classes of Earth-to-Moon trajectories in the patched three-body approach

    15'

    confirmed

    Dr. Priscilla Sousa Silva

    Instituto Tecnológico de Aeronáutica (ITA)

    Brazil

    10

    Transfer and rendez-vous strategies for the deployment and the servicing of an inhabited space station at Earth-Moon L2

    15'

    confirmed

    Prof. Stéphanie Lizy-Destrez

    SUPAERO- Ecole Nationale Supérieure de l'Aéronautique et de l'Espace

    France

    11

    Optimal Transfers in the Earth-Moon System through Polyhedral Representation of Invariant Manifolds

    15'

    confirmed

    Dr. Mauro Pontani

    Sapienza University of Rome

    Italy

    12

    MOID-Increasing Disposal Strategies for LPO Missions

    15'

    confirmed

    Dr. Elisa Maria Alessi

    IFAC-CNR

    Italy

    13

    quasi-periodic orbits in the vicinity of the sun-earth system l2 point and their implementation in "spectr-rg" and "millimetron" missions

    15'

    confirmed

    Mr. Ivan Ilin

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation