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  • C1
  • 4
  • session 4

    Title

    Mission Design, Operations & Optimization (1)

    type

    oral

    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.

    IPC members
    • Co-Chair: Dr. Richard Epenoy, Centre National d'Etudes Spatiales (CNES), France;

    • Co-Chair: Prof. Massimiliano Vasile, University of Strathclyde, United Kingdom;

    • Rapporteur: Prof. Yury Razoumny, RUDN University, Russian Federation;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Closing the Loop Between Mission Design and Navigation Analysis

    10

    confirmed

    Mr. Cristian Greco

    University of Strathclyde

    United Kingdom

    2

    On the use of A* Search for Active Debris Removal Mission Planning

    10

    confirmed

    Mr. Lorenzo Federici

    Sapienza University of Rome

    Italy

    5

    A multi-layer temporal network model of the space environment

    10

    confirmed

    Mr. Giacomo Acciarini

    University of Strathclyde

    United Kingdom

    6

    Cycler orbit design using low-thrust in the Sun-Earth-Moon system

    10

    confirmed

    Mr. miyahara keitaro

    Kyushu University

    Japan

    8

    Low-Thrust Trajectory Optimization for Cubesat Lunar Mission: HORYU-VI

    10

    confirmed

    Dr. Omer Burak Iskender

    Nanyang Technological University

    Singapore, Republic of

    10

    Multi-Objective Optimization for Low Thrust Spiral Trajectory of DESTINY+

    10

    confirmed

    Dr. Takayuki Yamamoto

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    12

    A new approach to low-thrust perturbed trajectory optimization based on the use of complex dual numbers

    10

    confirmed

    Dr. Viacheslav Petukhov

    RIAME

    Russian Federation

    13

    Low-thrust microspacecraft delivery to a lunar orbit after the launch to GTO or MEO

    10

    confirmed

    Dr. Maksim Shirobokov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    16

    A low-cost Earth-Moon-Mars mission using a microsatellite platform

    10

    confirmed

    Prof. Filippo Graziani

    G.A.U.S.S. Srl

    Italy