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  • session 4

    Title

    Mission Design, Operations & 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.

    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, Peoples's Friendship University of Russia, 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

    3

    Low-Thrust Geostationary Orbit Transfer with Minimal Space Radiation Dose

    Mr. Alexander Starchenko

    Research Institute of Applied Mechanics and Electrodynamics (RIAME), MAI

    Russian Federation

    4

    an analytical low-thrust control strategy for large constellation deployment

    withdrawn

    Ms. Simeng Huang

    Politecnico di Milano

    Italy

    4

    Trajectory optimization for constrained semi-low thrust orbit raising: The VIGORIDE case.

    withdrawn

    Mr. Marcello Sciarra

    Deimos Space SLU

    Spain

    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

    7

    LUMIO CubeSat: Phase-A Mission Design and Analysis

    withdrawn

    Dr. Francesco Topputo

    Politecnico di Milano

    Italy

    8

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

    10

    confirmed

    Dr. Omer Burak Iskender

    Nanyang Technological University

    Singapore, Republic of

    9

    Mission Contingency Recovery Options for the Double Asteroid Redirection Test (DART)

    Dr. Bruno Sarli

    The Catholic University of America

    United States

    10

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

    10

    confirmed

    Dr. Takayuki Yamamoto

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    11

    Design of sequence of resonant flybys at Europa through the Flyby map

    Mr. Davide Menzio

    Politecnico di Milano

    Italy

    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

    Prof. Mikhail Ovchinnikov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    15

    Sequence Optimization Method for Large-scale Interplanetary Missions based on Monte Carlo Tree Search

    Mr. Yifei Jiao

    Tsinghua University

    China