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  • session 7

    Title

    Mission Design, Operations & Optimization (2)

    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

    2024-10-15

    Time

    10:15

    Room

    Blue Hall 2

    IPC members
    • Co-Chair: Prof. Erick Lansard, Satellite Research Center, Nanyang Technological University (NTU), Singapore, Republic of;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Optimal Low-Thrust Orbit Transfers Connecting Earth, Moon, and Gateway

    15

    confirmed

    Dr. Mauro Pontani

    Sapienza University of Rome

    Italy

    2

    10:30

    Powered Descent Trajectory Design and Guidance Strategy of Chandrayaan-3 Lunar Lander Mission

    15

    confirmed

    Mr. RIJESH M P

    Indian Space Research Organization (ISRO)

    India

    3

    10:45

    A Graph-Aided Design Framework of Low-Energy Transfers

    15

    confirmed

    Dr. Kenta Oshima

    Hiroshima Institute of Technology

    Japan

    4

    11:00

    Cislunar Trajectory Design and Maneuver Autonomy for NASA's Moon to Mars Artchitecture

    15

    confirmed

    Mr. Aaron Houin

    NASA

    United States

    5

    11:15

    Practical Rendezvous Scenario for Logistics Resupply Mission to the Lunar Gateway after NRHO Insertion at the Perilune.

    15

    confirmed

    Ms. Naomi Murakami

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    6

    11:30

    Utilizing Momentum Dumps for KPLO Fine Trajectory Correction in Ballistic Lunar Transfer

    15

    confirmed

    Dr. SeungBum Hong

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    7

    11:45

    lunar navigation constellation design with periodic orbits in earth-moon system by multi-objective optimization

    15

    confirmed

    Mr. Ryusei Komatsu

    The Graduate University of Advanced Studies

    Japan

    8

    12:00

    Interplanetary Transfers by the Automatic Search of Earth and Earth/Moon Resonant Arcs

    15

    confirmed

    Mr. Davide Basso

    European Space Agency (ESA-ESOC)

    Germany

    9

    12:15

    Earth multi-target trajectory design with Artificial Neural Network

    15

    confirmed

    Ms. Anna Barbieri

    Politecnico di Milano

    Italy

    10

    12:30

    Dynamics of Jettison during Earth-to-NRHO Transfers

    15

    confirmed

    Dr. Diane Davis

    National Aeronautics and Space Administration (NASA), Johnson Space Center

    United States

    1*

    10:15

    Advanced optimization method for high-thrust and Weak Stability Boundary End-to-End high-fidelity Earth-Moon trajectories with space manoeuvres

    15

    confirmed

    Mr. Andrea D'Ottavio

    Thales Alenia Space Italia (TAS-I)

    Italy

    2*

    10:30

    Reinforcement Learning for Real-Time Low-Thrust Relative Orbital Rendezvous Design

    15

    confirmed

    Mr. Longwei Xu

    Harbin Institute of Technology

    China

    3*

    10:45

    Reachable Set of Invariant Manifold with Low Thrust

    15

    confirmed

    Dr. Yang Wang

    Nanjing University

    China

    4*

    11:00

    Accelerating Mega-Constellation Design: Efficient Visibility Computation and Multi-Shell Optimisation

    15

    confirmed

    Mr. Vassili Tunjov

    Delft University of Technology (TU Delft)

    The Netherlands

    5*

    11:15

    Vigil – Transfer design for the European Space Agency’s Space Weather Mission to the Sun-Earth Libration Point 5

    15

    confirmed

    Dr. Florian Renk

    European Space Agency (ESA)

    Germany