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  • session 1

    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.

    Date

    2019-10-21

    Time

    15:00

    Room

    150A

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

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

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:00

    Riemannian optimization for spacecraft trajectory design

    15

    confirmed

    Mr. Kyosuke Asaki

    Kyushu University

    Japan

    2

    15:15

    Low-thrust Trajectory Optimisation through Differential Dynamic Programming Method based on Keplerian Orbital Elements

    15

    confirmed

    Mr. Marco Nugnes

    Politecnico di Milano

    Italy

    3

    15:30

    Concepts and Applications of Aerodynamic Attitude and Orbital Control for Spacecraft in Very Low Earth Orbit

    15

    confirmed

    Ms. Sabrina Livadiotti

    The University of Manchester

    United Kingdom

    4

    15:45

    FLEX tandem with Sentinel-3

    15

    confirmed

    Mrs. Itziar Barat

    ESA - European Space Agency

    The Netherlands

    5

    16:00

    New Earth Observation Multi-Satellite Mission Concepts and Space Architectures for Disaster Risk Reduction

    15

    confirmed

    Ms. Stefania Cornara

    Deimos Space S.L.

    Spain

    6

    16:15

    optimization of transfer schemes between passive space objects in geo vicinity

    15

    confirmed

    Dr. Andrey Baranov

    Keldysh Institute of Applied Mathematics of RAS

    Russian Federation

    7

    16:30

    constraint analysis for servicing co-located satellites

    15

    confirmed

    Mr. Manwei Chan

    Massachusetts Institute of Technology (MIT)

    United States

    8

    16:45

    Trajectory Optimization Using Mixed Minimum-Error and Minimum-Fuel Cost Functions

    15

    confirmed

    Ms. Erica Jenson

    University of Colorado Boulder

    United States

    9

    17:00

    Trajectory optimization in the Three-body problem for a lunar transportation system

    15

    confirmed

    Mr. Mauro Viturro Balufo

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

    France

    10

    17:15

    Low-Thrust Trajectory Design for a Cislunar CubeSat Leveraging Structures from the Bicircular Restricted Four-Body Problem

    15

    confirmed

    Mr. Robert Pritchett

    Purdue University

    United States

    11

    17:30

    Mission Design for Close-range Lunar Mapping by Quasi-Frozen Orbits

    15

    confirmed

    Mr. Sandeep Singh

    Texas A&M University

    United States

    12

    17:45

    Formation Reconfiguration and Science Planning Architecture for the IRASSI Space Interferometer

    15

    confirmed

    Ms. Luisa Buinhas

    Bundeswehr University Munich

    Germany

    *

    Orbital insertion around Phobos via ballistic capture and its application to the Martian Moons eXploration mission

    withdrawn

    Dr. Diogene Alessandro Dei Tos

    Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)

    Japan