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  • session 6

    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.

    Date

    2017-09-28

    Time

    09:45

    Room

    Hall A

    IPC members
    • Co-Chair: Prof. Michèle Lavagna, Politecnico di Milano, Italy;

    • Co-Chair: Prof. Stéphanie Lizy Destrez, SUPAERO- Ecole Nationale Supérieure de l'Aéronautique et de l'Espace, France;

    • Rapporteur: Mr. Vincent Martinot, Thales Alenia Space France, France;

    • Rapporteur: Mr. Johannes Schoenmaekers, European Space Operations Centre, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Novel Piecewise Trajectory Shaping in Hill's Canonical Variables

    15

    confirmed

    Mr. Cristian Greco

    Delft University of Technology (TU Delft)

    The Netherlands

    2

    Indirect optimization of low-thrust Earth-Moon transfers in the Sun-Earth-Moon system

    15

    confirmed

    Dr. Richard Epenoy

    Centre National d'Etudes Spatiales (CNES)

    France

    3

    Costate Scaling for Multi-Rendezvous Low-Thrust Trajectory Optimization

    15

    confirmed

    Mr. Shiyu Chen

    Tsinghua University School of Aerospace

    China

    4

    IRASSI InfraRed Space Interferometer: Mission Analysis, Spacecraft Design and Formation Flying Overview

    15

    confirmed

    Ms. Luisa Buinhas

    Bundeswehr University Munich

    Germany

    5

    N-body boundary value problem solver using monotonic basin hopping with applications to Earth-Moon transfer

    15

    confirmed

    Mr. Weichen Xiao

    The Hong Kong University of Science and Technology

    China

    6

    Time-optimal solar sail heteroclinic connections for an Earth-Mars cycler

    15

    confirmed

    Ms. Merel Vergaaij

    Delft University of Technology (TU Delft)

    The Netherlands

    8

    Approximation by filtering in optimal control and applications to low thrust orbit transfer

    15

    confirmed

    Mr. Thierry Dargent

    Thales Alenia Space France

    France

    9

    Optimisation tool for low thrust orbit raising based on the Sequential Gradient Restoration Algorithm

    15

    confirmed

    Dr. Francesca Letizia

    OHB System AG-Bremen

    Germany

    11

    THE OPTIMAL TRAJECTORY FOR OBSERVING NON-COOPERATIVE TARGET WITH KOZs CONSTRAINTS

    15

    confirmed

    Mr. Junhua Zhang

    National Key Laboratory of Aerospace Flight Dynamic, Northwestern Polytechnical University

    China

    12

    In-Flight Results from the GPS Receiver on SmallGEO

    15

    confirmed

    Dr. Bernard Lübke-Ossenbeck

    OHB System AG-Bremen

    Germany