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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

    2015-10-12

    Time

    15:15

    Room

    Teddy B (ICC, lower level)

    IPC members
    • Co-Chair: Mr. Johannes Schoenmaekers, European Space Operations Centre, Germany;

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

    • Rapporteur: Prof. Moriba Jah, The University of Texas at Austin, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Philae’s Flight Dynamics challenges: report of the landing on a comet

    16'

    confirmed

    Dr. Elisabet Canalias

    CNES

    France

    2

    Applicability of the Tisserand Criterion for Optimization of Gravity-Assist Sequences for Low-Thrust Missions

    16'

    confirmed

    Mr. Volker Maiwald

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    3

    Survey of Low-Thrust Gravity Assist Trajectory Optimization Methods, with Comparisons to a Novel, Multi-Impulse Discretization Approach

    16'

    confirmed

    Mr. Joshua Fogel

    University of Southern California

    United States

    4

    Initial and final boundaries transformation when solving optimal control problem with averaging techniques and application to low thrust orbit transfer

    16'

    confirmed

    Mr. Thierry Dargent

    Thales Alenia Space France

    France

    5

    Joint Optimization of the Low-Thrust Trajectory and the Main Design Parameters of Electric Propulsion System

    16'

    confirmed

    Dr. Viacheslav Petukhov

    RIAME

    Russian Federation

    6

    low thrust minimum fuel optimization to libration point orbits using variable specific impulse engine

    16'

    withdrawn

    Mr. Hao Zeng

    School of Aerospace Engineering, Beijing Institute of Technology

    China

    7

    Optimal Control of Electric Propulsion Spacetag for Operation of the Near Lunar Infrastructure

    16'

    confirmed

    Prof. Olga Starinova

    Samara State Aerospace University

    Russian Federation

    8

    Low-thrust trajectory design and operations of PROCYON, the first deep-space micro-spacecraft

    16'

    confirmed

    Dr. Stefano Campagnola

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    9

    Optimal 3D Lunar soft landing trajectory design and Performance evaluation of explicit guidance laws

    16'

    no-show

    Mr. Remesh N

    Vikram Sarabhai Space Centre (VSSC)

    India

    10

    Asteroid Retrieval Missions Enabled by Invariant Manifold Dynamics

    16'

    confirmed

    Dr. Joan Pau Sanchez Cuartielles

    Cranfield University

    United Kingdom

    11

    Trajectory Options for the DART Mission

    16'

    confirmed

    Dr. Justin Atchison

    The John Hopkins University Applied Physics Laboratory

    United States