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  • 4
  • 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

    Date

    2016-09-28

    Time

    09:45

    Room

    Salon Jalisco E6

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

    • Co-Chair: Prof. Kathleen Howell, Purdue University, United States;

    • Rapporteur: Prof. Xiaoqian Chen, National University of Defense Technology, China;

    • Rapporteur: Prof. Massimiliano Vasile, University of Strathclyde, United Kingdom;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    statistical multicriteria evaluation of asteroid deflection methods

    15'

    confirmed

    Mr. Nicolas Thiry

    University of Strathclyde

    United Kingdom

    2

    Kinetic Impactor Mission Design Tool for Near Earth Object Deflection

    15'

    withdrawn

    Mr. Yadvender Singh Dhillon

    International Space University (ISU)

    France

    3

    Robust mission design using invariant manifolds

    15'

    confirmed

    Dr. Lamberto Dell'Elce

    University of Liège

    Belgium

    4

    Orbit Design of a Passive Distributed Radar based on Formation Flying

    15'

    confirmed

    Mr. Salvatore Sarno

    Seconda Università di Napoli

    Italy

    5

    Optimisation of low-thrust and hybrid Earth-Moon transfers

    15'

    confirmed

    Dr. Priscilla Sousa Silva

    Instituto Tecnológico de Aeronáutica (ITA)

    Brazil

    6

    Optimization of interplanetary trajectory of the spacecraft with electric propulsion taking into account the possibility of abnormal operation of the propulsion

    15'

    confirmed

    Prof. Mikhail S. Konstantinov

    Moscow Aviation Institute

    Russian Federation

    7

    Trajectory Optimization for Solar Sail in Cislunar Navigation Constellation with Minimal Lightness Number Control

    15'

    confirmed

    Mr. Hongwen Zhang

    National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an

    China

    8

    Assessment of hybrid propulsion for geostationary transfer orbits: A mission design approach

    15'

    confirmed

    Mr. Simone Ceccherini

    Politecnico di Milano

    Italy

    9

    Method of optimization of the servicing space-based system orbits and detached units maneuveres parameters in the problem of on-orbit-servicing of the given multi-satellite space infrastructure

    15'

    confirmed

    Prof. Yury Razoumny

    Peoples's Friendship University of Russia (RUDN)

    Russian Federation

    10

    Trajectory Design for Saturnian Ocean Worlds Orbiters using Multidimensional Poincaré Maps

    15'

    confirmed

    Dr. Diane Davis

    a.i. solutions, Inc.

    United States

    11

    Advanced methods of low cost mission design for outer planets moons' orbiters and landers

    15'

    confirmed

    Dr. Alexey Grushevskii

    Keldysh Institute of Applied Mathematics of RAS

    Russian Federation

    12

    An approach to estimate the total probability of impact with the Galilean satellites given failure for the Europa Mission

    15'

    confirmed

    Dr. Juan Arrieta

    Nabla Zero Labs

    United States