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  • session 1

    Title

    Mission Design, Operations and Optimization - Part 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

    2011-10-03

    Time

    15:00

    Room

    TS-04

    IPC members
    • Chairman: Mr. Nicolas Bérend, ONERA - The French Aerospace Lab, France;

    • Chairman: Prof. Yury Razoumny, RUDN University, Russian Federation;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Trajectory Tour of the Trojan Asteroids Generated via an Optimal Low-Thrust Algorithm

    15

    confirmed

    Mr. Jeffrey Stuart

    Purdue University

    United States

    2

    Optimum design of power-limited propulsion systems with application to fast Earth-to-Mars transfer

    15

    confirmed

    Mr. Nicolas Bérend

    Office National d’Etudes et de Recherches Aérospatiales (ONERA)

    France

    3

    A study of the Accessibility to Asteroids for IKAROS Mission after Venus Flyby

    15

    confirmed

    Dr. masaki nakamiya

    Kyoto University

    Japan

    4

    Nonlinear optimization in space applications with worhp

    15

    confirmed

    Mr. Tim Nikolayzik

    University of Bremen

    Germany

    5

    Fuel-Optimal Low-Thrust Trajectory Optimization of Multiple Asteroid Exploration Missions

    15

    no-show

    Dr. Yang Chen

    Tsinghua University

    China

    6

    Trajectory Optimization of Air-launched rockets via Direct Collocation Method

    15

    withdrawn

    Dr. Mauro Pontani

    Sapienza University of Rome

    Italy

    7

    Mission Analysis of Robotic, Low-Thrust Missions to the Martian Moons Deimos and Phobos

    15

    confirmed

    Mr. Uwe Derz

    EADS Astrium Space Transportation GmbH

    Germany

    8

    Trajectory Design in Proximity of Mars for Round-Trip Missions

    15

    withdrawn

    Mr. Cyrus Foster

    NASA Ames Research Center

    United States

    9

    Mission Design and Analysis for a Laser Occultation Demonstration Mission

    15

    confirmed

    Mr. Matthias Renard

    Deimos Space S.L.

    Spain

    10

    Continuous Low-Thrust Trajectory Optimization Based on a Symplectic Conservative Perturbation Method

    15

    no-show

    Dr. liu luhua

    National University of Defense Technology

    China

    11

    Design of optimal Earth pole-sitter transfers using low-thrust propulsion

    15

    confirmed

    Dr. Jeannette Heiligers

    University of Strathclyde

    United Kingdom

    12

    Optimal bi-impulsive Earth-Moon transfers

    15

    confirmed

    Dr. Francesco Topputo

    Politecnico di Milano

    Italy