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  • GLUC-2010
  • 2
  • 2
  • session 2

    Title

    Astrodynamics 

    Date

    2010-05-31

    Time

    15:00

    Room

    Ju Ying Hall - Room 1

    IPC members
    • Chairman: Mr. Trond Krovel, International Space University (ISU), France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Accuracy analysis of orbit determination and prediction for low orbit lunar satellite

    15'

    Ms. Jianrong Chen

    State Key Lab of Astrodynamics

    China

    1

    Attitude realisation with geometric constraints for Chandrayaan - 1

    Poster

    Dr. Ramachandran Mankali

    Indian Space Research Organization (ISRO)

    India

    1

    Prediction of landing point of Chang'e-1 lunar probe

    Poster

    Prof. Jiasong Wang

    State Key Lab of Astrodynamics

    China

    2

    Design of long-lifetime lunar orbits: a hybrid approach

    15'

    Dr. Martin Lara

    Spain

    2

    Time selection and error effects of the last midcourse correction maneuver of the moon-earth transfer trajectory

    Poster

    Ms. AiWu Zheng

    China

    3

    Entry Range and Corridor Analysis for Lunar Return Crew Module

    15'

    Mr. Hong-xin Shen

    National University of Defense Technology

    China

    3

    Gravity-Assist Trajectory Design Considering Orbital Motion in the Lunar Influence Sphere

    Poster

    Dr. Yan Zhang

    DFH Satellite Co. Ltd.

    China

    3

    Suboptimal Low-Thrust Trajectories for Lunar Missions

    Poster

    Dr. Viacheslav Petukhov

    RIAME

    Russian Federation

    4

    INDIA’S FIRST LUNAR MISSION CHANDRAYAAN-1 ORBIT DETERMINATION SYSTEM

    15'

    Dr. Narayanasetti Venkata Vighnesam

    Indian Space Research Organization (ISRO)

    India

    4

    Key Technology and Frame Design of SODAK(Space Orbit Design and Analysis Kit) for Space Exploration

    Poster

    Mr. junfeng wang

    China Academy of Launch Vehicle Technology (CALT)

    China

    4

    The Precise Design of Moon-Earth Trajectories Using Gauss Pseudospectral Method with Mesh Refinement

    Poster

    Dr. hongbo ding

    China

    5

    Landing footprint analysis for lunar return vehicle

    Poster

    Dr. chen hongbo

    The Aerospace Corporation

    China

    5

    lunar artificial satellites:frozen and helio-synchronous orbits

    15'

    Prof. Rodolpho Vilhena de Moraes

    Universidade Federal de SãoPaulo - USP

    Brazil

    5

    Using a Permanent Magnet Hall Thruster along trajectory arcs to orbit control of the lunar polar satellites.

    Poster

    Prof. Jose Leonardo Ferreira

    University of Brasilia

    Brazil

    6

    Lunar gravity and space flights

    Poster

    Prof. Vyacheslav V. Ivashkin

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    6

    Lunar Sample Return Using the Invariant Manifolds and Lunar Flyby

    15'

    Dr. Mingtao Li

    National Space Science Center (NSSC), Chinese Academy of Sciences

    China

    6

    Utilization of the Light Pressure in the Launch of Lunar Probes

    Poster

    Dr. Zhao Yuhui

    Nanjing University

    China

    7

    Modifying the Atlas of Low Lunar Orbits Using Inert Tethers

    Poster

    Dr. Martin Lara

    Spain

    7

    Reentry Trajectory Optimization for Manned Lunar Mission

    15'

    Dr. Min xuelong

    China Academy of Space Technology (CAST)

    China

    8

    SELTO (Space Exploration Landing Trajectory Optimiser): A tool for evaluation and optimisation of descent trajectories

    15'

    Mr. Davide Starnone

    STAR N1 Engineering

    Italy

    9

    Moon-to-Earth Trajectories Design Based on Pseudostate Theory

    15'

    Mr. lei zhang

    China Academy of Space Technology (CAST)

    China

    11

    The Selection of Touchdown Area for the Lunar Sample and Return Mission

    15'

    Dr. Zhanfeng Meng

    China Academy of Space Technology (CAST)

    China

    13

    semi-analytical propagation of satellite orbits about an arbitrary central body

    15'

    Dr. Paul Cefola

    University at Buffalo

    United States