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  • 11
  • session 11

    Title

    Optimization, Guidance and Control

    Date

    2009-10-16

    Time

    10:00

    Room

    Technical Session #3

    IPC members
    • Chairman: Dr. Brij Agrawal, Naval Postgraduate School, United States;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    mission planning for orbital rendezvous using mixed integer nonlinear programming

    15'

    Dr. Jin Zhang

    National University of Defense Technology

    China

    2

    Interplanetary Trajectory Optimization for a SEP Mission to Saturn

    15'

    Mr. Jörn Spurmann

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

    Germany

    3

    Improved Planetary Ephemeris Model for Interplanetary Mission Studies

    15'

    Dr. Rajesh Arora

    Indian Space Research Organization (ISRO)

    India

    4

    Optimization Of Wide-Scope And Rapid Orbital Transfers With Many Burns

    15'

    Mr. Lu Qisheng

    Shanghai Institute of Satellite Engineering

    China

    5

    Optimum Low-Thrust Power Transfer and Rendezvous Between Arbitrary Neighboring Orbits in the Presence of J2 Perturbation

    15'

    Mrs. Juan Zhang

    Northwestern Polytechnical University

    China

    6

    Terminal Area Guidance using the Energy Tube Concept for a Winged Re-entry Vehicle

    15'

    Mr. Sven De Ridder

    Delft University of Technology (TU Delft)

    Belgium

    7

    Lyapunov-based Lunar Capture Guidance Scheme

    15'

    Dr. Dong-Hyun Cho

    KARI

    Korea, Republic of

    8

    Feature Flow and Crater Landmark Based Navigation for Pinpoint Lunar Landing

    15'

    Mr. junhua feng

    Harbin Institute of Technology

    China

    9

    Trajectory Estimation of the Hayabusa Sample Return Capsule Using Optical Sensors

    15'

    Mr. Michael Shoemaker

    Kyushu University

    Japan

    10

    Lisa Pathfinder Attitude and Orbit Control Systems

    15'

    Ms. Luisella Giulicchi

    European Space Agency (ESA)

    The Netherlands

    11

    A fast initial fine alignment algorithm for a strapdown inertial navigation system of a satellite launcher

    15'

    Dr. Eun-Jung Song

    Korea, Republic of