• Home
  • IAC Papers Archive
  • Public Website
  • My papers
  • Home
  • event
  • IAC-15
  • C1
  • IP
  • session IP

    Title

    Interactive Presentations

    Date

    2015-10-14

    Time

    13:15

    IPC members
    • Coordinator: Dr. Alfred Ng, Canadian Space Agency, Canada;

    • Coordinator: Prof. Anna Guerman, Centre for Mechanical and Aerospace Science and Technologies (C-MAST), Portugal;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    2

    an improved shape-based method using fourier series for low-thrust orbit design

    confirmed

    Ms. Shiping Xing

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

    China

    3

    Guide star catalog for satellite attitude estimation

    confirmed

    Dr. Ivan Kruzhilov

    Russian Federation

    4

    DYNAMICS OF ORBITS FOR SPACE MISSIONS TAKING INTO ACCOUNT A DISTURBING BODY IN AN ELLIPTICAL-INCLINATED ORBIT: APPLICATIONS TO PLANETARY MOONS

    confirmed

    Mr. Josué Cardoso dos Santos

    São Paulo State University - Universidade Estadual Paulista (UNESP)

    Brazil

    5

    Shorter rotation path design in under-actuated wheel spacecraft

    withdrawn

    Prof. Hwa-Suk Oh

    Korea Aerospace University

    Korea, Republic of

    6

    Modeling and direct adaptive control of a manipulator with variable-speed control moment gyroscopes

    withdrawn

    Mr. Shiyuan Jia

    Beihang University

    China

    7

    Study on the system of a novel space borne ultra-quiet platform of double drag-free based on the electrostatic levitation

    withdrawn

    Dr. DA FAN

    China Academy of Space Technology (CAST)

    China

    8

    A Ground Attitude Analysis Method of the LEO Satellite employing large-scale Rotating Instruments

    confirmed

    Dr. Jie Liu

    China Academy of Space Technology (CAST)

    China

    9

    Constraints Handling Method in Indirect Trajectory Optimization for Manned Asteroid Exploration

    confirmed

    Mr. Anyi Huang

    State Key Laboratory of Astronautic Dynamics (ADL), affiliated to Xi’an Satellite Control Center, Xi’an

    China

    11

    Implementation, Tests and Characterization Results for CubeSat ADCS

    confirmed

    Mr. Stefano Rossi

    Swiss Space Center

    Switzerland

    12

    A NOVEL ATTITUDE QUATERNION FILTER FOR THE ESA EUROPEAN STUDENT EARTH ORBITER (ESEO)

    confirmed

    Mr. Martijn Geers

    Technical University Delft, Faculty of Aerospace Engineering

    The Netherlands

    13

    Attitude stabilization controller for underatuated spacecrafts based on hierarchical adaptive sliding-mode control

    Dr. li weiming

    Shandong Aerospace Electro-technology Institute

    China

    14

    Useful alternative parameterization of an orbital state vector with application to formations of LEO satellites

    confirmed

    Dr. Eran Rosenthal

    IAI MBT Space

    Israel

    15

    A MONOCULAR-BASED RELATIVE POSITION AND ATTITUDE FILTERING FOR UNKNOWN TARGETS

    confirmed

    Mr. Liang Song

    China Academy of Space Technology (CAST)

    China

    16

    Analytic parametrisation of periodic orbits around the rotational equilibria of an asteroid perturbed by Sun gravity and radiation pressure

    withdrawn

    Dr. marta ceccaroni

    Università degli Studi di Roma "Tor Vergata"

    Italy

    17

    Relative orbital motion analysis using dual Lie algebra representations

    confirmed

    Prof.Dr. Daniel Condurache

    Technical University of Iasi

    Romania

    18

    PANGU-4 Simulation Tool for the Testing of Vision-Based Navigation for Planetary Landers

    withdrawn

    Prof. Steve Parkes

    University of Dundee

    United Kingdom

    19

    robust control and double flexible vibration active suppression of space robot with flexible-link and flexible-joint that used in space station

    confirmed

    Dr. Jie Liang

    China

    20

    The Homoclinic and Heteroclinic Connections of Planar Symmetric Resonant Orbits in the Restricted Three-Body Earth-Moon System

    confirmed

    Mr. Chao Peng

    Chinese Academy of Sciences

    China

    21

    Compact Finite-Difference Method for Planetary Flyby Orbit Design

    confirmed

    Dr. An-Ming Wu

    National Space Organization

    Taiwan, China