IAF Digital Library

IP

session IP

Title: Interactive Presentations
type: interactive
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
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
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
Guide star catalog for satellite attitude estimation		confirmed	Dr. Ivan Kruzhilov		Russian Federation
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
Shorter rotation path design in under-actuated wheel spacecraft		withdrawn	Prof. Hwa-Suk Oh	Korea Aerospace University	Korea, Republic of
Modeling and direct adaptive control of a manipulator with variable-speed control moment gyroscopes		withdrawn	Mr. Shiyuan Jia	Beihang University	China
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on the system of a novel space borne ultra-quiet platform of double drag-free based on the electrostatic levitation		withdrawn	Dr.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
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
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
Implementation, Tests and Characterization Results for CubeSat ADCS		confirmed	Mr. Stefano Rossi	Swiss Space Center	Switzerland
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
Attitude stabilization controller for underatuated spacecrafts based on hierarchical adaptive sliding-mode control			Dr. li weiming	Shandong Aerospace Electro-technology Institute	China
Useful alternative parameterization of an orbital state vector with application to formations of LEO satellites		confirmed	Dr. Eran Rosenthal	IAI MBT Space	Israel
A MONOCULAR-BASED RELATIVE POSITION AND ATTITUDE FILTERING FOR UNKNOWN TARGETS		confirmed	Mr. Liang Song	China Academy of Space Technology (CAST)	China
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
Relative orbital motion analysis using dual Lie algebra representations		confirmed	Prof.Dr. Daniel Condurache	Technical University of Iasi	Romania
PANGU-4 Simulation Tool for the Testing of Vision-Based Navigation for Planetary Landers		withdrawn	Prof. Steve Parkes	University of Dundee	United Kingdom
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
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
Compact Finite-Difference Method for Planetary Flyby Orbit Design		confirmed	Dr. An-Ming Wu	National Space Organization	Taiwan, China