IAF Digital Library

9

session 9

Title: Orbital Dynamics (2)
Description: This theme discusses advances in the knowledge of natural motions of objects in orbit around the Earth, planets, minor bodies, Lagrangian points and more generally orbital dynamics of spacecraft in the Solar System. It also covers advances in orbit determination.
Date: 2013-09-27
Time: 13:30
Room: 306A

IPC members

Chairman: Prof. Othon Winter, São Paulo State University - Universidade Estadual Paulista (UNESP), Brazil;
Chairman: Prof. Josep J. Masdemont, Universitat Politecnica de Catalunya (UPC), Spain;
Rapporteur: Dr. Shoji Yoshikawa, Mitsubishi Electric Corporation, Japan;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		out-of-plane extension of resonant encounters for escape and capture	15'	confirmed	Dr. Elisa Maria Alessi	IFAC-CNR	Italy
2		A New Strategy of Designing Low-Thrust Trajectories in Alternate Rotational Coordinates	15'	confirmed	Dr. Junichiro Kawaguchi	Japan Aerospace Exploration Agency (JAXA)	Japan
3		Dynamics of a Spacecraft in the Vicinity of Binary Asteroids	15'	confirmed	Ms. Pamela Woo	McGill University	Canada
4		Orbit Dynamics in the Vicinity of Contact Binary Asteroids	15'	confirmed	Ms. Feng Jinglang	Delft University of Technology (TU Delft), The Netherlands	The Netherlands
5		Linear stability of the relative equilibria of a spacecraft around an asteroid	15'	confirmed	Dr. Yue Wang	Beihang University	Israel
6		Applications of SRP dominated highly non-Keplerian trajectories around minor bodies	15'	confirmed	Dr. Daniel Garcia Yarnoz	Advanced Space Concept Laboratory, University of Strathclyde	United Kingdom
7		Combined Orbit Determination for CE-2 and Toutatis Based on Optical Imaging Data at Fly-by	15'	confirmed	Dr. Songjie HU	1)Science and Technology on Aerospace Flight Dynamics Laboratory, China,2)Beijing Aerospace Control Center, China	China
8		A simulation tool for Space Situational Awareness: Near Earth Objects	15'	confirmed	Ms. Maria Piera Padula	Politecnico di Milano	Italy
9		Switch Points for Highly Eccentric Orbits: Modelling the Occurrences of Sign Changes in the Rate of Change of the Eccentricity	15'	confirmed	Mr. Matthew Bourassa	Carleton Univeristy	Canada
10		Adaptive structures for spacecraft orbit control	15'	confirmed	Ms. Stefania Soldini	University of Southampton	United Kingdom
11		Numerical Approximation of Invariant Manifolds in the Restricted Three-Body Problem	15'	confirmed	Dr. Francesco Topputo	Politecnico di Milano	Italy
12		The Farside Explorer: Mission Analysis - Design and computation of a Quasi Ballistic transfer trajectory to the far side of the Moon	15'	withdrawn	Mr. Andrea Campa	ISAE - Institut Supérieur de l'Aéronautique et de l'Espace	Italy