session 1

Title: Orbital Dynamics (1)
Description: This theme discusses advances in the knowledge of natural motions of objects in orbit aroung the Earth, planets, minor bodies, Lagrangian points and more generally natural orbital dynamics of spacecraft in the Solar System. It also covers advances in orbit determination.
Date: 2014-09-29
Time: 15:15
Room: 801A

IPC members

Co-Chair: Mr. Johannes Schoenmaekers, European Space Operations Centre, Germany;
Co-Chair: Prof. Weihua Zhang, National University of Defense Technology, China;
Rapporteur: Dr. Antonio Almeida Prado, INPE, Brazil;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		Station-keeping for quasi-periodic orbits	accepted	15'	confirmed	Mr. Marcel Duering	University of Strathclyde	United Kingdom
2		preliminary results from the lares mission to test general relativity	accepted	15'	confirmed	Prof. Ignazio Ciufolini	Università del Salento	Italy
3		Incorporating the Evolution of Multi-Body Orbits into the Trajectory Trade Space and Design Process	accepted	15'	confirmed	Ms. Amanda Haapala	Purdue University	United States
4		Confinement of spacecraft swarms in J2-perturbed orbits about the Earth	accepted	15'	confirmed	Dr. Laura Garcia-Taberner	Universitat de Girona	Spain
5		Spacecraft’s Resonance Orbit Design and Application Analysis	accepted	15'	confirmed	Prof. Qun Fang	Northwestern Polytechnical University，NPU	China
6		Optimal Control Theory to Dynamic Systems Methods of the Bi-Circular Four Body Problem	accepted	15'	withdrawn	Mr. Ryne Beeson	University of Illinois at Urbana-Champaign	United States
7		Solar Sail Periodic Orbits in the Earth-Moon Three-Body Problem	accepted	15'	confirmed	Dr. Jeannette Heiligers	University of Strathclyde	United Kingdom
8		Evidences of diffusion related to the center manifold of L3 of the SRTBP	accepted	15'	confirmed	Dr. Maisa Terra	Instituto Tecnológico de Aeronáutica (ITA)	Brazil
9		Families of heteroclinic connections between quasi-periodic libration point trajectories	accepted	15'	confirmed	Dr. Josep-Maria Mondelo	Universitat Autonoma de Barcelona	Spain
10		Stable 3-D Tether Structures in Orbit	accepted	15'	withdrawn	Mr. Charles Radley	Leeward Space Foundation	United States
11		Computation of Weakly Stable Structures in the Restricted Three-Body Problem using Differential Algebra Techniques	accepted	15'	withdrawn	Dr. Alexander Wittig	Politecnico di Milano	Italy
12		Combined Aerodynamic and Orbital Trajectories for Partial Drag-free Flight in Super Low Altitude	accepted	15'	confirmed	Dr. Ming Xu	Beihang University	China
13		Natural Configurations for Formation Flying around Triangular Libration Points for the Elliptic and the Bicircular Problem in the Earth-Moon system	accepted	15'	confirmed	Dr. Francisco Salazar	Universidade Estadual Paulista - Grupo de Dinâmica Orbital	Brazil