IAF Digital Library

6

session 6

Title: Orbital Dynamics (1)
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 natural orbital dynamics of spacecraft in the Solar System. It also covers advances in orbit determination.
Date: 2016-09-29
Time: 09:45
Room: Salon Jalisco E6

IPC members

Co-Chair: Prof. Daniel Scheeres, Colorado Center for Astrodynamics Research, University of Colorado, United States;
Co-Chair: Prof. Filippo Graziani, G.A.U.S.S. Srl, Italy;
Rapporteur: Prof. Gerard Gomez, University of Barcelona, Spain;
Rapporteur: Dr. Simei Ji, Beijing Institute of Technology, China;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Preliminary Results on the Dynamics of Large and Flexible Space Structures in Halo Orbits	15'	confirmed	Mr. Andrea Colagrossi	Politecnico di Milano	Italy
2		DYNAMICS OF SPACECRAFT ORBITAL MOTION AROUND ASTEROID APOPHIS	15'	confirmed	Ms. Anqi Lang	N.E. Bauman Moscow State Technology University	Russian Federation
3		Long-Term Orbit Propagation Using Symplectic Integration Algorithms	15'	confirmed	Prof. David B. Spencer	Pennsylvania State University	United States
4		transfers between libration point orbits using lunar gravity assist	15'	confirmed	Dr. Rui Zhong	Beijing University of Aeronautics and Astronautics (BUAA)	China
5		Influence of tether deployment on the atmospheric stage of tether-assisted payload return mission from elliptical orbit	15'	confirmed	Dr. Alexander Ledkov	Samara National Research University (Samara University)	Russian Federation
6		An Accurate and Robust Method for Interplanetary Orbit Design	15'	confirmed	Dr. An-Ming Wu	National Space Organization	Taiwan, China
7		Orbital dynamics of a solar sail accelerated by thermal desorption of coatings	15'	confirmed	Prof. Roman Ya. Kezerashvili	New York City College of Technology, The City University of New York	United States
8		Effectiveness of KS elements in orbit prediction using Earth's Gravity, Drag and Solar Radiation Pressure	15'		Dr. Xavier James Raj	Indian Space Research Organization (ISRO)	India
9		Using Equinoctial Orbital Elements and Quasi-average Element Method to Construct Analytical Solutions for Geostationary Satellite	15'	confirmed	Mr. Bin Liu	Nanjing University	China
10		artificial satellites orbiting planetary satellites: critical inclination and helio-synchronous orbits	15'	confirmed	Prof. Rodolpho V. Moraes	Federal University of São Paulo (UNIFESP)	Brazil
11		Analysis of the influence of area-to-mass ratio error on the orbital motion of a solar power satellite	15'	confirmed	Prof. Gianmarco Radice	University of Glasgow	United Kingdom
12		A heuristic strategy to compute ensembles of trajectories for 3D low-cost Earth-Moon transfers	15'	confirmed	Dr. Priscilla Sousa Silva	Instituto Tecnológico de Aeronáutica (ITA)	Brazil
13		Solar radiation pressure assisted transfers between lissajous orbits of the Sun-Earth system	15'	confirmed	Dr. Stefania Soldini	JAXA	Japan