session 9

Title: Modelling and Orbit Determination
Description: This session will address aspects of space debris orbit determination related to assessment of raw and derived data accuracy, optical measurements processing and modelling and risk analysis of space debris
Date: 2014-10-01
Time: 14:45
Room: 801B

IPC members

Co-Chair: Dr. Heather Cowardin, Jacobs Technology, ESCG, United States;
Co-Chair: Mr. Sven Kevin Flegel, European Space Agency (ESA), Germany;
Rapporteur: Dr. Hugh G. Lewis, University of Southampton, United Kingdom;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		Observation and analysis of the apparent spin period variations of inactive box-wing geosynchronous resident space objects	accepted	18'	confirmed	Mr. Michael Earl	Royal Military College	Canada
2		Results of two year dedicated Molniya-type HEO surveys	accepted	18'	confirmed	Dr. Vladimir Agapov	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
3		an orbit determination method of improving parameters by the track direction error based on sparse observation data	accepted	18'	no-show	Mr. Dongxu Xing	BITTT	China
4		Orbit determination of space debris using a bi-static radar configuration with a multiple-beam receiver	accepted	18'	confirmed	Mr. Alessandro Morselli	Politecnico di Milano	Italy
5		Analysis of Assumptions in Debris Environment Evolution Models	accepted	18'	confirmed	Dr. David Finkleman	SkySentry, LLC	United States
6		Disposal strategy for the geosynchronous orbits of the Beidou Navigation Satellite System	accepted	18'	confirmed	Dr. Jingshi Tang	Nanjing University	China
7		Reevaluation of the MASTER-2009 MLI and H-10 Debris Modeling	accepted	18'	confirmed	Mr. Sven Kevin Flegel	Fraunhofer Institute for High Frequency Physics and Radar Techniques (FHR)	Germany
8		A deformation model of flexible, high area-to-mass ratio debris for accurate propagation under perturbations	accepted	18'	confirmed	Mr. Sittiporn Channumsin	School of Engineering, University of Glasgow	United Kingdom
9		Re-entry of spacecraft on highly eccentric orbits - Cluster-II	accepted	18'	confirmed	Mr. Ronny Kanzler	Hypersonic Technology Göttingen	Germany
10		Orbital debris atmospheric re-entry prediction	accepted	18'	confirmed	Dr. Jean-Luc VERANT	Office National d’Etudes et de Recherches Aérospatiales (ONERA)	France
–		Contribution of Ariane H-10 fragmentations to the GTO debris environment	Merged with 21719			Mr. Sven Kevin Flegel	Fraunhofer Institute for High Frequency Physics and Radar Techniques (FHR)	Germany