session 9

Title: Orbit Determination and Propagation
type: oral
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: 2017-09-27
Time: 14:45
Room: Hall E1

IPC members

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	14:45	Effects of Thermosphere Total Density Perturbations on LEO Orbits During Severe Conditions Using SLR Data and TLE data sets.	15	confirmed	Dr. Florent Deleflie	Observatoire de Paris	France
2	15:00	Debris Shape Approximation using Ballistic Coefficient Estimation	15	confirmed	Dr. John McVey	The Aerospace Corporation	United States
4	15:30	Bayesian filtering using directional statistics for space debris tracking problem	15	confirmed	Mr. Shambo Bhattacharjee	University of Leeds	United Kingdom
5	15:45	A LED-based Technology to improve the orbit determination of LEO satellite	15	confirmed	Dr. Fabrizio Piergentili	University of Rome "La Sapienza"	Italy
6	16:00	Estimation of orbital parameters of broken-up objects from in-situ debris measurement	15	confirmed	Mr. Yutaka Kodama	Kyushu University	Japan
9	16:45	Analysis of Adaptive Gauss Mixture Unscented Kalman Filter with Sparse Optical Observations for Orbit Determination	15	confirmed	Dr. Yang Yang	RMIT University (Royal Melbourne Institute of Technology)	Australia
10	17:00	Debris Object Orbit Initialization using the Probabilistic Admissible Region with Asynchronous Heterogeneous Observations	15	confirmed	Mr. Waqar Zaidi	Applied Defense Solutions, Inc.	United States
11	17:15	Satellite Orbital Determination using the Desert Fireball Network	15	confirmed	Mr. Trent Jansen-Sturgeon	Curtin University	Australia