IAF Digital Library

9

session 9

Title: Orbit Determination and Propagation
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: 2016-09-28
Time: 14:45
Room: Salon Jalisco E7

IPC members

Co-Chair: Prof.Dr. Heiner Klinkrad, European Space Agency (ESA), Germany;
Co-Chair: Prof. Moriba Jah, Privateer Space, Inc., United States;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Improving the Orbit Propagation Accuracy of Two-Line-Element Satellite Data	18	confirmed	Mr. Jullian Rivera	Rutgers, The State University of New Jersey	United States
2		The effect of earth radiation pressure on the long term orbit of space debris	18	withdrawn	Dr. Stuart Grey	University College London (UCL)	United Kingdom
3		Analysis of the coupled orbit and attitude dynamics of space debris in Geostationary Earth Orbit	18	withdrawn	Mrs. CLEMENCE LE FEVRE	CNES	France
4		Probabilistic Orbit Determination for Real-time Multi-Modality Data Fusion	18	withdrawn	Prof. David B. Spencer	Pennsylvania State University	United States
5		Associating optical measurements of geocentric objects with a Genetic Algorithm: application to experimental data.	18	confirmed	Mr. Michiel Zittersteijn	Astronomical Institute University of Bern (AIUB)	Switzerland
6		Mapping Sensors Measurements to Resident Space Objects Energy and State Parameters Space via Extreme Learning Machines	18	confirmed	Prof. Roberto Furfaro	University of Arizona	United States
7		On the performance analysis of Initial Orbit Determination algorithms	18	confirmed	Mr. Juan Carlos Dolado Perez	Centre National d'Etudes Spatiales (CNES)	France
8		ANALYSIS OF THE ORBIT DETERMINATION ACCURACY USING LASER RANGES AND ANGULAR MEASUREMENTS	18	confirmed	Mr. Emiliano Cordelli	Astronomical Institute University of Bern (AIUB)	Switzerland
9		Space debris population on the LARES satellite orbit	18	confirmed	Dr. Giampiero Sindoni	Sapienza University of Rome	Italy
10		the trivial solution problem and a solvable method of initial orbit determination using Space-based angle-only measurements	18	confirmed	Dr. Qingbo Gan	Academy of Opto-Electronics, Chinese Academy of Sciences	China