IAF Digital Library

9

session 9

Title: Orbit Determination and Propagation - SST
type: oral
Description: This session will address every aspect of orbit determination coming from the SST (Space Surveillance and Tracking), related to assessment of raw and derived data accuracy, optical measurements processing and modelling and risk analysis of space debris.
Date: 2024-10-16
Time: 10:15
Room: Brown Hall 3

IPC members

Co-Chair: Dr. Rachit Bhatia, West Virginia University, United States;
Co-Chair: Dr. Paolo Marzioli, Sapienza University of Rome, Italy;
Co-Chair: Mr. Juan Carlos Dolado Perez, Centre National d'Etudes Spatiales (CNES), France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	Satellite Swarm Surveillance for Precise Orbit Determination and Guidance Design in Rendezvous Trajectory with Uncooperative Manoeuvring Target in Space	15	confirmed	Ms. Tanya Krishna Kumar	Indian Institute of Technology Kanpur	India
2	10:30	low earth orbit determination using heterogeneous sensor data	15	withdrawn	Ms. Agustina Gascue	Centre National d'Etudes Spatiales (CNES)	France
3	10:45	A Pontryagin Neural Network Application to Tracklets Correlation of Optical Observations	15	confirmed	Mr. Luca Ramponi	Politecnico di Milano	Italy
4	11:00	Analysing the Influence of Photometric Filters on LEO Satellite Orbit Determination	15	confirmed	Dr. Simone Varanese	Sapienza University of Rome	Italy
5	11:15	Recurrent Neural Networks for Resident Space Objects Characterization in MEO and GEO	15	confirmed	Dr. Nicola Cimmino	University of Naples "Federico II"	Italy
6	11:30	Cubesat positioning performance comparison between on-board GNSS, active 1-way ranging and TDOA methods by the Distributed Ground Station Network, and the resulting time from rideshare launch to identification - An operator’s selection help	15	confirmed	Mr. Andreas Hornig	AerospaceResearch.net	Germany
7	11:45	Stochastic integration for re-entry analysis	15	confirmed	Mrs. Aurora Saracini	Politecnico di Milano	Italy
8	12:00	Experimental validation of initial orbit determination and tracklet correlation methods based on admissible regions	15	withdrawn	Mr. Bart Kieboom	Airbus Defence and Space - Space Systems	Germany
9	12:15	A model framework for high-accuracy, short- and long-term orbit determination and propagation of Cislunar space debris, with realistically quantified uncertainties	15	confirmed	Mr. Daan Witte	Technical University Delft, Faculty of Aerospace Engineering	The Netherlands
10	12:30	Range and Doppler enabled initial orbit determination with LeoLabs radars	15	confirmed	Prof. Roberto Armellin	The University of Auckland	New Zealand