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: 2023-10-03
Time: 10:15
Room: BCC A6

IPC members

Co-Chair: Dr. Jan Siminski, ESA - European Space Agency, Germany;
Co-Chair: Mr. Juan Carlos Dolado Perez, Centre National d'Etudes Spatiales (CNES), France;
Rapporteur: Dr. Paolo Marzioli, Sapienza University of Rome, Italy;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	Latent Forces Model Approach to Observation-Based Space Object State and Uncertainty Propagation	15	withdrawn	Mr. Gleb Beliy	Moscow Institute of Physics and Technology (MIPT)	Russian Federation
2	10:30	improving orbit prediction in LEO with machine learning using exogenous variables	15	confirmed	Mr. Francisco Caldas	Faculdade de Ciências e Tecnologia - UNL	Portugal
3	10:45	enhancement of orbit prediction accuracy using transformer	15	confirmed	Mr. Sajjad Kazemi	University of Waterloo	Canada
4	11:00	GEO Optical Measurement Correlation and Angles-Only Orbit Determination	15	confirmed	Dr. Simone Varanese	Sapienza University of Rome	Italy
5	11:15	Radiative acceleration acting on non-spherical objects in near- Earth space	15	confirmed	Mr. Aleksandr Kuznetsov	Moscow Institute of Physics and Technology (MIPT)	Russian Federation
6	11:30	On a high-performance integrator of the equations of orbital motion of bodies in near-Earth space	15	confirmed	Mr. Ilya Fukin	Moscow Institute of Physics and Technology (MIPT)	Russian Federation
7	11:45	Debris Mitigation and Atmospheric Deorbiting Analysis for Lunar L2 NRHO Departing Spacecraft	15	confirmed	Mrs. Carmela Marika Accettura	Politecnico di Torino	Italy
8	12:00	Evaluating the Accuracy and Robustness of Initial Orbit Determination Methods for SSA in Low Earth Orbit Using Real Observation Data	15	confirmed	Mr. Süleyman Altınışık		Türkiye
9	12:15	Variable Calculation Domain Aerodynamic Numerical Method for Spacecraft Debris Reentry Disintegration	15	confirmed	Mr. Jingjiang Chu	China Academy of Aerospace Aerodynamics (CAAA)	China
10	12:30	Spacecraft Conjunction Assessment optimization using Deep Learning algorithms applied to Conjunction Data Messages (CDMs)	15	confirmed	Mr. Jose Javier Rosales Ruiz	Cranfield University, Cranfiel UK	United Kingdom