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Data-Driven Orbit Determination for Low-Earth Orbit Space Debris Using Ground-Based Measurements

  • Hanyu Liu
  • , Xiucong Sun
  • , Haichao Gui*
  • , Han Cai
  • *Corresponding author for this work
  • Beihang University
  • Ministry of Education in China
  • Beijing Institute of Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Fast and accurate orbit determination for Low-Earth Orbit (LEO) space debris using ground-based measurements presents a significant challenge due to the sparsity of observations, which leads to high nonlinearity. Classical orbit determination methods, such as the Extended Kalman Filter (EKF), Unscented Kalman Filter (UKF), Particle Filter (PF), Gaussian Mixture Filter (GMF), have been widely employed. However, for highly nonlinear systems, the accuracy of EKF and UKF is constrained by linearization errors and the Gaussian assumption, respectively. Moreover, PF and GMF require large number of particles or Gaussian components to achieve sufficient accuracy, resulting in high computational costs. Motivated by recent advancements in deep learning, this study investigates the potential of the data-driven filter in the LEO orbit determination task. The Data-driven Autoregressive nonlinear Filter (DAF), which is proposed recently, has demonstrated promise in handling high nonlinearities. In this paper, we train the DAF using the distance and direction measurements obtained from the ground station for different debris, without access to the true states of the debris. During the inference phase, the DAF relies entirely on the well-trained neural network to estimate the states of debris that are not encountered during training. Simulation results demonstrate that when the system nonlinearity is high enough, our proposed method can achieve higher accuracy compared to the classical filters while offering competitive computational efficiency, as it eliminates the need for numerical integration. To the best of our knowledge, this study represents the first attempt to apply a data-driven filter to orbit determination, providing an alternative to existing methods.

Original languageEnglish
Title of host publication23rd IAA Symposium on Space Debris - Held at the 76th International Astronautical Congress, IAC 2025
PublisherInternational Astronautical Federation, IAF
Pages672-680
Number of pages9
ISBN (Electronic)9798331329273
DOIs
Publication statusPublished - 2025
Externally publishedYes
Event23rd IAA Symposium on Space Debris at the 76th International Astronautical Congress, IAC 2025 - Sydney, Australia
Duration: 29 Sept 20253 Oct 2025

Publication series

NameProceedings of the International Astronautical Congress, IAC
Volume2-F218712
ISSN (Print)0074-1795

Conference

Conference23rd IAA Symposium on Space Debris at the 76th International Astronautical Congress, IAC 2025
Country/TerritoryAustralia
CitySydney
Period29/09/253/10/25

Keywords

  • Orbit determination
  • data-driven
  • nonlinear filter

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