The University of Southampton
University of Southampton Institutional Repository

Stochastic Bayesian model updating to reduce epistemic uncertainty in satellite attitude propagation

Stochastic Bayesian model updating to reduce epistemic uncertainty in satellite attitude propagation
Stochastic Bayesian model updating to reduce epistemic uncertainty in satellite attitude propagation

The tracking of space assets within increasingly populated orbits is a critical task in the pursuit of safe space operations; however, with limited observations the gaps in time series data must be filled by numerical attitude simulation models. In practice, given the non-linear nature of spacecraft dynamics and uncertain space disturbances, such simulations can be prone to deviating from the true underlying dynamics. In this work, we follow the approach adopted by the stochastic model updating community, where model discrepancy is accounted for by uncertain model parameters. Working from limited prior data due to sparsity and cost, such system parameters can be hard to define with a precise distribution and are left defined by epistemic uncertainty formulations. We propose an extension of the stochastic model updating scheme, which follows the basic foundational principles of likelihood and Maximum Likelihood Estimation to reduce the amount of epistemic uncertainty attached to model parameters in time-domain models. Compared to current stochastic model updating approaches, our new methodology avoids the use of Approximate Bayesian Computation while also being able to operate in an online fashion. The application of such an approach is demonstrated against a satellite attitude propagator with initially epistemic uncertain moments of inertia to highlight the reduction in parameter uncertainty as measurements arrive.

American Institute of Aeronautics and Astronautics
Smith, Ewan B.
342540d0-fff3-4426-b3cd-7bb7fa8ea6b6
Bi, Si Feng
93deb24b-fda1-4b18-927b-6225976d8d3f
Feng, Jinglang
9b759f87-98b1-4e40-8ccb-adffb22c46f8
Cavallari, Irene
8153726f-15e1-4ef2-b09d-ab6d835e6440
Vasile, Massimiliano
de6550cb-82fc-49eb-b90b-dffa9787bf7d
Smith, Ewan B.
342540d0-fff3-4426-b3cd-7bb7fa8ea6b6
Bi, Si Feng
93deb24b-fda1-4b18-927b-6225976d8d3f
Feng, Jinglang
9b759f87-98b1-4e40-8ccb-adffb22c46f8
Cavallari, Irene
8153726f-15e1-4ef2-b09d-ab6d835e6440
Vasile, Massimiliano
de6550cb-82fc-49eb-b90b-dffa9787bf7d

Smith, Ewan B., Bi, Si Feng, Feng, Jinglang, Cavallari, Irene and Vasile, Massimiliano (2024) Stochastic Bayesian model updating to reduce epistemic uncertainty in satellite attitude propagation. In AIAA SCITECH 2024 Forum. American Institute of Aeronautics and Astronautics.. (doi:10.2514/6.2024-0200).

Record type: Conference or Workshop Item (Paper)

Abstract

The tracking of space assets within increasingly populated orbits is a critical task in the pursuit of safe space operations; however, with limited observations the gaps in time series data must be filled by numerical attitude simulation models. In practice, given the non-linear nature of spacecraft dynamics and uncertain space disturbances, such simulations can be prone to deviating from the true underlying dynamics. In this work, we follow the approach adopted by the stochastic model updating community, where model discrepancy is accounted for by uncertain model parameters. Working from limited prior data due to sparsity and cost, such system parameters can be hard to define with a precise distribution and are left defined by epistemic uncertainty formulations. We propose an extension of the stochastic model updating scheme, which follows the basic foundational principles of likelihood and Maximum Likelihood Estimation to reduce the amount of epistemic uncertainty attached to model parameters in time-domain models. Compared to current stochastic model updating approaches, our new methodology avoids the use of Approximate Bayesian Computation while also being able to operate in an online fashion. The application of such an approach is demonstrated against a satellite attitude propagator with initially epistemic uncertain moments of inertia to highlight the reduction in parameter uncertainty as measurements arrive.

This record has no associated files available for download.

More information

e-pub ahead of print date: 4 January 2024
Published date: 4 January 2024
Venue - Dates: AIAA SciTech Forum and Exposition, 2024, , Orlando, United States, 2024-01-08 - 2024-01-12

Identifiers

Local EPrints ID: 490840
URI: http://eprints.soton.ac.uk/id/eprint/490840
PURE UUID: fdb8dd23-52c5-489e-82b4-7619307072d4
ORCID for Si Feng Bi: ORCID iD orcid.org/0000-0002-8600-8649

Catalogue record

Date deposited: 06 Jun 2024 17:17
Last modified: 20 Jun 2024 02:06

Export record

Altmetrics

Contributors

Author: Ewan B. Smith
Author: Si Feng Bi ORCID iD
Author: Jinglang Feng
Author: Irene Cavallari
Author: Massimiliano Vasile

Download statistics

Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.

View more statistics

Atom RSS 1.0 RSS 2.0

Contact ePrints Soton: eprints@soton.ac.uk

ePrints Soton supports OAI 2.0 with a base URL of http://eprints.soton.ac.uk/cgi/oai2

This repository has been built using EPrints software, developed at the University of Southampton, but available to everyone to use.

We use cookies to ensure that we give you the best experience on our website. If you continue without changing your settings, we will assume that you are happy to receive cookies on the University of Southampton website.

×