A time-sequence Bayesian framework for attitude dynamics model calibration with sparse measurements
Smith, Ewan and BI, Sifeng and Feng, Jinglang (2025) A time-sequence Bayesian framework for attitude dynamics model calibration with sparse measurements. Space: Science & Technology, 5. 0336. ISSN 2692-7659 (https://doi.org/10.34133/space.0336)
Preview |
Text.
Filename: Smith-Bi-Feng-2025-Space-A-time-sequence-Bayesian-framework-for-attitude-dynamics-model.pdf
Final Published Version License:
Download (3MB)| Preview |
Abstract
A precise spacecraft attitude dynamics model is essential for accurately predicting a satellite’s orientation in orbit, with such predictions being centerpiece to mission safety, operational control, and long-term risk management. However, the highly nonlinear nature of spacecraft dynamics, compounded by uncertain and varying space perturbations such as atmospheric drag, solar radiation pressure, and magnetic torques, poses a substantial challenge to model fidelity. The problem is further exacerbated by the limited availability of in-orbit attitude measurements, which constrains direct calibration efforts. This work proposes a Bayesian stochastic model updating framework to systematically calibrate complex attitude dynamics models under epistemic and aleatory uncertainties. The methodology leverages approximate Bayesian computation with Euclidean and Bhattacharyya distance-based likelihoods, integrated within a transitional Markov chain Monte Carlo sampling scheme. A pseudo-online updating process is developed to incorporate sparse, sequential attitude measurements, enabling continual refinement of uncertain model parameters and improved characterization of stochastic dynamics. A numerical case study involving a rigid-body satellite subject to hybrid perturbations is presented to demonstrate the effectiveness of the proposed approach. The results show successful convergence of posterior distributions around true values, a significant reduction in epistemic uncertainty, and an improved predictive capability for attitude propagation in data-sparse scenarios. This framework offers a promising direction for enhancing attitude modeling reliability in the context of increasingly congested and observation-limited space environments.
ORCID iDs
Smith, Ewan
ORCID: https://orcid.org/0009-0002-5961-3461, BI, Sifeng and Feng, Jinglang
ORCID: https://orcid.org/0000-0003-0376-886X;
-
-
Item type: Article ID code: 94011 Dates: DateEvent3 October 2025Published21 August 2025Published Online1 August 2025AcceptedSubjects: Science > Mathematics
Technology > Motor vehicles. Aeronautics. Astronautics > Aeronautics. Aeronautical engineeringDepartment: Faculty of Engineering > Mechanical and Aerospace Engineering Depositing user: Pure Administrator Date deposited: 01 Sep 2025 11:34 Last modified: 07 Aug 2026 06:00 URI: https://strathprints.strath.ac.uk/id/eprint/94011
Tools
Tools






