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Filtering Module on Satellite Tracking

Wafi, Moh Kamalul · 2023 · arxiv_oai
arXiv (OAI) · Papers · 2023
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dynamical-systemssystems-and-control
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[2304.04111] An Information-Based Micro-Kalman Filter for Satellite Tracking: A Comparative Study Skip to main content Search Submit Donate Log in Search arXiv Press Enter to search · Advanced search Electrical Engineering and Systems Science > Systems and Control arXiv:2304.04111 (eess) [Submitted on 8 Apr 2023 ( v1 ), last revised 19 Jun 2026 (this version, v3)] Title: An Information-Based Micro-Kalman Filter for Satellite Tracking: A Comparative Study Authors: Moh Kamalul Wafi View a PDF of the paper titled An Information-Based Micro-Kalman Filter for Satellite Tracking: A Comparative Study, by Moh Kamalul Wafi View PDF HTML (experimental) Abstract: Satellite dynamics and tracking remain important challenges in the context of space exploration and communication systems. Accurate state estimation is essential to maintain reliable orbital motion and system performance. This paper presents a mathematical framework for satellite state estimation based on a linearized model described by radial and angular states. The model incorporates two types of measurement noise corresponding to range and scaled angular deviations, which are assumed to be mutually independent with known covariance structures. The estimation problem is formulated using the Kalman filter, together with the associated Algebraic Riccati Equation (ARE), leading to both time-varying and steady-state solutions. In addition, a micro-Kalman filter ($\mu$KF) formulation is considered and compared with the classical Kalman filter, as well as with the extended Kalman filter (EKF), unscented Kalman filter (UKF), and an adaptive Kalman filter under a unified simulation setup. The results demonstrate that the proposed $\mu$KF achieves estimation performance nearly identical to that of the classical Kalman filter and its variants, with small and bounded estimation errors. The mean square estimation error (MSEE) remains low for all state variables under both noise configurations, confirming the effectiveness of the proposed approach for linear Gaussian systems. Comments: This version extends the previous version by including additional simulations, a comparative study with EKF, UKF, and adaptive Kalman filters, and enhanced trajectory visualization Subjects: Systems and Control (eess.SY) ; Dynamical Systems (math.DS) Cite as: arXiv:2304.04111 [eess.SY] (or arXiv:2304.04111v3 [eess.SY] for this version) https://doi.org/10.48550/arXiv.2304.04111 Focus to learn more arXiv-issued DOI via DataCite Submission history From: Moh Kamalul Wafi [ view email ] [v1] Sat, 8 Apr 2023 22:05:11 UTC (1,264 KB) [v2] Wed, 15 Apr 2026 01:38:51 UTC (753 KB) [v3] Fri, 19 Jun 2026 16:54:50 UTC (753 KB) Full-text links: Access Paper: View a PDF of the paper titled An Information-Based Micro-Kalman Filter for Satellite Tracking: A Comparative Study, by Moh Kamalul Wafi View PDF HTML (experimental) TeX Source view license Current browse context: eess.SY < prev | next > new | recent | 2023-04 Change to browse by: cs cs.SY eess math math.DS References & Citations NASA ADS Google Scholar Semantic Scholar export BibTeX citation Loading... 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