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Sequential Filtering Techniques for Simultaneous Tracking and Parameter Estimation

delete2026-02-24
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OA
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Y
Yannick Sztamfater Garcia
J
Joaquı́n Mı́guez
M
Manuel Sanjurjo Rivo
DOI:10.1016/j.ast.2026.111951delete
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Abstract

Abstract

En 中文
• A stochastic formulation of orbital dynamics based on Itô stochastic differential equations is introduced to model unresolved perturbations in orbit determination. • Three hybrid sequential Monte Carlo filtering algorithms are proposed for simultaneous spacecraft state tracking and online estimation of process-noise parameters. • The ensemble Kalman filter and particle filter are extended to jointly infer diffusion coefficients governing propagation uncertainty. • Extensive Monte Carlo simulations in LEO and GEO scenarios demonstrate improved uncertainty realism and competitive accuracy–cost trade-offs. • The proposed framework enables robust tracking with simplified dynamical models while maintaining estimation consistency.
Keywords:
Tracking
sequential filters
particle filters
SMC
parameter estimation
uncertainty propagation
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Journal

Aerospace Science and Technology cover
Aerospace Science and Technology
IF:
5.8
Papers:
1.0W
Citations:
3.0W

Organization

N
northstar earth and space
Scholars:
2
Papers: 2
Citations: 0
U
university carlos iii of madrid
Scholars:
32
Papers: 16
Citations: 0