TY - JOUR
T1 - Consensus control for relative configuration maintenance of large-scale LEO constellations
AU - Zuo, Xiaoyu
AU - Li, Ke
AU - Yang, Ziyuan
AU - Chen, Lin
N1 - Publisher Copyright:
© 2025 COSPAR. Published by Elsevier B.V. All rights are reserved, including those for text and data mining, AI training, and similar technologies.
PY - 2026/6/1
Y1 - 2026/6/1
N2 - Relative configurations of large-scale Low Earth Orbit constellations are susceptible to drift under initial insertion errors and long-term perturbations, rendering scalable and robust maintenance control both crucial and challenging. Conventional methods based on global optimization or reference satellites encounter prohibitive computational complexity and heavy communication loads, particularly at mega-constellation scales. Moreover, the strongly nonlinear nature of orbital dynamics poses additional difficulties for controller design and stability analysis. To overcome these limitations, this paper introduces a fully distributed consensus-based control framework that relies exclusively on local inter-satellite information. Orbital dynamics accounting for multiple perturbations, including Earth’s non-spherical gravity, atmospheric drag, and third-body effects from the Sun and Moon, are embedded within a graph-theoretic network model. A sliding-mode consensus controller is designed for both continuous- and discrete-time systems, and its global asymptotic stability is rigorously established through Lyapunov analysis. To enhance robustness against unmodeled disturbances, a radial basis function neural network is incorporated for adaptive compensation, along with a systematically derived weight update law and corresponding stability proof. Simulations of a 50,000-satellite constellation demonstrate rapid convergence of relative drifts within tight bounds, minimal steady-state control effort, and scale-independent computational complexity, validating the effectiveness and scalability of the proposed framework for maintaining relative configurations in large-scale LEO constellations.
AB - Relative configurations of large-scale Low Earth Orbit constellations are susceptible to drift under initial insertion errors and long-term perturbations, rendering scalable and robust maintenance control both crucial and challenging. Conventional methods based on global optimization or reference satellites encounter prohibitive computational complexity and heavy communication loads, particularly at mega-constellation scales. Moreover, the strongly nonlinear nature of orbital dynamics poses additional difficulties for controller design and stability analysis. To overcome these limitations, this paper introduces a fully distributed consensus-based control framework that relies exclusively on local inter-satellite information. Orbital dynamics accounting for multiple perturbations, including Earth’s non-spherical gravity, atmospheric drag, and third-body effects from the Sun and Moon, are embedded within a graph-theoretic network model. A sliding-mode consensus controller is designed for both continuous- and discrete-time systems, and its global asymptotic stability is rigorously established through Lyapunov analysis. To enhance robustness against unmodeled disturbances, a radial basis function neural network is incorporated for adaptive compensation, along with a systematically derived weight update law and corresponding stability proof. Simulations of a 50,000-satellite constellation demonstrate rapid convergence of relative drifts within tight bounds, minimal steady-state control effort, and scale-independent computational complexity, validating the effectiveness and scalability of the proposed framework for maintaining relative configurations in large-scale LEO constellations.
KW - Consensus control
KW - Discrete time
KW - Large-scale constellation
KW - RBF neural network
KW - Relative configuration maintenance
UR - https://www.scopus.com/pages/publications/105025207641
U2 - 10.1016/j.asr.2025.11.030
DO - 10.1016/j.asr.2025.11.030
M3 - 文章
AN - SCOPUS:105025207641
SN - 0273-1177
VL - 77
SP - 11234
EP - 11251
JO - Advances in Space Research
JF - Advances in Space Research
IS - 11
ER -