Electronics and Electrical Engineering and Control

Data-driven predictive control for multi-arm spacecraft after target capture

  • Bicheng CAI ,
  • Siming ZHANG ,
  • Xiaozhe JU ,
  • Yuan LI ,
  • Yong ZHAO
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  • 1.School of Intelligent Sensing and Optoelectronic Engineering,Northeastern University at Qinhuangdao,Qinhuangdao 066003,China
    2.College of Information Science and Engineering,Northeastern University,Shenyang 110819,China
    3.School of Astronautics,Harbin Institute of Technology,Harbin 150006,China
    4.Hangzhou Innovation Institute,Beihang University,Hangzhou 311121,China

Received date: 2025-08-18

  Revised date: 2025-10-16

  Accepted date: 2025-12-31

  Online published: 2026-01-15

Supported by

Young Scientists Fund of the National Natural Science Foundation of China (Category C)(12302055);Research Start-up Funds of Hangzhou International Innovation Institute of Beihang University of China(2024KQ089);State Key Laboratory of Micro-Spacecraft Rapid Design and Intelligent Cluster(MS0124107)

Abstract

This paper aims at realizing the post‑operation maneuvering of multi‑arm spacecraft after capturing non‑cooperative targets. To solve the problem that the combination dynamic parameters are unknown, we propose a Manifold‑constraint‑based Subspace Identification Integral Predictive Control (MSI‑IPC) method, which integrates a Manifold‑constraint‑based Subspace Identification (MSI) module with an Integral Predictive Control (IPC) scheme. By collecting historical input-state data of the multi-arm spacecraft, MSI extracts the inherent structural properties of the state equation parameters as structured constraints, thereby constructing a constraint manifold that enforces adherence to system invariants and enhances state prediction accuracy. IPC utilizes the control input increments as optimization variables within the predictive control problem, effectively suppressing control input chattering. The resulting MSI‑IPC method is applicable to multi‑arm spacecraft in arbitrary open‑loop configurations without requiring knowledge of any dynamic parameters. It overcomes the limitations of conventional indirect subspace predictive control in high‑dimensional, noisy systems, where input chattering often prevents convergence. A formal Input‑to‑State Stability (ISS) proof for the closed‑loop system is provided via Lyapunov analysis. Numerical simulations under measurement noise demonstrate that MSI‑IPC significantly surpasses conventional Indirect Subspace Predictive Control (ISPC) in both state prediction accuracy and control input smoothness, validating the method’s effectiveness and robustness.

Cite this article

Bicheng CAI , Siming ZHANG , Xiaozhe JU , Yuan LI , Yong ZHAO . Data-driven predictive control for multi-arm spacecraft after target capture[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2026 , 47(14) : 632687 -632687 . DOI: 10.7527/S1000-6893.2025.32687

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