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外部干扰与状态约束下卫星姿态系统预设性能跟踪控制

林泽楷 万敏 李涛

河南理工大学学报(自然科学版)2026,Vol.45Issue(5):60-70,11.
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河南理工大学学报(自然科学版)2026,Vol.45Issue(5):60-70,11.DOI:10.16186/j.cnki.1673-9787.2025120018

外部干扰与状态约束下卫星姿态系统预设性能跟踪控制

Prescribed performance tracking control for a satellite attitude control system under external disturbances and state constraints

林泽楷 1万敏 1李涛1

作者信息

  • 1. 南京航空航天大学 自动化学院,江苏 南京 211106
  • 折叠

摘要

Abstract

Objectives To achieve accurate tracking of reference trajectories,this study investigates the atti-tude tracking control problem for a satellite attitude control system subject to external disturbances,perfor-mance constraints,and state constraints.Methods A prescribed performance anti-disturbance control scheme is proposed based on improved prescribed performance control(PPC),disturbance observer-based control(DOBC),and barrier Lyapunov function(BLF)techniques.First,a finite-time performance func-tion with a slow-fast-slow convergence characteristic is designed to dynamically adjust convergence rates in different response stages,thereby improving transient and steady-state performance.Second,a prescribed-time disturbance observer(PTDO)based on a time-scale function is developed to ensure that the estimation error converges to a sufficiently small residual set within a predefined time.Third,the BLF method is employed to transform the constrained satellite attitude system into an equivalent unconstrained system,and a prescribed performance anti-disturbance controller is designed using the backstepping method combined with disturbance estimation.Furthermore,Lyapunov stability theory is applied to derive sufficient conditions guaranteeing uniform boundedness of the closed-loop system,and a coordinated design framework for the controller and observer is established.Finally,numerical simulations are conducted to verify the effectiveness of the proposed method.Results Under external disturbances,the PTDO achieves fast and accurate disturbance estimation and compensation within a predefined time.Meanwhile,the pro-posed controller ensures that the satellite attitude control system satisfies asymmetric time-varying state con-straints,and the attitude tracking error converges within a predefined performance bound.Conclusions Simulation results demonstrate that the proposed method enables high-precision attitude tracking control of satellite systems under external disturbances and complex state constraints.

关键词

卫星姿态系统/跟踪控制/预设性能控制/状态约束/预设时间干扰观测器

Key words

satellite attitude control system/tracking control/prescribed performance control/state con-straints/prescribed time disturbance observer

分类

信息技术与安全科学

引用本文复制引用

林泽楷,万敏,李涛..外部干扰与状态约束下卫星姿态系统预设性能跟踪控制[J].河南理工大学学报(自然科学版),2026,45(5):60-70,11.

基金项目

空间智能控制技术全国重点实验室项目(HTKJ2024KL502021) (HTKJ2024KL502021)

航空科学基金资助项目(2023Z032052001) (2023Z032052001)

河南理工大学学报(自然科学版)

1673-9787

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