Scaling-Transformation-Based Attitude Tracking Control for Rigid Spacecraft With Prescribed Time and Prescribed Bound

被引：27

作者：

Xiao, Yan ^{[1
,2
]}

Yang, Yulong ^{[3
]}

Ye, Dong ^{[1
,2
]}

Zhao, Yu ^{[4
]}

机构：

[1] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150001, Peoples R China

[2] Harbin Inst Technol, State Key Lab Microspacecraft Rapid Design & Intel, Harbin 150001, Peoples R China

[3] Shanghai Aerosp Control Technol Inst, Shanghai 201101, Peoples R China

[4] Inst Spacecraft Syst Engn, Beijing 100094, Peoples R China

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2025年 / 61卷 / 01期

基金：

中国国家自然科学基金; 国家重点研发计划; 中国博士后科学基金;

关键词：

Space vehicles; Attitude control; Torque; Uncertainty; Convergence; Backstepping; Satellites; Attitude tracking control; backstepping; prescribed-time prescribed-bound (PTPB) stability; rigid spacecraft; scaling transformation; NONLINEAR-SYSTEMS; STABILIZATION; CONSENSUS; FEEDBACK; DESIGN;

D O I：

10.1109/TAES.2024.3451454

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This article considers the attitude tracking control problem for rigid spacecraft with external disturbances and model uncertainties. An attitude controller with prescribed time and prescribed error bound is proposed based on scaling-transformation and backstepping. The controller can drive the attitude tracking error of the spacecraft to converge into the prescribed bound around the origin before the prescribed time with nonsingular and continuous torque. Numerical simulations are carried out to evaluate the performance of the proposed controller.

引用

页码：433 / 442

页数：10

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