Managing Unwinding in Quaternion-Based Antiwindup Compensation for Constrained Rigid Body Attitude Control

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2025-03-06 DOI:10.1109/TAES.2025.3548593
Homa Salehifar;Christopher M. Richards;Matthew C. Turner
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Abstract

This article investigates the problem of unwinding in quaternion-based antiwindup compensation for constrained rigid body attitude control. Quaternion-based compensators and controllers can lead to the unwinding phenomenon if the double covering problem of the rigid-body-attitude space is not considered. Moreover, actuator saturation is a source of performance degradation or even instability of control systems. Therefore, in this article, a quaternion-based antiwindup compensator is proposed and stability proofs are derived that provide asymptotic stability properties and a propensity to avoid attitude unwinding. Simulation results illustrate that the proposed method leads to significantly smaller rotation of the rigid body than an earlier antiwindup approach that does not address the unwinding phenomenon.
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约束刚体姿态控制中基于四元数反缠绕补偿的解卷管理
研究了约束刚体姿态控制中基于四元数的反缠绕补偿中的解缠绕问题。如果不考虑刚体-姿态空间的双重覆盖问题,基于四元数的补偿器和控制器会导致解卷现象。此外,执行器饱和是控制系统性能下降甚至不稳定的根源。因此,本文提出了一种基于四元数的反卷绕补偿器,并给出了稳定性证明,该证明提供了渐近稳定性和避免姿态卷绕的倾向。仿真结果表明,所提出的方法导致刚体的旋转明显小于先前的不解决解绕现象的反上卷方法。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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