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

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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Publication Details

Journal
IEEE Transactions on Aerospace and Electronic Systems
Published
2025-03-06
DOI
https://doi.org/10.1109/taes.2025.3548593
Primary Topic
Aerospace Engineering and Energy Systems
Type
article
Field-Weighted Citation Impact
0.00

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article

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

Matthew C. Turner, Christopher M. Richards, Homa Salehifar
IEEE Transactions on Aerospace and Electronic Systems
Aerospace Engineering and Energy Systems
article

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

Matthew C. Turner, Christopher M. Richards, Homa Salehifar
article en

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.

IEEE Transactions on Aerospace and Electronic SystemsVol. 61(4)
University of Louisville (US), University of Southampton (GB)
Engineering and Physical Sciences Research Council
Climate action
Openalex Percentile: Top 95%
Aerospace Engineering and Energy Systems
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