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.
Authors
- Matthew C. Turner (ORCID: https://orcid.org/0000-0003-2161-7635)
- Christopher M. Richards (ORCID: https://orcid.org/0000-0003-0643-7177)
- Homa Salehifar (ORCID: https://orcid.org/0000-0001-8952-2398)
Institutions
- University of Louisville (US)
- University of Southampton (GB)
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
Funders
- Engineering and Physical Sciences Research Council