Event-Triggered Tracking Control for a Flapping-Wing Aerial Vehicle With Prescribed Performance
This article proposes an adaptive prescribed performance control scheme utilizing an event-triggered mechanism for a flapping wing aerial vehicle to address communication constraints and position tracking error constraints. Flapping wing aerial vehicles confront unique control challenges due to their complex dynamics and inherent instability. To address these, the proposed scheme manages a transition from initially unconstrained to constrained position tracking errors, accommodating the practical need for unconstrained operation during initial flight phases. An intermediate performance function is introduced to derive a control solution that respects tracking error constraints, while a relative threshold event-triggered mechanism optimizes communication resource utilization. Simulation results validate the feasibility of this control methodology.
Authors
- Jianwei Xia (ORCID: https://orcid.org/0000-0002-5330-9349)
- Wei He (ORCID: https://orcid.org/0000-0002-8944-9861)
- Linghuan Kong (ORCID: https://orcid.org/0000-0001-9866-4822)
- Tingting Meng (ORCID: https://orcid.org/0000-0003-1083-2268)
- Xueliang Wang
Institutions
- Liaocheng University (CN)
- University of Macau (MO)
- Beijing Academy of Artificial Intelligence (CN)
- Beijing Information Science & Technology University (CN)
- University of Science and Technology Beijing (CN)
Publication Details
- Journal
- IEEE Transactions on Aerospace and Electronic Systems
- Published
- 2025-09-02
- DOI
- https://doi.org/10.1109/taes.2025.3605137
- Primary Topic
- Biomimetic flight and propulsion mechanisms
- Type
- article
- Field-Weighted Citation Impact
- 0.00