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.

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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
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article

Event-Triggered Tracking Control for a Flapping-Wing Aerial Vehicle With Prescribed Performance

Jianwei Xia, Wei He, Linghuan Kong, Tingting Meng et al.
IEEE Transactions on Aerospace and Electronic Systems
Biomimetic flight and propulsion mechanisms
article

Event-Triggered Tracking Control for a Flapping-Wing Aerial Vehicle With Prescribed Performance

Jianwei Xia, Wei He, Linghuan Kong, Tingting Meng, Xueliang Wang
article en

Abstract

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.

IEEE Transactions on Aerospace and Electronic SystemsVol. 61(6)
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)
Openalex Percentile: Top 68%
Biomimetic flight and propulsion mechanisms
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