A Dynamic Event-triggered Control Method for Unmanned Aircrafts Trajectory Tracking in Low-Altitude Airspace
This paper addresses the critical challenge of trajectory tracking control for unmanned aircraft in low-altitude urban environments, where dynamic wind disturbances significantly impact flight stability and precision, under the constraint of limited onboard computational resources. We propose a novel control framework to overcome this challenge. First, urban wind disturbances are formally characterized as persistent perturbations with unbounded energy and unknown dynamics. Based on this, a two-layer control architecture is developed. The position loop utilizes a dynamic event-triggered controller, designed via the internal model principle, achieving asymptotic trajectory tracking with optimized energy consumption. The attitude loop employs an adaptive robust controller to mitigate inertial uncertainties through real-time parameter adaptation. A composite Lyapunov-based proof rigorously establishes the overall system's asymptotic stability, systematically integrating the internal model principle across both control layers. High-fidelity numerical simulations demonstrate the controller's efficacy in maintaining accurate trajectory tracking, even with concurrent wind disturbances and parametric uncertainties.
Authors
- Peng Zhao (ORCID: https://orcid.org/0000-0002-3815-1248)
- Kaiquan Cai (ORCID: https://orcid.org/0000-0002-2108-291X)
- Ling He (ORCID: https://orcid.org/0000-0002-8692-7530)
- Zean Bao (ORCID: https://orcid.org/0009-0009-3575-9934)
Institutions
- Civil Aviation Administration of China (CN)
- Beihang University (CN)
Publication Details
- Published
- 2025-04-08
- DOI
- https://doi.org/10.1109/icns65417.2025.10976781
- Primary Topic
- Air Traffic Management and Optimization
- Type
- article
- Field-Weighted Citation Impact
- 0.00
Funders
- National Natural Science Foundation of China