摘要
This paper presents an adaptive control framework for dual-system VTOL UAVs capable of operating in both rotary-wing and fixed-wing modes. These aerial vehicles present considerable control challenges due to their nonlinear, time-varying dynamics and inherent instability during flight-mode transitions. The proposed approach addresses these issues by leveraging nonlinear system identification via Adaptive Sparse Identification of Nonlinear Dynamics (ASINDy) with a Lyapunov-based Model Predictive Control (LMPC) scheme. This integrated framework facilitates continuous model updating and guarantees stable trajectory tracking and robust performance. Compared to the GA-PID, the ASINDy–LMPC approach reduced tracking error by approximately 65%, maximum deviation by 67%, average deviation by 79%, and power consumption by 73% in simulation, while nearly halving the control effort. Preliminary hardware trials on a VTOL UAV prototype corroborate these trends, demonstrating consistent improvements during hovering and outdoor flights.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 2388-2417 |
| 页数 | 30 |
| 期刊 | International Journal of Robust and Nonlinear Control |
| 卷 | 36 |
| 期 | 5 |
| DOI | |
| 出版状态 | 已出版 - 25 3月 2026 |
| 已对外发布 | 是 |
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