Samenvatting
This paper introduces a novel cascade control structure with formal guarantees of uniform almost global asymptotic stability for the state tracking error dynamics of a quadcopter. The proposed approach employs a model predictive control strategy for the outer loop, explicitly addressing the non-zero total thrust constraint. The outer-loop controller generates an acceleration reference, which is then converted into attitude, angular velocity and acceleration references, subsequently tracked by a nonlinear inner-loop controller. A numerical case study validates the proposed scheme, highlighting its ability to track fast trajectories with small error.
| Originele taal-2 | Engels |
|---|---|
| Pagina's (van-tot) | 322-327 |
| Aantal pagina's | 6 |
| Tijdschrift | IFAC-PapersOnLine |
| Volume | 59 |
| Nummer van het tijdschrift | 19 |
| DOI's | |
| Status | Gepubliceerd - 1 jul. 2025 |
| Evenement | 13th IFAC Symposium on Nonlinear Control Systems, NOLCOS 2025 - University of Iceland, Reykjavik, IJsland Duur: 23 jul. 2025 → 25 jul. 2025 Congresnummer: 13 |
Bibliografische nota
Publisher Copyright:© 2025 The Authors. This is an open access article under the CC BY-NC-ND license.
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