Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 322-327 |
| Number of pages | 6 |
| Journal | IFAC-PapersOnLine |
| Volume | 59 |
| Issue number | 19 |
| DOIs | |
| Publication status | Published - 1 Jul 2025 |
| Event | 13th IFAC Symposium on Nonlinear Control Systems, NOLCOS 2025 - University of Iceland, Reykjavik, Iceland Duration: 23 Jul 2025 → 25 Jul 2025 Conference number: 13 |
Bibliographical note
Publisher Copyright:© 2025 The Authors. This is an open access article under the CC BY-NC-ND license.
Keywords
- Model predictive control
- quadcopter
- uniform global asymptotic stability
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