Abstract
This study proposes a universal (U)-control enhanced with dynamic inversion for a class of multiple-input multiple-output (MIMO) quadrotor flight tracking operations. In the technique, a robust compensator is integrated with the U-controller to achieve stabilisation at the equilibrium and setpoint tracking in the presence of any unmodelled uncertainties and external disturbances. A series of bench tests of simulated and real experiments on a Parrot Mambo quadrotor are conducted to show the design framework from the academic formulation to Simulink simulation and real flight tests.
| Original language | English |
|---|---|
| Article number | 599 |
| Journal | Drones |
| Volume | 8 |
| Issue number | 10 |
| Number of pages | 24 |
| DOIs | |
| Publication status | Published - 18.10.2024 |
Bibliographical note
Publisher Copyright:© 2024 by the authors.
Research areas and keywords
- quadrotor control
- quadrotor UAV
- simulation and flying tests
- trajectory tracking
- U-dynamic inversion
- U-model realisation
- Engineering
ASJC Scopus Subject Areas
- Aerospace Engineering
- Artificial Intelligence
- Computer Science Applications
- Information Systems
- Control and Systems Engineering
Fingerprint
Dive into the research topics of 'Dynamic Inversion-Enhanced U-Control of Quadrotor Trajectory Tracking'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver