Dynamic Inversion-Enhanced U-Control of Quadrotor Trajectory Tracking
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.
Authors
- Hamidreza Nemati (ORCID: https://orcid.org/0000-0002-5081-4630)
- Paolo Mercorelli (ORCID: https://orcid.org/0000-0003-3288-5280)
- Quanmin Zhu (ORCID: https://orcid.org/0000-0001-8173-1179)
- Ahtisham Aziz Lone
Institutions
- Leuphana University of Lüneburg (DE)
- University of the West of England (GB)
Publication Details
- Journal
- Drones
- Published
- 2024-10-18
- DOI
- https://doi.org/10.3390/drones8100599
- Citations
- 2
- Primary Topic
- Adaptive Control of Nonlinear Systems
- Type
- article
- Field-Weighted Citation Impact
- 0.66