| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 709162 | IFAC Proceedings Volumes | 2013 | 6 Pages |
Abstract
In this paper an altitude hold controller of a small fixed wing UAV is presented, designed with output feedback 1 adaptive control with switching adaptation law. The adaptive architecture is based on the estimated state as a substitute of full state knowledge. Simulation results on a real-time test bench show robustness of the adaptive controller to large uncertainties and disturbances which may act on the UAV.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
