Comparison of Tracking Performance and Robustness of Simplified Models of Multirotor UAV’s Propulsion Unit with CDM and PID Controllers (with anti-windup compensation)
[ 1 ] Instytut Automatyki i Inżynierii Informatycznej, Wydział Elektryczny, Politechnika Poznańska | [ P ] employee
2017
scientific article
english
- Coefficient Diagram Method
- anti-windup compensator
- pole placement
- PID control
- propulsion unit simplified model
- thrust controller
- robust control
31 - 40
CC BY (attribution alone)
open journal
final published version
at the time of publication
15
15
0,698