Because of the advantages of being reliable, saving weight, size and cost, reducing maintenance fees and environmental impact, More Electric Aircraft (MEA) has attracted more and more attention, and Electro-mechanical Actuators (EMA) are the realization of the MEA concept. This paper introduce the cascade controller design for the EMA of the flight surface, which includes current loop, speed loop and position loop. The simulation results using anti-windup method all meet the overshooting requirements of 5% and show the effectiveness of the design.
Controller Design for Electro-mechanical Actuators
Lect. Notes Electrical Eng.
Proceedings of the 5th China Aeronautical Science and Technology Conference ; Kapitel : 46 ; 466-472
02.11.2021
7 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Controller Design for Electro-mechanical Actuators
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