Position Servo Control for Dual Piezoelectric Pumps-Based Electro-Hydrostatic Actuator with Active Rectification Valve
Author:
Affiliation:
1. College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronaut,Nanjing,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10564848/10565383/10565509.pdf?arnumber=10565509
Reference13 articles.
1. Review on signal-by-wire and power-by-wire actuation for more electric aircraft
2. Analysis of the dynamic performance of an electro-hydrostatic actuator and improvement methods
3. Dynamic thermal coupling modeling and analysis of wet electro-hydrostatic actuator
4. Dynamic Analysis of Electro Hydrostatic Actuation System
5. Thermal-fluid-structure coupling analysis for valve plate friction pair of axial piston pump in electrohydrostatic actuator (EHA) of aircraft
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