The Formulation and Solution of the Multi-objective Optimization Problem for an Autonomous Electrohydraulic Servo Actuator with Combined Control
He rapid development of electrical engineering industries for aviation has resulted in a gradual transition to the autonomous electrohydraulic drives, among which an electro-hydrostatic drive is currently considered to be the most advanced. However, high requirements for dynamic parameters of modern unstable and low-stability aircrafts put restriction on implementation of electro-hydrostatic drives in the industry.