INVESTIGATION OF HELICOPTER STABILITY CONSIDERING THE EFFECT OF ITS HYDRAULIC SERVOACTUATOR AND AUTOPILOT

INVESTIGATION OF CHARACTERISTICS OF AN ELECTROHYDRAULIC SERVOACTUATOR INCORPORATING JET PIPE AMPLIFIER

Motion control of an aircraft electro-hydraulic servo actuator

Investigation of Electrohydraulic Control of A Gas Turbine Engine’s Inlet Guide Vanes

INVESTIGATION OF LATERAL FLYING QUALITIES OF AIRCRAFT

Investigation of Dynamic Performance of an Electro-Hydraulic Proportional System

THEORETICAL AND EXPERIMENTAL INVESTIGATIONS OF DYNAMIC BEHAVIOR OF AN ELECTRO-HYDRAULIC DIRECTIONAL PROPORTIONAL VALVE

AN INTEGFATED FLIGHT CONTROL SYSTEM PERFORMING TERRAIN FOLLOWING MISSIONS

DYNAMIC PERFORMANCE OF AN ELECTROHYDRAULIC SERVO ACTUATOR WITH CONTACTLESS CONTROLLED SPOOL

MODELLING OF AN AIRCRAFT LONGITUDINAL CONTROL SYSTEM.