Actuator parametric synthesis for aircraft hydraulic steering gear with rate delivery control

Аuthors

Polkovnikov V. A.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

Abstract

Design expressions are obtained for parametric synthesis of hydraulic servo actuators under speed delivery control. Total actuator power is used as the criterion to be minimized. The design expressions are based on the theory of dynamic capabilities maximization for servo drives. An arbitrary and harmonic object motion control laws are considered. Principal limitations for servo actuator energy channel are taken into account.