Functioning analysis for actuator of electrical-driven control system powered with combined current supply

Аuthors

, Samokhina K. E., Sorokin A. E.

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

Abstract

Electrical-driven actuators for flying vehicle control surfaces attract more attention in recent years, but for all that power supply aspects do not consider properly in most cases. However current supply type and its characteristics influence considerably on dynamical properties, mass and size of autonomous electrical-driven control systems. An integrated functioning analysis is carried out to reveal performances for some electrical-driven control system powered with combined current supply.