Design of a Kind of Control Circuit for Electromechanical Actuator System;

Forecast of DSP Application within the Electromechanical Actuator of Missile;

Analysis of the Feasibility and Reliability of Electromechanical Actuator for BTT Missile;

An identification arithmetic for the generalized frequency response function (GFRF) is modified firstly in this paper to improve the accuracy and robustness of this identification method, and then, a fault forecasting method based on nonlinear spectral analysis is proposed and is applied into the fault forecasting of certain helicopters electric rudders.

A mathematic model for the electric actuator of two-speed torpedo was built and introduced to the existing actuator loop and control system model.

Based on the virtual instrument development platform of Lab windows/CVI and combined with the software design for the electric actuator automatic testing equipment of flight control system,the key technique of DBS software and function module software applications is introduced and the main technical characteristic of the software development is analyzed in the paper.

Sliding mode variable structure control of electric steering engine with uncertain parameters