Design of the aeroload simulator for the test of a small sized electro-mechanical actuator

Author

Chun, Tae-Young ; Hur, Gyee-Young ; Choi, Kwang-Jin ; Woo, Hyun-Wook ; Kang, Dong-Seok ; Kim, Jin-Cheon

Author_Institution

Mech. Eng. R&D Center, Yongin

fYear

2007

fDate

17-20 Oct. 2007

Firstpage

1416

Lastpage

1419

Abstract

The aeroload simulator is a test instrument that can produce a wide range of rotary position motion, and active dynamic torque, to simulate loads that control surfaces experience during missile flight. In this paper, we designed the aeroload simulator that is stable, accurate and optimal for a small sized electro-mechanical actuator. It is the simple system that consists of a DC(direct current) motor and an encoder. The performance of the designed aeroload simulator is verified by simulation results.

Keywords

DC motors; aerospace instrumentation; aerospace simulation; aerospace test facilities; electric actuators; missile control; DC motor; active dynamic torque; aeroload simulator design; encoder; missile flight; rotary position motion; small sized electro-mechanical actuator testing; test instrument; Actuators; Aerodynamics; Aerospace simulation; DC motors; Frequency response; Gears; Missiles; Motion control; Testing; Torque control; aeroload simulator; electro-mechanical actuator; missile;

fLanguage

English

Publisher

ieee

Conference_Titel

Control, Automation and Systems, 2007. ICCAS '07. International Conference on

Conference_Location

Seoul

Print_ISBN

978-89-950038-6-2

Electronic_ISBN

978-89-950038-6-2

Type

conf

DOI

10.1109/ICCAS.2007.4406560

Filename

4406560