Title :
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
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;
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
DOI :
10.1109/ICCAS.2007.4406560
