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Control of Electro-Mechanical Actuator for Aerospace Applications

Muhammad Ashraf KHAN ; Faculty of Mechanical Engineering,University of Belgrade, Belgrade, Serbia
Ivana TODIĆ ; Faculty of Mechanical Engineering,University of Belgrade, Belgrade, Serbia
Marko MILOŠ   ORCID icon orcid.org/0000-0002-1931-1170 ; Faculty of Mechanical Engineering,University of Belgrade, Belgrade, Serbia
Zoran STEFANOVIĆ ; Faculty of Mechanical Engineering,University of Belgrade, Belgrade, Serbia
Đorđe BLAGOJEVIĆ ; Faculty of Mechanical Engineering,University of Belgrade, Belgrade, Serbia

Puni tekst: engleski, pdf (3 MB) str. 303-313 preuzimanja: 2.942* citiraj
APA 6th Edition
KHAN, M.A., TODIĆ, I., MILOŠ, M., STEFANOVIĆ, Z. i BLAGOJEVIĆ, Đ. (2010). Control of Electro-Mechanical Actuator for Aerospace Applications. Strojarstvo, 52 (3), 303-313. Preuzeto s https://hrcak.srce.hr/64422
MLA 8th Edition
KHAN, Muhammad Ashraf, et al. "Control of Electro-Mechanical Actuator for Aerospace Applications." Strojarstvo, vol. 52, br. 3, 2010, str. 303-313. https://hrcak.srce.hr/64422. Citirano 18.08.2019.
Chicago 17th Edition
KHAN, Muhammad Ashraf, Ivana TODIĆ, Marko MILOŠ, Zoran STEFANOVIĆ i Đorđe BLAGOJEVIĆ. "Control of Electro-Mechanical Actuator for Aerospace Applications." Strojarstvo 52, br. 3 (2010): 303-313. https://hrcak.srce.hr/64422
Harvard
KHAN, M.A., et al. (2010). 'Control of Electro-Mechanical Actuator for Aerospace Applications', Strojarstvo, 52(3), str. 303-313. Preuzeto s: https://hrcak.srce.hr/64422 (Datum pristupa: 18.08.2019.)
Vancouver
KHAN MA, TODIĆ I, MILOŠ M, STEFANOVIĆ Z, BLAGOJEVIĆ Đ. Control of Electro-Mechanical Actuator for Aerospace Applications. Strojarstvo [Internet]. 2010 [pristupljeno 18.08.2019.];52(3):303-313. Dostupno na: https://hrcak.srce.hr/64422
IEEE
M.A. KHAN, I. TODIĆ, M. MILOŠ, Z. STEFANOVIĆ i Đ. BLAGOJEVIĆ, "Control of Electro-Mechanical Actuator for Aerospace Applications", Strojarstvo, vol.52, br. 3, str. 303-313, 2010. [Online]. Dostupno na: https://hrcak.srce.hr/64422. [Citirano: 18.08.2019.]

Sažetak
The paper mainly focuses two major areas of electromechanical actuator
system composed of power screw, spur gear train and Brushless DC Servo
Motor. First it describes control of electromechanical actuator system with
three level of current controller which is composed of power amplifier,
DSP module and interfacing circuitry. The non-linear model of the three
level controllers developed in SIMULINK environment is presented. A
second point which was included in this study is the comparison of two
control strategies i.e. three level controller and PWM current controller.
The main outcomes of the study is that three level controller is simple
in construction and much more stable. This is much suitable for higher
reduction systems, short missions and low power density actuators;
however it has few limitation that make it unsuitable for applications such
as high power density, long missions and direct drive system.

Ključne riječi
Brushless DC Motor; Electro-Mechanical Actuator; PID controller; Planetary Roller Screw; Sensor; Thrust Vector Control

Hrčak ID: 64422

URI
https://hrcak.srce.hr/64422

[hrvatski]

Posjeta: 3.365 *