Control of Electro-Mechanical Actuator for Aerospace Applications
Апстракт
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.
Кључне речи:
Thrust Vector Control / Sensor / Planetary Roller Screw / PID controller / Electro-Mechanical Actuator / Brushless DC MotorИзвор:
Strojarstvo, 2010, 52, 3, 303-312Издавач:
- Croation Union of Mech. Engineers and Naval Architects
Колекције
Институција/група
Mašinski fakultetTY - JOUR AU - Khan, Muhammad Ashraf AU - Todić, Ivana AU - Miloš, Marko AU - Stefanović, Zoran AU - Blagojević, Đorđe PY - 2010 UR - https://machinery.mas.bg.ac.rs/handle/123456789/994 AB - 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. PB - Croation Union of Mech. Engineers and Naval Architects T2 - Strojarstvo T1 - Control of Electro-Mechanical Actuator for Aerospace Applications EP - 312 IS - 3 SP - 303 VL - 52 UR - https://hdl.handle.net/21.15107/rcub_machinery_994 ER -
@article{ author = "Khan, Muhammad Ashraf and Todić, Ivana and Miloš, Marko and Stefanović, Zoran and Blagojević, Đorđe", year = "2010", abstract = "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.", publisher = "Croation Union of Mech. Engineers and Naval Architects", journal = "Strojarstvo", title = "Control of Electro-Mechanical Actuator for Aerospace Applications", pages = "312-303", number = "3", volume = "52", url = "https://hdl.handle.net/21.15107/rcub_machinery_994" }
Khan, M. A., Todić, I., Miloš, M., Stefanović, Z.,& Blagojević, Đ.. (2010). Control of Electro-Mechanical Actuator for Aerospace Applications. in Strojarstvo Croation Union of Mech. Engineers and Naval Architects., 52(3), 303-312. https://hdl.handle.net/21.15107/rcub_machinery_994
Khan MA, Todić I, Miloš M, Stefanović Z, Blagojević Đ. Control of Electro-Mechanical Actuator for Aerospace Applications. in Strojarstvo. 2010;52(3):303-312. https://hdl.handle.net/21.15107/rcub_machinery_994 .
Khan, Muhammad Ashraf, Todić, Ivana, Miloš, Marko, Stefanović, Zoran, Blagojević, Đorđe, "Control of Electro-Mechanical Actuator for Aerospace Applications" in Strojarstvo, 52, no. 3 (2010):303-312, https://hdl.handle.net/21.15107/rcub_machinery_994 .