DocumentCode
2431883
Title
Controller design of missile actuator using DSP
Author
Jeong, Dae-Seong ; Choi, Kwang-Jin ; Woo, Hyun-Wook ; Kim, Jong-Gi
Author_Institution
LIG Nex1, Yongin
fYear
2007
fDate
17-20 Oct. 2007
Firstpage
2110
Lastpage
2113
Abstract
This paper proposes a design method of the position, velocity, and current controller for a hall sensored BLDC motor using TMS320F2812, a velocity estimation algorithm using a hall sensor, and a robust controller design method for an actuator system with uncertainties. The actuator for missiles requires high precision, fast response, and smaller size. The controller of the actuator should also satisfy these requirements. Although the analog controller provide precise control and fast response, the implementation of control algorithm and the modification of controller design are not easy. However, the digital controller solves these difficulties of the analog controller, since it implement the control algorithm as software. Moreover, it is easy to simulate under MATLAB/SIMULINK with the digital controller, which makes the digital controller more preferred.
Keywords
DC motors; actuators; control system synthesis; digital control; digital signal processing chips; electric current control; missile guidance; position control; pulse width modulation; robust control; uncertain systems; velocity control; DSP; PWM; TMS320F2812; current controller; guidance control unit; hall sensored BLDC motor; missile actuator digital controller design; position controller; robust controller design method; uncertain actuator system; velocity controller; velocity estimation algorithm; Actuators; Brushless DC motors; Control systems; Design methodology; Digital control; Digital signal processing; Missiles; Robust control; Sensor systems; Velocity control; Control; DSP; 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.2007.4406678
Filename
4406678
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