Servo Controller Based on DSP and MCX314 for pneumatic load simulation platform of aircraft actuator

Author

Li, Zongshuai ; Qia, Hui

Author_Institution

Aeronaut. Autom. Coll., Civil Aviation Univ. of China, Tianjin, China

fYear

2011

fDate

15-17 April 2011

Firstpage

3567

Lastpage

3570

Abstract

According to pneumatic load simulation platform of aircraft actuator, the paper introduces the general structure and operation principle of the system. Firstly, the interface circuit of DSPF2812 is given. Next the the interface circuit of MCX314 between external equipment is presented. The design of sofware also is presented. At last, In order to validate the feasibility of the design, the experiment is done, Experimental results indicate that the Servo Controller and platform has an outstanding performance.

Keywords

actuators; aerospace computing; aircraft; control engineering computing; digital signal processing chips; microprocessor chips; pneumatic control equipment; servomechanisms; DSPF2812; MCX314 interface circuit; aircraft actuator; pneumatic load simulation platform; servo controller; Aerospace control; Aircraft; Atmospheric modeling; Digital signal processing; Integrated circuit modeling; Pulse width modulation; Servomotors; DSPF2812; MCX314; Servo Controller; actuator;

fLanguage

English

Publisher

ieee

Conference_Titel

Electric Information and Control Engineering (ICEICE), 2011 International Conference on

Conference_Location

Wuhan

Print_ISBN

978-1-4244-8036-4

Type

conf

DOI

10.1109/ICEICE.2011.5777382

Filename

5777382