Title :
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
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;
Conference_Titel :
Electric Information and Control Engineering (ICEICE), 2011 International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-8036-4
DOI :
10.1109/ICEICE.2011.5777382
