DocumentCode :
1587617
Title :
Design of real-time inspection and aeronautical instrument displaying system for areomotor revving
Author :
Dongmei, Wang ; Lingshun, Liu ; Junwei, Lv
Author_Institution :
Dept. of Control Eng., Naval Aeronaut. & Astronaut. Univ., Yantai, China
Volume :
2
fYear :
2011
Firstpage :
252
Lastpage :
254
Abstract :
In this paper, a kind of real-time inspection and aeronautical instrument displaying system of areomotor revving based on single chip technical is introduced. The system is mainly consisted of signal transformation, single chip microcomputer AT89C51 and step motor´s drive electric circuit. Experimental results show that when the intial signal frequency inputted, the aeronautical instrument starts to turn to the corresponding angle position; when the signal frequency constantly changing, the aeronautical instrument turns to move corresponding angle; The accuracy comes to control request while changing frequency; The system is small in size and simple in operation and high steady.
Keywords :
aerospace instrumentation; display instrumentation; microprocessor chips; motor drives; stepping motors; aeronautical instrument displaying system; areomotor revving; real-time inspection; signal transformation; single chip microcomputer AT89C51; single chip technical; step motor drive electric circuit; Algorithms; Frequency control; Instruments; Motor drives; Process control; Real time systems; Rectifiers; AT89C51; Rev; areomotor; step motor;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electronic Measurement & Instruments (ICEMI), 2011 10th International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-8158-3
Type :
conf
DOI :
10.1109/ICEMI.2011.6037809
Filename :
6037809
Link To Document :
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