• 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