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Design and Implementation of a Missile-Borne Turbine Engine Controller Based on SOPC

  • HAN Bin ,
  • DING Li ,
  • LI Hongcai ,
  • WANG Gaitang
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  • Xi'an Modern Control Technology Research Institute, Xi'an 710065, China

Received date: 2018-09-15

  Online published: 2025-05-19

Abstract

In order to meet the requirement of short starting time and high speed control accuracy for missile-borne turbine engine, the controller system based on SOPC is designed. In this system, the milli volt level signal is transformed to TTL level signal, the starter for pilots, oil valve, pump and other accessories are driven by the MOSFET of the engine, which achieve the fast starting and speed control of engine. The test results show that the controller is a stable and reliable operation, which meet the requirements of control precision and real-time performance.

Cite this article

HAN Bin , DING Li , LI Hongcai , WANG Gaitang . Design and Implementation of a Missile-Borne Turbine Engine Controller Based on SOPC[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019 , 39(4) : 89 -92 . DOI: 10.15892/j.cnki.djzdxb.2019.04.021

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