제어로봇시스템학회:학술대회논문집

Institute of Control, Robotics and Systems (제어로봇시스템학회)
권호 표지

Command to line of sight guidance loop based on LQG design

LQG 설계에 의한 시선지령 유도루우프의 구성

  • Chang, Sang-Keun (Dept. of Electronics Eng., Chungnam National University) ;
  • Lyou, Joon (Dept. of Electronics Eng., Chungnam National University)
  • 장상근 (충남대학교 전자공학과) ;
  • 유준 (충남대학교 전자공학과)
  • Published : 1992.10.01
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Abstract

A guidance loop of the missile system which uses a command to line of sight(CLOS) guidance law is designed based on LQG theory. In the environment of the severe tracking system noise, the system requires small aerodynamic control fin travel and small miss distance simultaneously. Results from a sample airframe shows good performance against a randomly maneuvering target.

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