제어로봇시스템학회:학술대회논문집
- 제어로봇시스템학회 1992년도 한국자동제어학술회의논문집(국내학술편); KOEX, Seoul; 19-21 Oct. 1992
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- Pages.567-571
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- 1992
LQG 설계에 의한 시선지령 유도루우프의 구성
Command to line of sight guidance loop based on LQG design
- Chang, Sang-Keun (Dept. of Electronics Eng., Chungnam National University) ;
- Lyou, Joon (Dept. of Electronics Eng., Chungnam National University)
- 발행 : 1992.10.01
초록
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.
키워드