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Performance Comparisons between Command to Line-of-Sight Guidance Law and Proportional Navigation Guidance Law in Short Range Surface-to-Air Missile

단거리 지대공 유도무기에서의 시선지령식 유도법칙과 비례항법 유도법칙의 성능비교

  • 이연석 (군산대학교 전자정보공학부) ;
  • 유악환 (군산대학교 전자정보공학부) ;
  • 김양우 (동국대학교 정보통신공학과)
  • Published : 2007.03.01

Abstract

In this paper, a performance comparison between CLOS(Command to Line-of-Sight) guidance law and PN(Proportional Navigation) guidance law is made, based on a short range surface-to-air missile simulation program called KNUCLOS. This simulation program has a full nonlinear aerodynamic missile model, a tracker model for missile and target, and target model. According to the simulation results, the PN guidance law has a better performance than CLOS guidance law under various target speed.

Keywords

References

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