Journal of the Korea Institute of Military Science and Technology (한국군사과학기술학회지)

The Korea Institute of Military Science and Technology (한국군사과학기술학회)
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Range Sensitivity Analysis of a Canard Controlled Missile

유도 미사일의 사거리 민감도 연구

  • 양영록 (경상대학교 & 항공기부품기술연구소) ;
  • 조태환 (경상대학교 & 항공기부품기술연구소) ;
  • 명노신 (경상대학교 & 항공기부품기술연구소)
  • Received : 2010.10.08
  • Accepted : 2011.01.20
  • Published : 2011.02.05
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Abstract

This study describes a range sensitivity of a canard controlled missile. An investigation was conducted into the relative importance of aerodynamic parameters on a guided missile. Also this study was analyzed by quantifying their effects on the missile range. To analyze the range sensitivity of a guided missile, a trajectory analysis program of a guided missile was developed. The range sensitivity analysis was conducted on a thrust, weight, drag and lift. The result of the range sensitivity analysis shows that the design parameters with the greatest effect on the missile range are thrust, drag, weight, and lift, in descending order of importance. The thrust on range extension is quite obvious to extend a range of a guided missile. In particular, the drag exhibited greater range sensitivity than lift at a guided flight. The result also shows that missile range could be maximized by applying the appropriate launch angle and canard pitch-up control.

Keywords

References

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