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Proportional Navigation-Based Optimal Collision Avoidance for UAVs

비례항법을 이용한 무인 항공기의 최적 충돌 회피 기동

  • 한수철 (한국과학기술원 기계공학과) ;
  • 방효충 (한국과학기술원 기계공학과)
  • Published : 2004.11.01

Abstract

Optimal collision avoidance algorithm for unmanned aerial vehicles based on proportional navigation guidance law is investigated this paper. Although proportional navigation guidance law is widely used in missile guidance problems, it can be used in collision avoidance problem by guiding the relative velocity vector to collision avoidance vector. The optimal navigation coefficient can be obtained if an obstacle if an obstacle moves at constant velocity vector. The stability of the proposed algorithm is also investigated. The stability can be obtained by choosing a proper navigation coefficient.

Keywords

References

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