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A Modified Nonlinear Guidance Logic for a Leader-Follower Formation Flight of Two UAVs

무인항공기의 Leader-Follower 편대비행을 위한 수정된 비선형 유도법칙

  • Published : 2009.01.01

Abstract

A formation flight guidance logic that enables the leader-follower station keeping between two UAVs is presented in this paper. The logic is motivated by the investigation of the relation between the proportional navigation and the nonlinear trajectory tracking guidance law, The simplicity of the presented method provides computational efficiency and allows easy implementation. An excellent performance of the proposed logic is demonstrated via various numerical simulations for multiple UAVs environment.

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