与えられた経路のための飛行制御系

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タイトル別名
  • Given flight trajectory controller for aircraft.
  • アタエラレタ ケイロ ノ タメ ノ ヒコウ セイギョケイ

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In this paper, the synthesis of nonlinear flight control system for an aircraft to track a given trajectory is presented. The trajectory is given in the form of position in space, which is the functions of time or the tangent velocity and the two path angles which are computed from the differentiation of the position with respect to time. The forces which guide the airplane along the given trajectory are basically constracted of two parts. One is the force necessary for the program motion and the other is the force to eliminate the guidance errors. The algorithm of this controller was applied to F-4 fighter performing a barrel roll maneuver and some numerical simulations were performed. The results showed that the differences between the actual flight path and the given one were negligible.

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