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In this paper, a modified PID control law for aircraft pitch movement control is studied. New design parameters are introduced for improving pitch movement control performance. A comparison to traditional PID controllers is carried out. The simulation results show that the proposed PID controller can stabilize the aircraft pitch movement and has better performance compared to conventional PID controllers and serves the consideration in designing pitch control system for real aircrafts.

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An Improved PID Controller for Aircraft Pitch Movement Control

  • 会议论文

  • 发表日期：

    2026年

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  • Tung Thanh Le

摘要

In this paper, a modified PID control law for aircraft pitch movement control is studied. New design parameters are introduced for improving pitch movement control performance. A comparison to traditional PID controllers is carried out. The simulation results show that the proposed PID controller can stabilize the aircraft pitch movement and has better performance compared to conventional PID controllers and serves the consideration in designing pitch control system for real aircrafts.