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This paper mainly introduces a flare control law design of a civil aircraft. The characteristic of auto landing was analyzed in this paper. The flare controller was designed based on the PID method which consists of two loops. The outer-loop generates a vertical speed command based on both the initialization flare altitude and the ground speed. The inner-loop is a vertical speed controller, which tracks the vertical speed command. The simulation results show that the flare control law has high precision and satisfy the vertical speed requirement when touch down.

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Design and Simulation of Automatic Flare Control Law for Civil Aircrafts

  • 会议论文

  • 发表日期：

    2025年

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  • Ziqin Xu,
  • Haonan Xu,
  • Chang Liu,
  • Zeyu Kang,
  • Zibo Wei

摘要

This paper mainly introduces a flare control law design of a civil aircraft. The characteristic of auto landing was analyzed in this paper. The flare controller was designed based on the PID method which consists of two loops. The outer-loop generates a vertical speed command based on both the initialization flare altitude and the ground speed. The inner-loop is a vertical speed controller, which tracks the vertical speed command. The simulation results show that the flare control law has high precision and satisfy the vertical speed requirement when touch down.