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Establishing the controlled dynamic model of a micro-small fixed-wing Unmanned Aerial Vehicle (UAV) is fundamental. In order to describe the attitude and position of the micro-small fixed-wing UAV, appropriate coordinate systems must be established. The attitude of the fixed-wing UAV in space is mainly described by the rotation relationship among the ground coordinate system, the body coordinate system, the wind coordinate system, and the flight path coordinate system.

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Controlled Dynamic System Modeling Experiment

  • 章节

  • 发表日期：

    2026年

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  • Lin Xu,
  • Wenhan Gao,
  • Hao Sha,
  • Xunhua Dai,
  • Quan Quan

摘要

Establishing the controlled dynamic model of a micro-small fixed-wing Unmanned Aerial Vehicle (UAV) is fundamental. In order to describe the attitude and position of the micro-small fixed-wing UAV, appropriate coordinate systems must be established. The attitude of the fixed-wing UAV in space is mainly described by the rotation relationship among the ground coordinate system, the body coordinate system, the wind coordinate system, and the flight path coordinate system.