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<p>Problems of quadcopter (unmanned aerial vehicle) control have been considered in the literature for mathematical models with different classes of controls with various options for phase variables and control parameters. The article presents a&#xa0;derivation of a&#xa0;quadcopter dynamics model with Euler and Krylov angles, in a&#xa0;fixed coordinate system.</p>

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Quadcopter Dynamics Equations

  • 期刊论文

  • 发表日期：

    2025年12月1日

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  • V. P. Gorkov,
  • N. L. Grigorenko

摘要

Problems of quadcopter (unmanned aerial vehicle) control have been considered in the literature for mathematical models with different classes of controls with various options for phase variables and control parameters. The article presents a derivation of a quadcopter dynamics model with Euler and Krylov angles, in a fixed coordinate system.