在倾斜驱动同轴旋转机无人机中,旋转机间距和态度转变的空气动力学分析
Wei Wu1, Xinyu Tan1, Xing Liu1
1School of Electronic Information Engineering, Xi'an Technological University, Xi'an 710021, China.
Sensors (Basel, Switzerland)
|November 27, 2024
概括
优化倾斜驱动的同轴双转子无人机 (UAV) 需要了解空气动力学转换. 9°的倾斜角度提高了飞行稳定性和旋转器在垂直向前飞行机动过程中的效率.
科学领域:
- 航空航天工程 航空航天工程
- 流体动力学 流体动力学
- 控制系统 控制系统
背景情况:
- 倾斜驱动的同轴双旋转机无人机 (UAV) 在倾斜转移时面临飞行控制方面的挑战.
- 了解复杂的空气动力学特性对于优化其性能至关重要.
研究的目的:
- 在无人机从垂直飞行到前进飞行的态度过渡期间调查空气动力学机制.
- 优化控制参数以提高飞行稳定性和效率.
主要方法:
- 为无人机开发一个动态模型.
- 理论分析和数值模拟的结合.
- 分析不同倾斜角度的负载分布和空气动力学特征.
主要成果:
- 最佳转子间距的确定为h = 0.5 R.
- 9°的倾斜角度显著增加了推力 (439%) 和倾斜速度.
- 9°的倾斜角度显示出更高的流散射,更好的旋转器布局效率,和稳定的流.
结论:
- 9°的倾斜角度优化了倾斜驱动的同轴双旋转机无人机的空气动力性能和稳定性.
- 该研究增强了无人机的理论模型和参数优化.
- 这些发现为未来的无人机开发和飞行控制设计提供了宝贵的见解.
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