龙悬浮飞行期间的推力平衡模型
Kaixuan Zhang1, Xiaohui Su1, Yong Zhao2
1School of Hydraulic Engineering, Dalian University of Technology, Dalian 116024, People's Republic of China.
Bioinspiration & biomimetics
|October 30, 2024
概括
本研究引入了一种双翼推力平衡模型 (DTBM),以解决微型空中车辆 (MAV) 由于推力不平衡而产生的振荡. DTBM有效地平衡推力,改善MAV的稳定性和控制.
科学领域:
- 航空航天工程 航空航天工程
- 生物模拟学是一种生物模拟学.
- 流体动力学 流体动力学
背景情况:
- 微型空中车辆 (MAV) 由于推力失衡而经历振荡.
- 在MAV中实现稳定的飞行,特别是在悬浮时,仍然是一个挑战.
研究的目的:
- 提出和验证双翼推力平衡模型 (DTBM) 以减轻MAV振荡.
- 分析翅膀动力学和推力产生之间的关系,以改善MAV控制.
主要方法:
- 开发了一种双翼推力平衡模型 (DTBM),使用修改的旋转角度公式.
- 调查了"au角度" (中转时的翅膀角度) 对推力系数的影响.
- 在模拟龙飞行中分析了推力平衡的实现和运动模式 (线性与非线性).
主要成果:
- 在几次代中,DTBM将平均推力系数降低到0.001以下.
- 对于复杂的运动模式,推力平衡在0.278秒内实现.
- 确定了与侧向力干扰相关的"角度",翅膀间距和翻动轨迹之间的线性和非线性相关性.
结论:
- DTBM为MAV的推力失衡问题提供了有效的解决方案.
- 了解机翼运动的非线性动力学对于先进的MAV设计至关重要.
- 未来的MAV可以从整合DTBM的算法中获益,以提高悬浮稳定性.
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