无尾控制一个四翼的飞翼微型空中飞行器与翅膀扭转调制
Heetae Park1, Seungkeun Kim1, Jinyoung Suk1
1Department of Aerospace Engineering, Chungnam National University, 99 Daehak-ro, Yuseong-gu, Daejeon 34134, Republic of Korea.
Bioinspiration & biomimetics
|January 17, 2025
概括
本研究介绍了一种无尾控制系统,用于四翼的飞式微型飞行器,使用可变的飞频率和翼扭曲调制来提高稳定性和灵活性. 飞行实验证实了其在提供控制时刻的有效性,同时最大限度地减少交叉合效应.
科学领域:
- 航空航天工程 航空航天工程
- 机器人技术 机器人技术 机器人技术
- 控制系统 控制系统
背景情况:
- 起伏翼微型飞行器 (FWMAV) 在机动性和悬空能力方面提供了独特的优势.
- 传统的FWMAV往往依赖于复杂的尾部结构来保持稳定和控制.
- 开发无尾控制系统对于小型化和提高空气动力学效率至关重要.
研究的目的:
- 为四翼FWMAV设计和分析一个无尾控制系统.
- 为了研究可变飞频率和翼扭曲调制对飞行控制的有效性.
- 优化机翼几何和执行方法,以提高控制权力和效率.
主要方法:
- 对于滚动动量的产生,差异性折叠频率.
- 机翼扭转调制用于俯仰和俯仰时刻的产生.
- 分析翅膀几何形状 (长度,前边厚度,曲率,静脉配置) 和执行方法.
- 控制表面互连的设计,以减轻交叉合效应.
主要成果:
- 可变的飞频率和翅膀扭转调制为稳定和敏捷的飞行提供了高的控制权.
- 翼扭曲调制有效地产生俯冲和曲折的时刻.
- 优化的翼设计和控制机制保持高控制权,在垂直力和功率效率的最小损失.
- 一个控制面互连成功地弥补了降低位权威和不利的滚动时刻.
结论:
- 开发的无尾控制系统适用于四翼FWMAV.
- 机翼扭转调制提供了一种可行的方法来产生足够的控制时刻.
- 该系统有效地减少交叉合效应,提高整体飞行性能.
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