基于节点曲率向量的可变翼前沿的形态重构.
Jie Zeng1, Qingfeng Zhu1, Yueqi Zhao1
1State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.
Biomimetics (Basel, Switzerland)
|April 26, 2024
概括
这项研究引入了一种用于准确重建可变翼前端形状的新方法. 基于节点曲率向量的曲率传播方法 (NCV-CPM) 提高了生物灵感自适应控制系统的准确性.
科学领域:
- 航空航天工程 航空航天工程
- 机械工程 机械工程
- 生物模拟学是一种生物模拟学.
背景情况:
- 准确地获得可变的翅膀前端形态是生物灵感的自适应控制的关键.
- 现有的方法,如基于线性插曲的曲率传播方法 (LI-CPM),存在累积错误,特别是在未连接的传感器位置.
研究的目的:
- 为可变的翼前边提出一种新的形态重建方法.
- 为了提高曲率计算的准确性,并减少结构健康监测的应变场重建中的错误.
主要方法:
- 使用基于节点曲率向量的曲率传播方法 (NCV-CPM).
- 建立了应变弧曲率函数,以减轻表面曲率角度对准确度的影响.
- 使用高阶曲率配合函数来确定弧线段节点的曲率向量.
- 集成的曲率-应变功能用于翼前端应变场重建.
- 使用粒子群算法优化传感点分布,以减少网络复杂性.
主要成果:
- 与传统LI-CPM相比,显著提高了形态重建的准确性.
- 减少在未连接传感器位置的曲率计算中的累积错误.
- 为结构健康监测证明了改进的应变场重建.
结论:
- NCV-CPM提供了一种卓越的方法,用于精确地获取可变翼前边的形态.
- 该方法支持先进的结构健康监测和航空航天应用中的自适应控制.
- 优化传感器位置进一步提高了系统的效率和有效性.
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