摘要
面向高性能飞行器结构形态主动监测研究背景,以光纤光栅柔性细杆机敏结构为研究模型对象,侧重于空间正交曲率信息的三维曲线重构方法分析和研究.在简述基于正交分布式光纤光栅传感阵列曲率检测原理基础上,进行空间三维曲线重构方法分析,并给出了详细的算法过程和实现步骤,同时进行了离散曲率连续化方法分析;基于V isual C++开发平台及OpenGL技术,针对方法研究结果与算法分析过程,开发可视化仿真实验环境进行了实验分析与验证,基于3种离散曲率连续化方法进行图形重构效果对比;实验分析结果不仅表明了3维重构方法与实现过程的有效性,而且获得了离散曲率连续化方法上的相关有益结果.
Facing the background of active structural shape monitoring for high performance aircraft,a 3D curve reconstruction method based on the orthogonal curvatures is analyzed and researched in this paper,taken flexible fiber Bragg grating rod as the research object.With the curvatures detection principle of the orthogonally distributed Fiber Bragg Grating briefly introduced,the reconstruction method for three-dimensional curve is analyzed,while the detailed algorithmic procedure,implementation steps and analysis of continuum method for discrete curvature are given.Then a visual simulation platform is developed to analyze and verify the algorithmic procedure and the methodology with Visual C++ and OpenGL employed.The performance comparison of the three type of continuum methods for discrete curvature,suggests that not only the 3D curve reconstruction method and its implementation proposed in this paper is effective but also related beneficial results about continuum method for discrete curvature are obtained.
出处
《应用基础与工程科学学报》
EI
CSCD
2011年第2期305-313,共9页
Journal of Basic Science and Engineering
基金
国家自然科学基金重大研究计划资助项目(90716027)
上海市教委科研创新重点项目(09ZZ88)
上海市教委"机械电子工程"创新团队资助
上海大学"十一五"211建设项目
上海市电站自动化技术重点实验室资助
关键词
高性能飞行器
光纤智能结构
曲率信息
空间曲线
重构
high performance aircraft
fiber optic intelligent structures
curvature information
space curve
reconstruction