摘要
针对机翼变形中的传感器最优配置问题,建立悬臂梁模型,基于Ko位移理论的形变位移算法估计机翼变形,通过求解双目标0-1规划模型实现了传感器最优配置.计算结果验证了方法的正确性.
Cantilever beam model was built for the problem of optimal sensors design in airfoil deformation.After that, algorithm was designed by way of Ko displacement theory to estimate airfoil deformation.The optimal sensors was obtained by solving bi-objective 0-1 optimization model,the numerical results proved the accuracy of proposed approaches.
出处
《高师理科学刊》
2015年第12期6-9,共4页
Journal of Science of Teachers＇College and University
基金
西安电子科技大学本科教育质量提升计划资助项目
关键词
机翼变形
传感器
悬臂梁
分段插值
airfoil deformation
sensor
cantilever beam
piecewise interpolation
