边缘信息对图像分割是十分重要的。把图像的边缘信息融入C-V模型(active contours without edges),提出一个新的几何模型,它同时利用同质区域信息和边缘信息使演化曲线在目标边缘处停止。实验显示:新模型能够克服C-V模型的一些缺点;在...边缘信息对图像分割是十分重要的。把图像的边缘信息融入C-V模型(active contours without edges),提出一个新的几何模型,它同时利用同质区域信息和边缘信息使演化曲线在目标边缘处停止。实验显示:新模型能够克服C-V模型的一些缺点;在减少分割时间的同时,对目标灰度不均匀或背景灰度不均匀、含弱边缘或强噪声的图像,分割效果不仅优于C-V模型,也优于C-V模型的两个最新改进模型(LBF和GACV)。展开更多
结冰会导致飞行安全包线收缩、严重威胁飞行安全,研究结冰后安全包线变化对于操纵应对策略设计及提高飞行安全具有重要意义。以美国国家航空航天局(NASA)的项目飞机GTM(Generic Transport Model)为研究对象,通过对飞机的气动参数进行多...结冰会导致飞行安全包线收缩、严重威胁飞行安全,研究结冰后安全包线变化对于操纵应对策略设计及提高飞行安全具有重要意义。以美国国家航空航天局(NASA)的项目飞机GTM(Generic Transport Model)为研究对象,通过对飞机的气动参数进行多项式拟合,建立了结冰飞机纵向通道的动力学模型。为了得到能随结冰程度变化的安全包线,将可达性分析理论引入到对结冰飞机着陆过程的安全性分析。提出将正向可达集与反向可达集的交集作为飞行安全包线,其中可达集的确定是基于水平集方法求解哈密尔顿-雅克比方程的最优解。最后针对不同程度的结冰条件进行了操纵时域验证,并提出了相应的操纵控制策略。研究结果表明,轻度结冰对安全包线影响较小,整个着陆过程的飞行状态始终能在最优控制指导下保持在安全包线以内;但对于重度结冰,飞行安全包线收缩严重,常规操纵已经很难使飞机达到着陆要求,需要进行飞行状态改出处理。研究结果为指导飞行操纵及实时包线保护打下基础。展开更多
The number of constraints imposed on the sur- face, the light source, the camera model and in particular the initial information makes shape from shading （SFS） very dif- ficult for real applications. There are a con...The number of constraints imposed on the sur- face, the light source, the camera model and in particular the initial information makes shape from shading （SFS） very dif- ficult for real applications. There are a considerable number of approaches which require an initial data about the 3D ob- ject such as boundary conditions （BC）. However, it is difficult to obtain these information for each point of the object Edge in the image, thus the application of these approaches is lim- ited. This paper shows an improvement of the Global View method proposed by Zhu and Shi [1]. The main improvement is that we make the resolution done automatically without any additional information on the 3D object. The method in- volves four steps. The first step is to determine the singular curves and the relationship between them. In the second step, we generate the global graph, determine the sub-graphs, and determine the partial and global configuration. The proposed method to determine the convexity and the concavity of the singular curves is applied in the third step. Finally, we apply the Fast-Marching method to reconstruct the 3D object. Our approach is successfully tested on some synthetic and real im- ages. Also, the obtained results are compared and discussed with some previous methods.展开更多
The principle aim of this essay is to illustrate how different phenomena is captured by different discretizations of the Hopf equation and general hyperbolic conservation laws. This includes dispersive schemes, shock ...The principle aim of this essay is to illustrate how different phenomena is captured by different discretizations of the Hopf equation and general hyperbolic conservation laws. This includes dispersive schemes, shock capturing schemes as well as schemes for computing multi-valued solutions of the underlying equation. We introduce some model equations which describe the behavior of the discrete equation more accurate than the original equation. These model equations can either be conveniently discretized for producing novel numerical schemes or further analyzed to enrich the theory of nonlinear partial differential equations.展开更多
文摘边缘信息对图像分割是十分重要的。把图像的边缘信息融入C-V模型(active contours without edges),提出一个新的几何模型,它同时利用同质区域信息和边缘信息使演化曲线在目标边缘处停止。实验显示:新模型能够克服C-V模型的一些缺点;在减少分割时间的同时,对目标灰度不均匀或背景灰度不均匀、含弱边缘或强噪声的图像,分割效果不仅优于C-V模型,也优于C-V模型的两个最新改进模型(LBF和GACV)。
基金Supported in part by Ministry of Science and Technology of China(2012BAJ15B04)by Research Grants Council of Hong Kong(PolyU 15223015+2 种基金PolyU 5249/12E)by National Natural Science Foundation of China(41331175)by Leading Talent Project of the National Administration of Surveying(K.SZ.XX.VTQA)
文摘结冰会导致飞行安全包线收缩、严重威胁飞行安全,研究结冰后安全包线变化对于操纵应对策略设计及提高飞行安全具有重要意义。以美国国家航空航天局(NASA)的项目飞机GTM(Generic Transport Model)为研究对象,通过对飞机的气动参数进行多项式拟合,建立了结冰飞机纵向通道的动力学模型。为了得到能随结冰程度变化的安全包线,将可达性分析理论引入到对结冰飞机着陆过程的安全性分析。提出将正向可达集与反向可达集的交集作为飞行安全包线,其中可达集的确定是基于水平集方法求解哈密尔顿-雅克比方程的最优解。最后针对不同程度的结冰条件进行了操纵时域验证,并提出了相应的操纵控制策略。研究结果表明,轻度结冰对安全包线影响较小,整个着陆过程的飞行状态始终能在最优控制指导下保持在安全包线以内;但对于重度结冰,飞行安全包线收缩严重,常规操纵已经很难使飞机达到着陆要求,需要进行飞行状态改出处理。研究结果为指导飞行操纵及实时包线保护打下基础。
文摘The number of constraints imposed on the sur- face, the light source, the camera model and in particular the initial information makes shape from shading （SFS） very dif- ficult for real applications. There are a considerable number of approaches which require an initial data about the 3D ob- ject such as boundary conditions （BC）. However, it is difficult to obtain these information for each point of the object Edge in the image, thus the application of these approaches is lim- ited. This paper shows an improvement of the Global View method proposed by Zhu and Shi [1]. The main improvement is that we make the resolution done automatically without any additional information on the 3D object. The method in- volves four steps. The first step is to determine the singular curves and the relationship between them. In the second step, we generate the global graph, determine the sub-graphs, and determine the partial and global configuration. The proposed method to determine the convexity and the concavity of the singular curves is applied in the third step. Finally, we apply the Fast-Marching method to reconstruct the 3D object. Our approach is successfully tested on some synthetic and real im- ages. Also, the obtained results are compared and discussed with some previous methods.
基金the National Science Foundation under Grant DMS05-05975.
文摘The principle aim of this essay is to illustrate how different phenomena is captured by different discretizations of the Hopf equation and general hyperbolic conservation laws. This includes dispersive schemes, shock capturing schemes as well as schemes for computing multi-valued solutions of the underlying equation. We introduce some model equations which describe the behavior of the discrete equation more accurate than the original equation. These model equations can either be conveniently discretized for producing novel numerical schemes or further analyzed to enrich the theory of nonlinear partial differential equations.
