共查询到19条相似文献,搜索用时 171 毫秒
1.
2.
3.
4.
5.
针对零件数据采集过程中可能出现的测量数据边界不完整的情况,提出一种点云部分缺失条件下边界曲面的直接拟合算法。对于两种不同的边界曲面类型,选择相应的方法自动构造贴近点云的基面;对点云中的点进行基面投影参数化的同时,运用改进的病态指标准则确定基面的病态控制顶点;在曲面拟合过程中,通过对病态控制顶点的抑制和加入离散边界约束条件,使得拟合得到的边界曲面在逼近点云的同时保持了良好的曲面内部品质,且和周围曲面之间达到近似G1连续。工程应用实例验证了提出算法的有效性及实际应用价值。 相似文献
6.
基于B样条曲面的点云孔洞拟合填充 总被引:1,自引:0,他引:1
为了后续曲面重构的需要,针对有孔洞的点云数据,提出了一种孔洞拟合填充的自适应方法。由于孔洞与其周围离散点有一定的连续性,该算法首先从孔洞周围已有的点云数据中选取离散点,用新的参数化方法对得到的离散点参数化后,用最小二乘法进行自适应曲面拟合,对得到的拟合曲面通过迭代法逐步逼近优化,考虑曲率变化的影响在曲面上取点,实现了孔洞光滑填充。实例表明,改进的参数化方法使算法的复杂度减低,进一步迭代优化提高了曲面拟合精度,在面上取点时考虑了曲率变化,因此该方法可以应用于具有复杂曲面形状的点云中的孔洞填充。 相似文献
7.
基于B样条曲面的点云孔洞拟合填充 总被引:1,自引:0,他引:1
为了后续曲面重构的需要,针对有孔洞的点云数据,提出了一种孔洞拟合填充的自适应方法.由于孔洞与其周围离散点有一定的连续性,该算法首先从孔洞周围已有的点云数据中选取离散点,用新的参数化方法对得到的离散点参数化后,用最小二乘法进行自适应曲面拟合,对得到的拟合曲面通过迭代法逐步逼近优化,考虑曲率变化的影响在曲面上取点,实现了孔洞光滑填充.实例表明,改进的参数化方法使算法的复杂度减低,进一步迭代优化提高了曲面拟合精度,在面上取点时考虑了曲率变化,因此该方法可以应用于具有复杂曲面形状的点云中的孔洞填充. 相似文献
8.
为在CAD/CAE/CAM中使用精确度和光顺性良好的机载薄壁共形件三维模型,提出了一种基于NURBS理论的机载薄壁共形件曲面拟合方法。首先利用基于特征点的斜率分割法对共形件点云数据进行精简,通过建立目标函数对边界点进行B样条曲线拟合,然后构建双三次Coons面作为基面并将点云数据向基面逼近,最后利用迭代优化得到曲面控制顶点,从而得到满足要求的曲面。分析结果表明:拟合后的曲面具有良好的精确度和光顺性。 相似文献
9.
10.
11.
提出一种自由曲面数控加工轨迹曲线计算方法。根据这一方法,可由自由曲面上一定数量的任意分布型值点来 计算曲面加工时的刀具曲线。算法的基本思想是,型值点影响并决定着其控制区域内的曲面形状,这种影响的大小与到 型值点的距离及权指数相关。分别给出了沿X向进给及Y向进给时刀具轨迹曲线的生成算法。讨论了算法中参数选取 对加工曲面形状及拟合精度的影响。 相似文献
12.
基于加权双向递推模型的自由曲面反向工程方法 总被引:2,自引:0,他引:2
提出了一种基于加权双向递推模型的自由曲面反向工程方法。根据这一方法,可由已采集到的自由曲面上一定数量的任意分布型值点来反向工程出自由曲面。加权双向递推模型的基本思想是,型值点影响并决定着其控制区域内的曲面形状,这种影响的大小与到型值点的距离及权指数相关。给出了将区域划分为m×n的矩形网格下沿x、y方向的加权递推模型。讨论了该方法中网格划分和权指数对反向工程曲面形状及精度的影响。 相似文献
13.
任意拓扑三角网格模型的Loop细分曲面重建系统 总被引:2,自引:0,他引:2
提出一种从任意拓扑密集的三角网格模型拟合Loop细分曲面系统,包含对原网格模型进行特征识别,把保持了原有特征的简化网格和拓扑优化所获得的网格作为拟合初始控制网格。系统通过对控制网格顶点的循环修正和局部自适应细分来求解最终拟合细分曲面控制网格,避免了求解线性方程组,提高了拟合曲面的质量,实现了在给定精度下用较少的控制网格反映物体细节特征的分片光滑(片内除奇异点C^1外其余C^2连续)的Loop细分曲面重建。实例表明,Loop细分曲面重建系统对于任意拓扑海量三角网格测量数据的细分曲面重建是高效可行的。 相似文献
14.
H. Park 《The International Journal of Advanced Manufacturing Technology》2001,18(7):474-482
Owing to their specific functionality, surfaces are often given as bivariate functions including non-polynomial or higher-orde polynomial terms. It is necessary to represent them in standard formats such as non-uniform rational B-splines (NURBS) for approximation. As most such surfaces require fine quality of surfacing and high precision of manufacturing, accuracy should be guaranteed in their representations. As high accuracy is likely to result in bulky and redundant representations, it is also important to make them more com-pact. For NURBS surfaces, control points must be reduced without sacrificing accuracy. This paper presents an approximate lofting method for B-spline surface fitting to a functional surface within a specified accuracy. It adopts adaptive sampling and multiple B-spline curve fitting. The method is very effective when the surface shape is longish or the cross-sectional curves vary regularly in shape along a specific direction. Some experimental results demonstrate its usefulness and quality.This revised version with a corrected online cover date was published online in April 2004. 相似文献
15.
论述了在凸凹模数控加工时如何处理测量数据点,生成边界曲线,边框曲面及拟合曲面的方法,讨论刀具运动轨迹的生成和编辑方法,并介绍数控加工数据转换技术在汽车覆盖件模具制造上的应用。 相似文献
16.
Lixin Cao Jian Liu 《The International Journal of Advanced Manufacturing Technology》2008,35(11-12):1053-1064
For given data points on different cylindrical section curves of marine propeller during the design period, the fair fitting method with the least squares of the cubic B-spline curve has been used to form cylindrical section curves with different radius. Then the control points of the cylindrical section curves were used as new data points to process fair fitting in another direction, and the pressure surface and the suction surface of the propeller can be acquired at last. Aims to overcome disadvantages of the present machining method of propeller, such as lower machining precision and efficiency, repeated clamping, and limited machining scope, a new machining method—the second order osculating machining method—has been presented. By using this method, not only the cylindrical cutter and the machined surface can keep line contact, but also the propeller can be machined with one clamping. It’s very suitable for the machining of propeller with larger projected area ratio and the machining precision and efficiency will be improved. 相似文献
17.
18.
Calculation of the unit normal vector using the cross-curve moving mask method for probe radius compensation of a freeform surface measurement 总被引:1,自引:0,他引:1
This paper proposes a cross-curve moving mask method to calculate the unit normal vector based on 5 or 9 data points of a freeform surface measurement for probe radius compensation. This is done in order to simplify the calculation and thus, produce a more efficient and time-saving process. Passing through the middle point and 4 or 8 neighboring points, two crossed curves – longitude and latitude can be constructed. The unit normal vector at the middle point can be determined by calculating the cross product of two tangent vectors along these two crossed curves. Different curve fitting methods for the curves passing through 5 or 9 data points, such as Bézier and B-spline methodologies, have been investigated. Three kinds of surfaces, namely, a spherical surface, a cosine-like surface and a shoe-shaped surface (hereby termed “shoe last”) are selected for evaluating the accuracy of the calculated unit normal vectors. 相似文献