多项式方程区间内重根的快速判定和裁剪

目的多项式求实根问题有着广泛的应用。改进传统的裁剪方法,在多项式重根的情形下,保持计算稳定性的同时显著地提高相应的收敛阶。方法提出了基于R~3空间内的3次裁剪方法。该方法继承了传统裁剪求根方法的优点,充分利用了Bernstein基函数较好的计算稳定性,同时给出简单方法判别重根的存在性,从而使得重根的情形可以转化为单根的情形。结果与已有的基于R~1和R~2空间的3次裁剪方法相比,本文方法可以具有更好的逼近效果。单根情形下,本文方法与基于R~2空间的3次裁剪方法同时具有5次收敛阶,略高于基于R~1空间3次裁剪方法的4次收敛阶;m(≥2)重根情形下,本文方法理论上可具有5次收敛阶,明显优于已有的基于R~1和R~2空间的3次裁剪方法的4/m或5/m收敛阶。基于R~1,R~2和R~3空间的3次裁剪方法的计算时间复杂度大致相当,均为O(n~2)。结论本文方法可以快速判定重根的情形,同时具有更高的收敛阶和更好的逼近效果。     

基于测地距离的KPCA人脸识别

针对人脸检测数据集中的信息均为高维特征向量且人脸识别易受表情变化影响等问题,本文提出一种基于测地距离的KPCA人脸识别方法,该方法利用非线性方法提取主成分。先采用KPCA方法把人脸数据映射到高维空间,进而在高维空间中提取人脸的主成分,其中核函数为多项式核函数;然后引入测地距离替换原来的欧氏距离进行相似度量,其能更准确地测量出两像素点间的实际距离,使得人脸识别率受表情变化影响小。该方法不但可以实现降维,而且还能达到有效提取特征的目的。在ORL人脸库上的实验结果表明,该方法的识别率明显优于PCA、KPCA等方法的识别率。     

多参数融合的飞行品质评估模型的建立

目前航空管理机构与航空公司进行飞行品质评估主要是依据经验与简单飞行参数统计数字,这样做难以得出科学、客观的评估结果。基于提升全行业安全保障能力和运行品质的需求,研究了利用计算机技术对飞行品质进行综合评估的方法。选取了理想值逼近法作为飞行品质综合评估的手段,结合波动通道模型作为飞行品质评估的理论基础,基于提出的飞行品质评估模型对飞行品质评估系统进行了设计。对真实的飞行参数数据建立综合评估模型,同时考察多次航班的多个飞行参数,给出综合的飞行品质评估结论,为飞行评估、训练提供理论基础和科学的评判方法。     

电力无线通信异构多网共存环境中的网络选择算法

综合考虑电力业务需求和无线专网性能因素,针对邻域网、LTE无线专网、WiMAX无线专网和230 MHz无线专网等构成的异构多网混合共存场景,提出一种网络选择算法。该算法以AHPTOPSIS算法为基础,首先构建能表征候选网络与决策属性之间关系的决策矩阵,归一化处理获得归一化决策矩阵;利用AHP算法,依据不同业务类型下决策属性与网络性能之间的相对关系定义权重,对归一化决策矩阵加权获得加权归一化决策矩阵;然后对TOPSIS算法进行改进,依据加权归一化决策矩阵确定正负理想值,利用正理想值与候选网络之间的最小距离以及负理想值与候选网络之间的最大距离确定理想网络,计算各候选网络与理想网络之间的有效距离;据此执行候选网络排序和最佳网络选择,以避免运行TOPSIS算法可能存在的排序异常。仿真结果表明,该算法能根据电力业务需求对候选网络进行正确排序和最优选择,且能在满足业务服务质量的同时,提高资源利用率。     

基于变差函数全局纹理增强的结构相似度图像质量评价

为解决结构相似度算法的图像质量评价缺陷,提出了一种基于变差函数全局纹理增强的结构相似度图像质量评价。该方法首先利用改进的对数变差函数模型提取原图像和失真图像在水平0°、垂直90°和对角45°、135°四个方向的纹理信息特征,然后分别求出对应的纹理增强图像,最后改进SSIM中的结构信息来确定纹理区域的明显失真,计算得到整幅图像的VSSIM值。目前大多数的全参考评价方法不能对数据库中的所有失真类型进行评价,只能对某一类固定的失真类型来评价。本方法对LIVE数据库中的五种失真类型都适用,仿真实验表明,该算法对五种不同失真类型的评价结果具有一定的合理性,并且与主观评价数据库较为一致,其性能也优于其他质量评价模型。     

具有自动加载功能的SPI总线控制器设计与验证

本文结合设计需求,提出了一种SPI主模式的接口电路设计,使其可以在多种SPI传输模式下进行数据的传输,且针对实时信息处理占用时间较长的不足,采取信息自动加载方法,有效降低了处理器占用时间.设计并搭建仿真验证平台对其进行验证.仿真测试结果表明,该SPI总线接口电路满足实际应用需求.     

Discrete time sliding mode control with reduced switching – a new reaching law approach

In this paper, a novel reaching law for discrete‐time variable structure systems is proposed. It ensures that the representative point (state) of the controlled plant approaches the switching plane in finite time and then crosses it in every subsequent step. Moreover, the proposed reaching law ensures that for the nominal plant the absolute value of the sliding variable asymptotically decreases to zero, and for the perturbed plant, it converges to a smaller interval around zero than with the application of previously proposed reaching laws. The control method proposed in this paper guarantees asymptotic stability of the nominal system and uniform ultimate boundedness of the perturbed one. Furthermore, the method ensures that the sliding variable rate of change (i.e. the difference between its values at any two subsequent sampling instants) is bounded by design parameters, which do not depend on the system initial conditions. This is a highly desirable property, as it results in a priori specified, ‘almost’ constant convergence rate of the sliding variable when the system state is far off the switching plane and helps enforce state constraints in the system. Copyright © 2014 John Wiley & Sons, Ltd.     

Robust cascaded automatic cruise control of electric vehicles

This article focuses on automatic cruise control for electrically driven vehicles. The objective is to track a given vehicle‐velocity profile. For this type of application, the so‐called wheel slip plays a key role, as it is a measure for the force transmitted from the wheel to the road. Conventional wheel‐ slip controllers are usually activated if the absolute value of the slip exceeds pre‐assumed thresholds. Furthermore, it is distinguished between a braking and acceleration maneuver using separately designed and implemented controllers. In contrast, the proposed concept requires neither an activation strategy for the slip controller nor a distinction between braking and acceleration. The cascaded control structure is based upon adaptive‐gains super twisting sliding‐mode algorithm, and the friction force estimator is realized as a second‐order sliding‐mode observer with constant gains. The effectiveness and robustness of the proposed concept are demonstrated in numerical simulations using a complex multibody vehicle model. Copyright © 2015 John Wiley & Sons, Ltd.     

Tethered space orientation via adaptive sliding mode

Here, we study the problem of a rotating tethered satellite system (TSS) orientation. The rotation TSS is used for propellantless delivery of the payload from low earth orbits to geostationary orbits or other transfer orbits. Driving the angular positions to correct desired orientation in rendezvous and tossing moments, in fact, is important operation in many real sceneries. We suggest the mathematical model describing the dynamics of TSS and catch mechanism/payload rendezvous with external disturbance terms. Here is shown that using sliding mode control (SMC), we are able to control successfully the position of TSS. The conventional and adaptive versions of SMC are considered. We show that SMC with the gain matrix adaptation based on the equivalent control method can significantly reduce the undesirable chattering effect provoking possible damages of TSS. Copyright © 2015 John Wiley & Sons, Ltd.