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991.
以含盐染料废水为研究对象,应用商业化的卷式膜组件,研究了纳滤膜对染料和盐的截留特性.实验结果表明,纳滤膜对染料的截留率高达99%以上.当染料分子量高于膜截留分子量时,染料初始浓度和染料品种对染料截留率的影响甚小,盐浓度对染料截留也无明显影响,但对NaCl截留率影响显著.随料液中NaCl浓度的增加,盐截留率快速下降,当盐浓度达到3.5%时,NaCl的截留率低于25%.纳滤膜对染料的高截留率和对NaCl的低截留率,使得应用纳滤技术从含盐染料废水中回收染料具有较好的经济性和可行性.  相似文献   
992.
研究了使用AutoCAD和AutoLISP语言中进行服装衣片的计算机辅助绘图与设计的方法。文中给出了用AutoCAD的AutoLISP语言写所的程序模块,用该程序模块可以实现由服装的几个基本尺寸转换成衣片图并用绘图机或打印机输出衣片图,实现衣片的计算机辅助设计。  相似文献   
993.
合理的户型设计将成为未来住宅市场上的核心竞争力.通过分析当前张家口住宅产业发展现状和市场需求,提出了进行中小套型住宅的开发策略.  相似文献   
994.
随着城市化进程的加快,旧城改造力度也随之加大.结合张家口的古建筑特征,探讨了进行古建筑保护的原则.  相似文献   
995.
分析了山东省某测井公司放射工作人员职业健康检查结果。结果表明:(1)放射工作人员的血压异常率与年龄、工龄有关,随着年龄、工龄的增加而增高,差异显著;(2)不同年龄段间比较,肾功能异常率差异显著;(3)不同工龄段间比较,胸部X射线摄影异常率差异显著。结论认为,从事测井工作的放射工作人员长期接触低剂量辐射,应提高防护意识,...  相似文献   
996.
997.
A fixed-time sliding mode controller based plant/controller co-design scheme is developed for dual-motor driving systems. The proposed controller is fixed-time stable subject to unknown disturbances which guarantees the robustness of the proposed control scheme and a less conservative solution can be ensured by comparing with the conventional fixed-time convergence technique. Due to the existence of couplings between the plant and the controller, traditional design procedures in which the plant and the controller are designed sequentially and separately cannot guarantee the overall optimum of control systems. A co-design scheme based on the nested optimisation strategy is developed in this paper. With the nested optimisation strategy, the co-design solution can be achieved efficiently and reliably. A combined cost function considering both the plant and the controller is developed so that the largest load can be achieved without degrading the control performance. The fixed-time convergent controller is employed and considered into the co-design scheme. The gravitational search algorithm is adopted to optimise controller parameters in the co-design scheme. With the presented co-design method, the largest load of the studied system can be achieved with the satisfactory control performance. Contrastive Simulation and experimental results demonstrate the efficacy of the proposed controller and co-design scheme.  相似文献   
998.
In this paper, we introduce and investigate two new classes of meromorphic multivalent functions. Such results as subordination properties, coefficient inequalities, convolution properties and integral representations are proved. Several sufficient conditions for meromorphic multivalent starlikeness and convexity are also derived.  相似文献   
999.
Supervised dimensionality reduction with tensor representation has attracted great interest in recent years. It has been successfully applied to problems with tensor data, such as image and video recognition tasks. However, in the tensor-based methods, how to select the suitable dimensions is a very important problem. Since the number of possible dimension combinations exponentially increases with respect to the order of tensor, manually selecting the suitable dimensions becomes an impossible task in the case of high-order tensor. In this paper, we aim at solving this important problem and propose an algorithm to extract the optimal dimensionality for local tensor discriminant analysis. Experimental results on a toy example and real-world data validate the effectiveness of the proposed method.  相似文献   
1000.
In this article, the problem of finite‐time attitude‐tracking control for rigid spacecraft is addressed. Uncertainties caused by external disturbances, unknown inertial matrix, actuator failures, and saturation constraints are tackled simultaneously. First, a smooth function that is more qualified to approximate the standard saturation characteristics is presented to deal with the actuator saturation constraints. Second, a fast nonsingular terminal sliding mode (FNTSM) manifold is constructed as a foundation of controllers design. By incorporating the fuzzy logic system into FNTSM technique, a less demanding solution of coping with model uncertainties is provided because the requirement of a prior knowledge of unknown inertial parameters and external disturbances in many existing achievements is removed. To reduce the number of parameters to be estimated, the norm approximation approach is exploited. Subsequently, an antichattering attitude controller is presented such that all the tracking errors converge into arbitrary small domains around the origin in finite time. The result is further extended to obtain a fault‐tolerant controller against completely failed actuators. Finally, numerical simulation is conducted to verify the effectiveness of the proposed control scheme and comparison with relevant literature demonstrates its high performance. Furthermore, an experiment for the large satellite Hubble Space Telescope is carried out to validate the practical feasibility.  相似文献   
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