基于一类时变广义系统的产业结构预测及控制模型

本文建立了经济增长与动态产业结构预测模型,并得了动态产业结构协调发展的充要条件,从而利用最优控制方法讨论了产业结构调整问题。     

全国国有及规模以上非国有工业企业经济发展情况综合分析

本文采用熵权法和主成份投影法对全国国有及规模以上非国有工业企业的经济发展情况进行了综合分析和评价并排序     

主成份分析在证券市场个股评析中的应用

本文利用主成份分析方法 ,对证券市场上 31种股票进行综合评价 ,通过使用统计软件SAS进行计算和分析 ,提出用第一主成份作为个股业绩的度量 ,得到了这些股票 1997年上半年财务状况的排列次序     

用光学参量啁啾脉冲放大技术产生TW级激光脉冲系统的最优化设计

用数值模拟的方法,给出了一种适合以纳秒级的高功率钕玻璃激光系统为抽运源的光学参量啁啾脉冲放大(OPCPA)系统的最优化设计.该系统主要由一级LBO预放大器和一级LBO主放大器组成.数值模拟结果表明该系统能够把纳焦级能量的飞秒脉冲放大到焦级,从而产生几十个太瓦(1012W)的脉冲输出.这一结果为进一步利用OPCPA技术放大飞秒脉冲产生拍瓦(1015W)的超短超强激光脉冲输出奠定了基础,从而为强场科学研究提供崭新的技术手段.     

一种带锁相放大的高稳定温度控制电路

介绍一种高稳定的温度控制电路 ,该电路采用锁相放大方法对温度的微小变化进行检测 ,利用半导体制冷器进行温度的实时控制。在室温环境下 ,其温度稳定度可到1 0 - 3K量级。     

重建极性连续统理论的基本定律和原理(Ⅹ)——主均衡定律

通过对诸主均衡定律和应用Noether定理得出的守恒定律进行比较,自然地导出微极连续统力学的1个统一的主均衡定律和6个物理上可能的均衡方程．其中,通过扩展众所周知和惯用的能量动量张量的概念,得到相当一般的定名为能量-动量的、能量-角动量的和能量-能量的守恒定律和均衡方程．显然,在这后3种情况下的主均衡定律中,物理场量是难以凭借直觉假定出来的．最后,作为特殊情形,直接推演出若干现有的结果．     

Quantum Privacy Amplification for a Sequence of Single Qubits

We present a scheme for quantum privacy amplification （QPA） for a sequence of single qubits. The QPA procedure uses a unitary operation with two controlled-not gates and a Hadamard gate. Every two qubits are performed with the unitary gate operation, and a measurement is made on one photon and the other one is retained. The retained qubit carries the state information of the discarded one. In this way, the information leakage is reduced. The procedure can be performed repeatedly so that the information leakage is reduced to any arbitrarily low level. With this QPA scheme, the quantum secure direct communication with single qubits can be implemented with arbitrarily high security. We also exploit this scheme to do privacy amplification on the single qubits in quantum information sharing for long-distance communication with quantum repeaters.     

基于广义判别分析的光谱分类

提出了基于广义判别分析(generalized discriminant analysis, GDA)方法对恒星(Star)、星系(Galaxy)和类星体(Quasars)的光谱进行分类。广义判别分析将核技巧与Fisher判别分析结合起来,通过非线性映射将样本集映射到高维特征空间F,在F空间中进行线性判别分析。实验对比了LDA, GDA, PCA, KPCA算法对于恒星、星系和类星体的光谱分类性能。结果表明基于GDA的算法对于这3种类型光谱的分类正确率最高,LDA次之;尽管KPCA也是一种基于核的方法,但是选择主成分个数较少时效果较差,甚至低于LDA;基于PCA的分类效果最差。     

重离子碰撞中超重核的形成机制(英文)

在双核模型框架下,用数值解主方程方法计算了超重核的熔合几率。 明确描述了包含能量、角动量和碎片形变弛豫的相对运动,并与核子扩散过程相耦合。因此,用微观方法推导出的核子跃迁几率是与时间相关的。所计算的以Pb为靶的冷熔合超重核形成截面和以48Ca为弹核的热熔合超重核形成激发函数与已知的实验值在合理的范围内符合。In the dinuclear system conception, the master equation is solved numerically to calculate the fusion probabilities of super heavy nuclei. The relative motion concerning the energy, the angular momentum and the fragment deformation relaxations is explicitly treated to couple with the diffusion process. The nucleon transition probabilities, which are derived microscopically, are related with the energy dissipation of the relative motion, thus they are time dependent. The formation cross sections of the super heavy nuclei from Pb based cold fusion and excitation functions from 48Ca induced hot fusion are reasonably consistent with known experimental data.     

加速器驱动快/热耦合次临界系统的概念设计

对加速器驱动快／热耦合次临界系统进行了概念设计研究。在该系统中,内区的快包层和外区的热包层是相互独立的,快、热包层之间为空腔和B4C包层以实现单向耦合。快包层装以合金（MA＋Pu）Zr为燃料,热包层初始循环装以氧化物（Th＋Pu）O₂为燃料,平衡循环装以（Th＋^233 U＋Pu）O2为燃料。^99Tc,^129I和^135Cs分别以单质、NaI和CsCl的形式装入热包层。该系统具有较高的能量放大倍数、嬗变效率和燃料转换比:系统能量放大系数不低于320;锕系元素（MA）和裂变产物（FP）的嬗变支持比分别为1个和2个压水堆;热包层的燃料转换比为0．715。 Accelerator driven coupled fast/thermal subcritical system is conceptually designed. In the system, the inner/fast blanket and the outer/thermal blanket are separated each other by large vacuum and B4C coating for on edirection coupling. The metal type fuel （MA ＋ Pu）Zr is loaded into the fast blanket. The oxide type fuels （Th ＋ Pu） O2 and （Th ＋ ^233U ＋ Pu）O2 are loaded into the thermal blanket during the initial cycle and the equilibrium cycle, respectively. ^99Tc, ^129I and ^135Cs are loaded respectively in the form of pure technetium metal, sodium iodide and cesium chlorine into the thermal blanket. The system has good transmutation efficiency, high energy amplification factor and good fuel conversion ability: the energy amplification factor is above 320; the transmutation support ratios of MA and FP are about 1.0 and 2.0 PWRs respectively; the fuel conversion ratio in the thermal blanket is about 0. 715.