俄交变中磁标准装置研究

介绍了从俄罗斯引进的用于交变磁场的国防标准——交变中磁标准装置的基本工作原理,以及对其设计方案的剖析。该标准装置工作频率（20～1 000）Hz,复现交变磁场强度（0.1～1 000）mT,在这一领域内代表国际最高水平。通过对其信号获取、磁场感应信号的放大处理、大电流的产生办法、安全互锁设计,以及整体系统理论计算的分析,为该领域内标准装置的国产化提供理论基础,具有较好的实用价值。     

基于宽带宽测量的姿态确定方法

针对由飞轮等星上高速旋转部件所引起的高频姿态和指向抖动,提出一种基于磁流体动力学特性的角位移敏感器用于星上高精度宽带宽的微振动测量,以弥补常规姿态测量系统测量频带低,动态范围有限的缺点.介绍以扩展姿态确定带宽为基础的高精度姿态确定方法.给出了以陀螺、星敏及ADS测量信息为基础的宽带宽的姿态确定方法及系统的模型,采用了卡尔曼滤波来确定卫星姿态.仿真分析结果表明存在高频姿态抖动的情况下,宽带宽的姿态确定方法的估计精度优于传统的姿态确定方法,由此验证了宽带宽的姿态确定方法的有效性及精确性.     

基于线性模型的风电场发电量计算与分析

针对相对平坦地形,采用线性化流体方程描述流场,并根据大气边界层特性进一步简化计算方法,即利用所谓地形影响系数快速求解感兴趣点(一般为风机位置)的流动速度;针对尾流影响,采用工程上广泛使用的修正Park模型来求解,尾流线性叠加并忽略较弱的尾流影响。文中介绍了一个已建典型海滨风电场的装机规模、地表粗糙度以及测风情况,并以此风电场为算例采用不同测风数据进行发电量计算,预测结果与实际发电量较好地吻合。最后探索了算例风电场各风机发电量不均衡原因,提出地形图大小对风场模拟准确性的影响,并从工程设计角度提出具体意见。     

Three-dimensional path planning for unmanned aerial vehicle based on interfered fluid dynamical system

This paper proposes a method for planning the three-dimensional path for low-flying unmanned aerial vehicle(UAV) in complex terrain based on interfered fluid dynamical system(IFDS) and the theory of obstacle avoidance by the flowing stream. With no requirement of solutions to fluid equations under complex boundary conditions, the proposed method is suitable for situations with complex terrain and different shapes of obstacles. Firstly, by transforming the mountains, radar and anti-aircraft fire in complex terrain into cylindrical, conical, spherical, parallelepiped obstacles and their combinations, the 3D low-flying path planning problem is turned into solving streamlines for obstacle avoidance by fluid flow. Secondly, on the basis of a unified mathematical expression of typical obstacle shapes including sphere, cylinder, cone and parallelepiped, the modulation matrix for interfered fluid dynamical system is constructed and 3D streamlines around a single obstacle are obtained. Solutions to streamlines with multiple obstacles are then derived using weighted average of the velocity field. Thirdly, extra control force method and virtual obstacle method are proposed to deal with the stagnation point and the case of obstacles’ overlapping respectively. Finally, taking path length and flight height as sub-goals, genetic algorithm(GA) is used to obtain optimal 3D path under the maneuverability constraints of the UAV. Simulation results show that the environmental modeling is simple and the path is smooth and suitable for UAV. Theoretical proof is also presented to show that the proposed method has no effect on the characteristics of fluid avoiding obstacles.     

Semi-analytic Solution of Steady Temperature Fields During Thin Plate Welding

Usually, it is very difficult to find out an analytical solution to thermal conduction problems during high temperature welding. Therefore, as an important numerical approach, the method of lines (MOLs) is introduced to solve the temperature field characterized by high gradients. The basic idea of the method is to semi-discretize the governing equation of the problem into a system of ordinary dif-ferential equations (ODEs) defined on discrete lines by means of the finite difference method, by which the thermal boundary condition with high gradients are directly embodied in formulation. Thus the temperature field can be obtained by solving the ODEs. As a numeri-cal example, the variation of an axisymmetrical temperature field along the plate thickness can be obtained.     

Hall MHD reconnection with an initial guide field By0

An uniform out-of-plane magnetic field component B_y0 is added to the equilibrium Harris sheet with plasma β = 0.5 and L_c = 0.5d_i (where L_c is the half-width of the equilibrium current layer and d_i is the ion inertial length). Driven by the continuous boundary inflows, the magnetic reconnections with the guide field B_y0/B₀ ranging from 0 to 4.0 are investigated using a 2.5D Hall magnetohydro-dynamic (MHD) code developed from a multi-step implicit scheme. The features of the reconnection field are substantially altered in the presence of the guide field. The openness of the magnetic separatrix angle is slightly reduced and the anti-symmetric quadrupolar structure of B_y field and the symmetric distribution of plasma pressure P are replaced by an asymmetric B_y four-wing structure and an asymmetric P plot as a non-zero B_y0 is added. The decoupling of electrons and ions also occurs near the X line in the case with a finite B_y0, but the effect of initial B_y0 on the electron flow is greater than that on the ion flow. The reconnection rates at the X-line drops from 0.151 to 0.06, namely, ∂A/∂t is reduced by a factor of 2.5 as B_y0/B₀ increases from 0 to 4.0. The reduction of reconnection rate might be related to the reducing openness of reconnection layer with the increasing B_y0.     

浅论红色文化产品的创新设计与价值实现——以河北省为例

本文通过对红色文化领域物质与精神两方面产品的研发现状与经验的分析,结合未来设计领域的发展趋势,提出开发体验性和个性化的红色文化产品。以河北省为例,探讨如何在实现红色文化产品的价值同时,更好的使红色文化为当代精神文明建设服务。     

Planetary Magnetic Dynamo Effect on Atmospheric Protection of Early Earth and Mars

In light of assessing the habitability of Mars, we examine the impact of the magnetic field on the atmosphere. When there is a magnetic field, the atmosphere is protected from erosion by solar wind. The magnetic field ensures the maintenance of a dense atmosphere, necessary for liquid water to exist on the surface of Mars. We also examine the impact of the rotation of Mars on the magnetic field. When the magnetic field of Mars ceased to exist (about 4 Gyr ago), atmospheric escape induced by solar wind began. We consider scenarios which could ultimately lead to a decrease of atmospheric pressure to the presently observed value of 7 mbar: a much weaker early martian magnetic field, a late onset of the dynamo, and high erosion rates of a denser early atmosphere.     

高斯激光束照射圆柱体一端面上引起温升和热应力的分析

激光加热应用很广，热应力是一常见现象。本文讨论的内容是来自辐射加固技术和激光武器效应中遇到的一个问题，因此，对其剖析具有很大的实用价值和理论意义。     

某型飞机导航误差对CCD稳瞄系统目标搜索域的影响

分析了DG-1型多普勒／GPS组合导航系统，在不同工作方式下导航误差所引起的搜索方位角的误差；讨论了由于搜索方位角的变化引起的搜索域的变化。通过对机理的研究提出了解决办法。