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231.
范梅 《西安航空技术高等专科学校学报》2015,(1)
分部积分法是求不定积分的重要方法之一,也是求不定积分中的一个难点。在教学中,采用简单可行的方法准确的确定哪个函数为 u ,哪个函数为 dv ,再用简便的运算方法和技巧,可以快速求出 v。 相似文献
232.
双语词典资源对于自然语言处理研究的巨大价值已经得到越来越多的认可,尤其是在机器翻译、跨语言信息检索等方面。传统人工构建词典存在规模小、时效性差、语种不够灵活等问题,而且耗费大量的人力财力。提出了一种基于web的获取日英释义的新方法。该方法采用双向融合计算技术,首先对日语单词进行启发式搜索,在返回的网页摘要中应用基于距离和频率的方法挖掘出其候选英语单词;在第二阶段对候选英语单词进行二次搜索,并对两个阶段的结果进行融合计算来确定日英释义。 相似文献
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235.
某卫星在进行真空热试验时,对热流提出了三个方面的新要求:(1)对某些热流要求较低的加热区的加热笼进行修改,提高其低热流实现能力;(2)减小支架漏热;(3)实时计算设计热流和实际热流的周期积分偏差。由于修改时的约束条件较多,新的要求的满足非常困难。经过努力,最终解决了这些问题,通过对某些加热笼采取加热带双面涂黑漆的方法,实现了低热流;经过计算和针对性的设计,支架漏热不超过0.1188W;同时实现了设计热流与实际热流周期积分偏差的实时计算。 相似文献
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237.
Inner Attitude Integration Algorithm Based on Fault Detection for Strapdown Inertial Attitude and Heading Reference System 总被引:1,自引:0,他引:1
This article proposes a new inner attitude integration algorithm to improve attitude accuracy of the strapdown inertial attitude and heading reference system(SIAHRS), which, by means of a Kalman filter, integrates the calculated attitude from the accelerometers in inertial measuring unit(IMU), called damping attitudes, with those from the conventional IMU. As vehicle's acceleration could produce damping attitude errors, the horizontal outputs from accelerometers are firstly used to judge the vehicle's motion so as to determine whether the damping attitudes could be reasonably applied. This article also analyzes the limitation of this approach. Furthermore, it suggests a residual chi-square test to judge the validity of damping attitude measurement in real time, and accordingly puts forward proper information fusion strategy. Finally, the effectiveness of the proposed algorithm is proved through the experiments on a real system in dynamic and static states. 相似文献
238.
谢智慧 《长沙航空职业技术学院学报》2008,8(4):12-15
提出理实一体教学改革的具体思路,探讨“项目引导,任务驱动,综合测评”在课程教学改革中的具体实施方法。 相似文献
239.
As an efficient artificial truncating boundary condition, conformal perfectly matched layer (CPML) is a kind of multilayer anisotropic absorbing media. To reduce computing effort of CPML, this article proposes a layer-oriented element integration algorithm. In this algorithm, the relative dielectric constant and permeability are considered as constants for each the very thin monolayer of CPML, and the element integration of multilayer along the normal direction is substituted by the element integration of monolayer. The CPML is divided into multilayer elements, whose element matrixes are evaluated by monolayer integration. Numerical examples show that the layer-oriented element integration algorithm is reliable and the CPML formed with this algorithm possesses high-efficient absorbing performance. 相似文献
240.
The aim of this work is to realize a new numerical program based on the development of a mathematical model allowing determining the parameters of the supersonic flow through a conical shock under hypothesis at high temperature, in the context of correcting the perfect gas model. In this case, the specific heat at constant pressure does not remain constant and varies with the increase of temperature. The stagnation temperature becomes an important parameter in the calculation. The mathematical model is presented by the numerical resolution of a system of first-order nonlinear differential equations with three coupled unknowns for initial conditions. The numerical resolution is made by adapting the higher order Runge Kutta method. The parameters through the conical shock can be determined by considering a new model of an oblique shock at high temperature. All isentropic parameters of after the shock flow depend on the deviation of the flow from the transverse direction. The comparison of the results is done with the perfect gas model for low stagnation temperatures, upstream Mach number and cone deviation angle. A calculation of the error is made between our high temperature model and the perfect gas model. The application is made for air. 相似文献