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排序方式: 共有817条查询结果,搜索用时 15 毫秒
131.
杨海丽 《华北航天工业学院学报》2002,12(1):53-55
这篇文章从词汇的重要性及教学实践入手,概括地总结了四种词汇记忆的有效方法,意在更好的帮助学生在短时间内迅速地扩大词汇量。 相似文献
132.
杨居奎 《运载火箭与返回技术》2006,27(2):14-17
文章介绍了3种平行光管中大口径反射镜的安装方法,并通过力学分析进行比较,给出了各自的优缺点。 相似文献
133.
毕丽 《华北航天工业学院学报》2002,12(4):51-53
精读课的主要任务是词汇,语法和语篇,围绕这三大任务采取灵活多样的教学方法,来调动学生的学习积极性,培养自主学习能力,从而提高教学质量。 相似文献
134.
A Class of TVD Type Combined Numerical Scheme for MHD Equations With a Survey About Numerical Methods in Solar Wind Simulations 总被引:3,自引:0,他引:3
It has been believed that three-dimensional, numerical, magnetohydrodynamic (MHD) modelling must play a crucial role in a
seamless forecasting system. This system refers to space weather originating on the sun; propagation of disturbances through
the solar wind and interplanetary magnetic field (IMF), and thence, transmission into the magnetosphere, ionosphere, and thermosphere.
This role comes as no surprise to numerical modelers that participate in the numerical modelling of atmospheric environments
as well as the meteorological conditions at Earth. Space scientists have paid great attention to operational numerical space
weather prediction models. To this purpose practical progress has been made in the past years. Here first is reviewed the
progress of the numerical methods in solar wind modelling. Then, based on our discussion, a new numerical scheme of total
variation diminishing (TVD) type for magnetohydrodynamic equations in spherical coordinates is proposed by taking into account
convergence, stability and resolution. This new MHD model is established by solving the fluid equations of MHD system with
a modified Lax-Friedrichs scheme and the magnetic induction equations with MacCormack II scheme for the purpose of developing
a combined scheme of quick convergence as well as of TVD property. To verify the validation of the scheme, the propagation
of one-dimensional MHD fast and slow shock problem is discussed with the numerical results conforming to the existing results
obtained by the piece-wise parabolic method (PPM). Finally, some conclusions are made.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
135.
M. K. Tleulinov 《Russian Aeronautics (Iz VUZ)》2009,52(2):158-164
A method of direct integration with respect to time is proposed to solve dynamic problems of structural mechanics and comparison with the well-known methods is presented. 相似文献
136.
Σ-演算是并发演算CC的子理论,集中体现CC中的并行运算部分的特征。本文将并发通信系统看作是由状态加变换构成的动态系统,建立了Σ-演算的范畴模型(Categorical ModeI),其基本思想是:把Σ-演算中的公式对应于范畴构造中的对象(Objects),Σ-演算中的推演对应于范畴中的态射(Morphisms),从而通过Σ-演算的结构操作语义自然地得到一种范畴结构。这种方法可以推广到其它并发理论之中,例如网论和逻辑方法(如线性逻辑Linear Logic),从而范畴论可以作为描述并发、通信和非确定性行为的统一的形式化框架。 相似文献
137.
Mode decision-maker is a critical component in the logic-based Integrated Estimation and Guidance(IEG) system. For the best possible estimation and guidance performance, the mode decision delay of the mode decision-maker should be limited to a range as small as possible. This paper presents a numerical method for computing the maximal admissible mode decision delay that varies with time-to-go. Particular attention has been paid to highly maneuvering target interception in terminal guidance. The results of this research offer useful guidelines for the design of the mode decision-maker in IEG systems. 相似文献
138.
考虑弹性高超声速飞行器纵向动力学模型,提出了一种基于时标分解的智能控制方法。考虑刚体状态和弹性模态具有不同的时标特性,采用奇异摄动理论进行快慢时标分解,将模型转换为刚体慢变子系统和弹性快变子系统。针对刚体子系统考虑动力学不确定,基于平行估计模型构造表征不确定逼近效果的预测误差,结合跟踪误差给出复合学习控制策略。针对弹性子系统设计自适应滑模控制稳定弹性模态。通过李雅普诺夫稳定性分析可证系统状态一致终值有界。仿真表明所提出的控制方法能够实现刚弹模态的稳定收敛,且具有更高的跟踪精度、更好的学习性能和更快的收敛速度。 相似文献
139.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(7):1714-1722
The space debris environment is one of the major threats against payloads. Space debris orbital distribution is of great importance for space debris environment modeling. Due to perturbation factors, the Right Ascension of Ascending Node (RAAN) of space objects changes consistently, causing regular rotation of the orbit plane around Earth’s axis. Based on the investigation of the RAAN perturbation rate of concerned objects, this paper proposes a RAAN discretization method in order to present the space debris longitude-dependent distribution. Combined with two line element (TLE) data provided by the US Space Surveillance Network, the estimated value from RAAN discretization method is compared with the real case. The results suggest that using only the initial orbital data at the beginning of the time interval of interest, the RAAN discretization method is able to provide reliable longitude distribution of concerned targets in the next following period. Furthermore, spacecraft cumulative flux against space debris is calculated in this paper. The results suggest that the relevance between spacecraft RAAN setup and flux output is much smaller for LEO targets than MEO targets, which corresponds with the theory analysis. Since the nonspherical perturbation is the major factor for RAAN variation, the RAAN perturbation rate has little connection with the size of orbital objects. In other words, the RAAN discretization method introduced in this paper also applies to space debris of different size range, proposing a possible suggestion for the improvement of space debris environment engineering models. 相似文献
140.
Navigation and positioning is an important and challenging problem in many control engineering applications. It provides feedback information to design controllers for systems. In this paper, a bibliographical review on factor graph based navigation and positioning is presented. More specifically, the sensor modeling, the factor graph optimization methods, and the topology factor based cooperative localization are reviewed. The navigation and positioning methods via factor graph are considered a... 相似文献