整体壁板数字化展开建模方法

针对整体壁板零件数字化制造过程中对展开模型的需求,提出了一种整体壁板展开建模流程,针对曲面半径在2500mm以上的小曲率整体壁板零件,运用基于单元等变形的复杂曲面展开方法和基于单元变形能的复杂曲面展开方法对曲面展开,并以型号整体壁板零件为例,分别验证了运用两种曲面展开方法展开外形面及所创建板坯模型的效率和准确性.结果表明,基于单元等变形的复杂曲面展开方法适用于曲面半径在2500mm以上的小曲率整体壁板展开计算,展开的外形面及以此为基础建立的板坯模型形状尺寸准确,效率明显提高.     

Regional VTEC modeling with multivariate adaptive regression splines

Different algorithms have been proposed for the modeling of the ionosphere. The most frequently used method is based on the spherical harmonic functions achieving successful results for global modeling but not for the local and regional applications due to the bounded spherical harmonic representation. Irregular data distribution and data gaps cause also difficulties in the global modeling of the ionosphere. In this paper we propose an efficient algorithm with Multivariate Adaptive Regression Splines (MARS) to represent a new non-parametric approach for regional spatio-temporal mapping of the ionospheric electron density using ground-based GPS observations. MARS can handle very large data sets of observations and is an adaptive and flexible method, which can be applied to both linear and non-linear problems. The basis functions are directly obtained from the observations and have space partitioning property resulting in an adaptive model. This property helps to avoid numerical problems and computational inefficiency caused by the number of coefficients, which has to be increased to detect the local variations of the ionosphere. Since the fitting procedure is additive it does not require gridding and is able to process large amounts of data with large gaps. Additionally the model complexity can be controlled by the user via limiting the maximal number of coefficients and the order of products of the basis functions. In this study the MARS algorithm is applied to real data sets over Europe for regional ionosphere modeling. The results are compared with the results of Bernese GPS Software over the same region.     

On the use of NeQuick topside option in IRI-2007

The latest version of IRI includes various options for the computation of the topside electron density profile. One of the possible choices is based on NeQuick model. Its inclusion in IRI has been made transferring all the formulations used in NeQuick model. In details, an Epstein layer function is used to describe the electron density profile and the topside shape is controlled by an empirical parameter, connected to the NeQuick F2 bottomside thickness parameter, B2bot. It is computed also in this IRI topside option in order to maintain self-consistency with its original formulation. This paper analyses the possibility of using the IRI bottomside parameters for this option and its impact on the profile and TEC. The case of experimental peak values given as input is also analysed.     

基于定性模型的故障诊断方法

基于定性模型的故障诊断方法，利用定性模型描述系统结构和定性地预测系统行为，并通过与实际行为进行比较，可推理得到系统的故障诊断结果。详细介绍了基于定性模型故障诊断方法的诊断机理、建模方式及优缺点。此外，还概述了该方法的研究与应用现状及发展趋势。     

改进的相位建模法在瞬时频率估计中的应用

瞬时频率估计是非平稳信号分析的重要内容.相位建模法估计瞬时频率的精度高、抗噪性能好,但是计算复杂,在工程上难以实时实现,限制了其进一步发展.先介绍了瞬时频率的定义和相位建模法,然后针对传统相位建模法存在的计算复杂的问题提出了改进的相位建模法,并进行了仿真分析.结果证明,在保证精度的前提下,该改进算法有效地简化了计算.     

Exploring the global shock scenario at multiple points between sun and earth: The solar transients launched on January 1 and September 23, 1978

We revisit the transient interplanetary events of January 1 and September 23, 1978. Using in-situ and remote sensing observations at locations widely separated in longitudes and distances from the Sun, we infer that in both cases the overall shock surface had a very fast “nose” region with speeds >900 and >1500 km⁻¹ in the January and September events, respectively, and much slower flank speeds (∼600 km⁻¹ or less), suggesting a shock surface with a strong speed gradient with heliospheric longitude. The shock-nose regions are thus likely efficient acceleration sites of MeV ions, even at 1 AU from the Sun. Our 3D magnetohydrodynamics modeling suggests that a 24° × 24° localized disturbance at 18 solar radii injecting momentum 100 times the background solar wind input over 1 h can produce a disturbance in semi-quantitative agreement with the observed shock arrival time, plasma density and velocity time series in the January 1978 event.     

Unsteady aerodynamic modeling at high angles of attack using support vector machines

Accurate aerodynamic models are the basis of flight simulation and control law design.Mathematically modeling unsteady aerodynamics at high angles of attack bears great difficulties in model structure determination and parameter estimation due to little understanding of the flow mechanism.Support vector machines(SVMs)based on statistical learning theory provide a novel tool for nonlinear system modeling.The work presented here examines the feasibility of applying SVMs to high angle-of-attack unsteady aerodynamic modeling field.Mainly,after a review of SVMs,several issues associated with unsteady aerodynamic modeling by use of SVMs are discussed in detail,such as selection of input variables,selection of output variables and determination of SVM parameters.The least squares SVM(LS-SVM)models are set up from certain dynamic wind tunnel test data of a delta wing and an aircraft configuration,and then used to predict the aerodynamic responses in other tests.The predictions are in good agreement with the test data,which indicates the satisfying learning and generalization performance of LS-SVMs.     

基于模态综合法的含间隙折叠舵面动态特性分析

基于模态综合法对含间隙折叠舵面的非线性动态特性进行了研究。首先根据折叠舵面的结构特性建立含铰链连接的有限元模型，并采用双协调自由界面模态综合法对折叠舵面的有限元模型进行降阶。其次对不含间隙的折叠舵面进行扫频和模态实验，检验有限元模型及其降阶动力学模型的精度，并基于模型修正得到铰链的等效线性连接刚度。最后将等效线性连接刚度和间隙值进行组合，得到不同间隙下铰链的非线性连接刚度，完成含间隙折叠舵面的非线性动力学模型建立。基于非线性动力学模型对含间隙折叠舵面进行数值扫频，计算结果与实验扫频结果吻合良好，验证了所建立非线性动力学模型的精度及其在含间隙折叠舵面非线性动态特性分析中的可行性。     

Control techniques of tilt rotor unmanned aerial vehicle systems:A review

The tilt rotor unmanned aerial vehicle (TRUAV) exhibits special application value due to its unique rotor structure. However, varying dynamics and aerodynamic interference caused by tiltable rotors are great technical challenges and key issues for TRUAV's high-powered flight con-trols, which have attracted the attention of many researchers. This paper outlines the concept of TRUAV and some typical TRUAV platforms while focusing on control techniques. TRUAV struc-tural features, dynamics modeling, and flight control methods are discussed, and major challenges and corresponding developmental tendencies associated with TRUAV flight control are summa-rized.     

发动机凸轮靠模制造实践与分析

通过叙述标准轴（原始靠模）的选择，修正标准轴的刮削，靠模的反靠，工件凸轮的磨削，以及标准轴和工件凸轮轴的检测，“补偿反靠”的工艺过程等，阐明了发动机凸轮靠模的制造方法与过程