基于特征的锻件分类及特征有限元法

综合分析锻件后引入特征技术并归纳锻件的形状及变形特点 ,提出了锻件特征概念并给出锻件形状特征的一般定义和构成 ;采用面向对象技术表示特征 ,提出了锻件特征类的概念模式和具体的参数化数据模型 ;针对有限元分析中复杂多变的约束条件和载荷状况两个关键性因素的表达 ,提出特征类的关联思想。在基于特征的锻件分类基础上 ,把锻件变形归纳为“挤”或“压”两种特征元 ,提出了采用基于特征的有限元法 ,并综合自适应FEM、并行FEM、智能型FEM共同求解大型复杂锻件的变形模拟问题。     

银行印鉴的模糊识别方法

印鉴的计算机自动识别在金融电子化进程中是一个关键问题,也是一项十分难以解决的课题,目前国内外已提出了一些算法,但仍然在存在若干未能解决的问题,本文结合遗传算法,图像分析,模糊识别等方法,提出了一套完整的印鉴识别方法,能适应不同形状,大小的印鉴,配准精度高,特征提取较为全面,有效,分类准确,且能较好的消除背景干扰,基本达到实用要求。     

Design and Experimental Analysis of Aircrew Design Parameters to Vertical Takeoff and Landing

The calculation of the design parameters of lifting airscrew systems with fixed and tilted rotor, including the investigation of the operation schemes of actuators for the propeller control system, is carried out.     

Using the radial basis function neural network to predict ionospheric critical frequency of F2 layer over Wuhan

Neural networks (NNs) have been applied to ionospheric predictions recently. This paper uses radial basis function neural network (RBF-NN) to forecast hourly values of the ionospheric F₂ layer critical frequency(f_oF₂), over Wuhan (30.5N, 114.3E), China. The false nearest neighbor method is used to determine the embedding dimension, and the principal component analysis (PCA) is used to reduce noise and dimension. The whole study is based on a sample of about 26,000 observations of f_oF₂ with 1-h time resolution, derived during the period from January 1981 to December 1983. The performance of RBF-NN is estimated by calculating the normalized root-mean-squared (NRMSE) error, and its results show that short-term predictions of f_oF₂ are improved.     

An approach to forming the design performance of the attitude control system for small spacecraft

The elements for various types of attitude control systems used in a number of small spacecraft are considered. An approach for assessment of such system effectiveness based on design requirements for spacecraft purpose and restriction in accuracy, mass and energy is proposed.     

基于ADAMS/Aircraft的起落架滑跑模型仿真

以小车式起落架为例,利用ADAMS/Airc- raft建立了起落架滑跑试验仿真模型.给出了起落架滑跑运动方程,并进行了滑跑试验仿真分析。仿真结果与理论要求对比具有较好的一致性。