一种窄带平稳随机过程功率谱的简化拟合方法

基于平稳随机过程的基本原理,建立了拟合窄带平稳随机过程的功率谱所需的成形滤波器的简化模型,推导了窄带平稳随机功率谱的峰值、峰值频率、带宽与成形滤波器相应参数之间的关系,给出了拟合窄带平稳随机过程功率谱的简化方法。应用此方法对美国海军 CVA59航空母舰海上运动的垂荡、纵摇和横荡运动分量的 3个具体的功率谱实例进行了拟合,通过对将实测值与拟合结果进行比较,表明 :这种方法能够很好地拟合典型的对称窄带平稳随机过程,对于对称性不好和带宽较大的的功率谱,拟合的误差相对大一些。     

飞机大振幅滚转运动动态气动特性实验研究

在南航NH-2低速风洞中,对BJ-1飞机模型动态气动特性进行了实验研究.模型在不同攻角、不同振幅和不同频率时绕体轴作大振幅滚转运动,测量了模型的动态气动特性,着重分析了模型不同运动参数对模型滚转力矩和偏航力矩的影响.结果表明,模型攻角从小到大变化过程中,模型的滚转阻尼和偏航阻尼变化很大,滚转力矩和偏航力矩迟滞环变化方向发生改变.模型滚转频率对模型的滚转阻尼和偏航阻尼影响不明显,只改变力矩迟滞环的大小.随着模型振幅增加,滚转力矩和偏航力矩迟滞环从一个变成3个,出现2个交叉点,大滚转角时滚转阻尼和偏航阻尼特性与小滚转角时的相反.     

Co-rotating particle enhancements out of the ecliptic plane

The characteristics of the recurrent electron (38–53 keV) and ion (>0.5 MeV) enhancements observed by Ulysses from mid-1992 to April 1994 are presented. The magnitude of the ion flux increases reached a maximum at a latitude of 20°S and decreased afterwards by 23%/degree until early 1994. The magnitude of the electron increases showed a similar trend until May, 1993, after which time it became approximately constant, until it started to increase again in early 1994. The electron enhancements have lagged the protons by up to 5 days once Ulysses left the heliospheric current sheet (mid-1993). The electron spectral index tended to harden (a) during the decay of the event and (b) as the latitude increased, up to 50°S. The events have recurred on a 26.0 day period, but with significant phase shifts over the 25 rotations studied. The H/He ratio decreases across the maximum intensity. The mean minimum value for H/He was 3.5±0.3, lower than that measured in previous studies in the ecliptic plane.     

非定常气动力作用下弹性飞行器的稳定性及耦合特性

本文对所建立的弹性飞行器非定常动力学模型,以系统矩阵和返回差矩阵讨论了这类多变量模型的稳定性,由此导出定量评价弹性飞行器系统运动变量,即姿态、弹性自由度、控制及观测变量相互间的开环与闭环耦合测度,从频域的角度描述了耦合特性,具有较状态空间分析更直观、简捷的优点。文中还以算例给予了分析和验证。     

平面叶栅内固体粒子运动特性的实验研究

 利用ＮａｃＥ－１０型高速摄影机拍摄了流经平面叶栅的气固两相流中固体粒子的运动过程；在ＭｏｖｉｅｓＭｏｄｅｌ１００型胶片运动分析仪上对固体粒子的运动轨迹和速度进行了分析；并讨论了粒子的尺寸、初始速度的大小和方向对粒子在叶栅内运动特性的影响。     

基于单数码相机自由拍摄的空间点定位

 提出并实现了一种空间点定位方法。该方法仅用一台数码相机围绕目标进行多角度自由拍摄获得多帧图像,采用一套具有身份唯一性的标记点实现多图像间点的稳定匹配;在此基础上根据多视图几何约束,精确计算各次拍摄时的相机姿态和位置;进而求解目标点的三维位置信息,并对结果进行优化。实验表明空间点定位的相对误差优于0.03%。该方法所用设备十分简单,操作方式非常灵活,适用于大型物体多视角测量的拼合、某些情况下的装配检查等,也可直接用于较规则构型物体的三维数据获取与CAD模型重建。     

Research on Auto-detection for Remainder Particles of Aerospace Relay Based on Wavelet Analysis

Aerospace relay is one kind of electronic components which is used widely in national defense system and aerospace system. The existence of remainder particles induces the reliability declining, which has become a severe problem in the development of aerospace relay. Traditional particle impact noise detection (PIND) method for remainder detection is ineffective for small particles, due to its low precision and involvement of subjective factors. An auto-detection method for PIND output signals is proposed in this paper, which is based on direct wavelet de-noising (DWD), cross-correlation analysis (CCA) and homo-filtering (HF), the method enhances the affectiv-ity of PIND test about the small particles. In the end, some practical PIND output signals are analysed, and the validity of this new method is proved.     

Preparation of Highly Dispersed Antimony-doped Tin Oxide Nano-powder via Ion-exchange Hydrolysis of SnCl4 and SbCl3 and Azeotropic Drying

Antimony-doped tin hydroxide colloid precipitates have been synthesized by hydrolysis of SnCl4 and SbCl3 using: (1) an ion-exchange hydrolysis to remove chlorine ions, and (2) isoamyl acetate as an azeotropic solvent to obviate water. The obtained dried powder is of high dispersivity without any need for further grinding. The size and dispersivity of the final particles are investigated with the aid of TG-DTA, BET, XRD and TEM. After having calcined, the antimony-doped tin oxide nanopowder possesses a tetragonal rutile structure with high dispersivity, uniform particles and low hard agglomeration.     

Gain Scheduling Control of Nonlinear Shock Motion Based on Equilibrium Manifold Linearization Model

The equilibrium manifold linearization model of nonlinear shock motion is of higher accuracy and lower complexity over other models such as the small perturbation model and the piecewise-linear model. This paper analyzes the physical significance of the equi- librium manifold linearization model, and the self-feedback mechanism of shock motion is revealed. This helps to describe the stability and dynamics of shock motion. Based on the model, the paper puts forwards a gain scheduling control method for nonlinear shock mo- tion. Simulation has shown the validity of the control scheme.     

基于变分迭代的航天器相对姿轨耦合动力学解算方法

针对航天器相对姿轨耦合一体化运动,在定义坐标系下利用对偶四元数和旋量表示航天器的一般运动,推导出航天器六自由度运动学和动力学模型,并分别采用Runge-Kutta四阶算法和变分迭代法的配点形式求解该非线性模型。变分迭代法的配点形式是变分迭代法与配点法的复合,先给出变分迭代法的迭代方程,再把迭代方程应用到局部时间区间上探讨了局部变分迭代法,然后把变分迭代法与配点法结合得到数值迭代方程。利用对偶四元数所建立的模型相对于其他模型较为简洁,便于分析姿轨耦合特性。仿真结果表明,相比Runge-Kutta四阶算法,变分迭代法的解算精度更高。