断裂韧性K1C和断裂门槛值 Δ Kth可靠性测定方法

采用定量方程随机化方法,建立了断裂p-J_R-Δa曲线方程,断裂p-J_R-Δa曲线与钝化线的交点即为试验测定具有可靠度p的J积分临界值(J_1C)_p值,根据断裂力学测试原理,由试验测定(J_1C)_p值可转化出断裂韧性(K_1C)_p值;还建立了断裂门槛ΔK_th值的可靠性测定方法,并对试验数据进行了统计分析处理,得到了一些具有重要应用价值的结果和数据.研究发现:断裂门槛值ΔK_th服从正态分布.     

基于熵权法改进的航班延误影响因素评估研究

随着航空运输业的不断发展,航班延误问题越来越受到重视,已成为社会的热点问题.通过实际运行的相关统计数据,研究影响航班延误的各项因素,提取主要因子,构建航班延误综合评价指标体系.用熵权法对航班延误的各项影响因子进行客观评价,建立了基于熵权法改进航班延误影响因素的综合评估模型,并利用1 000架次航班实例对模型的有效性进行了验证,研究结果表明评估模型客观、准确、有效.     

自动倒码式力标准机技术及其应用

静重式力标准机是最重要的力值计量、传递仪器之一。采用倒换砝码的加载方法,只需少量的砝码,可以实现大范围测量应用,并减小设备体积。理论上,一台较大规格的自动倒码式力标准机可以替代其容量以下所有规格的设备。分析了加载过程中砝码倒换的力学原理,论述了所研制的自动倒码式力标准机的工作原理及其自动监控问题,并进行了应用实验。结果表明,关于砝码倒换的力学原理的理论分析和力标准机的监控方法是正确和有效的。自动倒码式力标准机非常适合于包括宇航推力计量器具在内的各种测力仪的标定和校准。     

伺服阀滑阀副叠合量测试技术中的数据处理方法

介绍了伺服阀滑阀副叠合量的测试原理。将数理统计中的相关系数、一元线性回归、F检验等方法应用到了叠合量测试中的数据处理上。给出了伺服阀滑阀副小开口弯曲度的概念,为分析伺服阀滑阀副的小开口特性提供了依据。     

A variational Bayesian-based robust adaptive filtering for precise point positioning using undifferenced and uncombined observations

In the application of precise point positioning (PPP), especially in the dynamic mode, the classical Kalman filter (KF) usually produces a large number of estimation errors or diverges when there are gross errors in the observation data or unexpected turbulences occur in target motion state or both of them. For such problem, a variational Bayesian (VB)-based robust adaptive Kalman filtering (VB-RAKF) is proposed in this paper. This filter introduces a classification robust equivalent weight function to resist observation gross error and the inverse Wishart prior to model inaccurate process noise covariance matrix (PNCM). To improve the instantaneous accuracy of state estimation, the VB approach is used to obtain better estimations of inaccurate PNCM. Several sets of observation data collected by IGS reference stations and vehicles are employed to check the robustness and positioning accuracy of the VB-RAKF model. The results show that the VB-RAKF algorithm is more robust than the KF, and can effectively resist the gross error in observation data and control state disturbance. In the IGS reference station tests, when compared to the KF, the static positioning accuracies of the VB-RAKF in the north, east and up directions are improved by 13%, 8% and 22%, respectively, and the simulated dynamic positioning accuracies of the VB-RAKF in the north, east and up directions are improved by 19%, 9% and 21%, respectively. The in-vehicle dynamic test verifies that the VB-RAKF outperforms the KF, and shows that the VB-RAKF has better performance than the KF when dealing with observation data which has obvious gross errors, and similar performance as the KF when gross errors are small.     

Influence of non-equilibrium reactions on the optimization of aerothrust aeroassisted maneuver with orbital change

The spaceplane is perspective vehicle due to wide maneuverability in comparison with a space capsule. Its maneuverability is expressed by the larger flight range and also by a possibility to rotate orbital inclination in the atmosphere by the aerodynamic and thrust forces. Orbital plane atmospheric rotation maneuvers can significantly reduce fuel costs compared to rocket-dynamic non-coplanar maneuver. However, this maneuver occurs at Mach numbers about 25, and such velocities lead to non-equilibrium chemical reactions in the shock wave. Such reactions change a physicochemical air property, and it affects aerodynamic coefficients. This paper investigates the influence of non-equilibrium reactions on the aerothrust aeroassisted maneuver with orbital change. The approach is to solve an optimization problem using the differential evolution algorithm with a temperature limitation. The spaceplane aerodynamic coefficients are determined by the numerical solution of the Reynolds-averaged Navier-Stokes equations. The aerodynamic calculations are conducted for the cases of perfect and non-equilibrium gases. A comparison of optimal trajectories, control laws, and fuel costs is made between models of perfect and non-equilibrium gases. The effect of a chemically reacting gas on the finite parameters is also evaluated using control laws obtained for a perfect gas.     

非线性热传导方程混合问题插值逼近

以Legendre-Gauss-type积分节点为插值节点,构造插值基函数展开数值解,逼近有界杆上的非线性热传导方程Dirichlet边界条件的正确解。给出算法格式和相应的数值算例,表明所提算法格式的有效性和高精度。所给算法适合于非线性问题求解。     

基于颜色、形状和纹理的多特征融合图像检索

基于单一特征的图像检索的许多方法都已经相当成熟,如何有效利用这些特征是基于内容图像检索的一个关键问题。利用颜色、纹理、形状等特征,在多特征融合检索时用动态生成权值的方法进行图像检索。实验结果表明,算法能够准确、高效地检索出目标图像,相对于单一特征的检索,有效提高了图像的检索精度。     

武器装备采办模糊多属性群体决策方法

针对武器装备采办的模糊多属性群体决策问题,文章假设定性属性指标都是梯形模糊数状态,运用模糊数学理论和广义海明权距离,提出了一种定性判断和定量分析相结合的武器装备采办模糊多属性群体决策方法,并给出了一个方法应用及求解计算的实际例子,算例结果证明了方法有效。     

飞机构型管理与重量控制技术研究

介绍了飞机构型管理、重量控制的基本内容及实施过程,分析了构型管理与重量控制的相互关系,结合具体工作,对构型与重量的管理与控制综合技术进行了初步研究。