信息管理系统设计中几个问题之管见

本文结合实际研制信息管理系统的经验,着重讨论了系统设计(或称总体设计)阶段中几个需注意的关键性问题。尽管问题讨论是以dBASEⅢ为背景,但对dBASEⅣ及FOXBASE均有一定的实际意义。     

某型船机舱通风系统设计

根据某型船机舱设备及其布置特点,按照机舱通风系统设计要求,计算确定了前、后机舱通风量．根据机舱通风量和抽风式通风组织方案,选择了合适的通风设备．在设计中分析比较了若干通风系统设计方案,最后确定采用抽风式机舱通风系统．该船航行试验证明,机舱通风系统设计十分成功．     

车辆驾驶仿真中地形匹配的数学模型

建立了地形匹配的一种新的数学模型,开发了相应的C语言程序,并进行了定性检验。该模型已在实际中得到应用,效果良好。     

多传感器信息融合技术述评

近十几年来,多传感器信息融合技术获得了普遍的关注和广泛的应用,其理论与方法已成为智能信息处理的一个重要研究领域。本文概述了信息融合的基本原理,从系统的信息层次和功能划分两个方面阐述了信息融合的基本结构,并对信息融合的具体方法及应用进行了层次化概括,较完整地展示了这一研究领域的全貌。最后进一步分析了信息融合研究领域所存在的一些主要问题,以此指明这一研究领域的发展侧重点。     

具有指定误差协方差的相关域预测方法

利用协方差控制的理论和方法,研究了Ｃ３Ｉ系统中航迹数据融合的未来点相关域预测问题,提出了根据格定预测误差协方差来确定目标航迹未来点所处的相关域位置及大小的新方法。该方法具有实时性好、计算量小的特点。仿真结果表明了该方法的可行性。     

惯性定向定位/导航技术及发展概况

阐述了惯性导航、陀螺罗经定向工作原理和捷联惯性导航的计算问题,以及GPS的有关情况。最后,预测捷联惯性系统和GPS 组合将成为航空、航海和陆地车辆导航定位的主要装置。     

圆锥壳方程的二次渐近解

本文由旋转壳的一对二阶常微分方程得出圆锥壳的复变量方程,利用渐近积分法推导出方程的一次近似解和二次近似解。二次近似解达到薄壳理论所具有的精度,一次近似解也具有足够精度。对于所取算例,本文解的计算结果与已有的Kelvin函数解的结果符合良好。但本文解为有限形式的简单表达式,便于计算应用。     

建立不工作失效率理论预测模型的具体方法

本文介绍了建立不工作失效率理论预测模型的具体方法和途径,提出检验数据是否可用的五条标准,并讨论了模型建立过程中应注意的几个特殊因素。     

Experimental investigation on enhanced damage to fuel tanks by reactive projectiles impact

Enhanced damage to the full-filled fuel tank,impacted by the cold pressed and sintered PTFE/AL/W reactive material projectile(RMP)with a density of 7.8 g/cm3,is investigated experimentally and theoretically.The fuel tank is a rectangular structure,welded by six pieces of 2024 aluminum plate with a thickness of 6 mm,and filled with RP-3 aviation kerosene.Experimental results show that the kerosene is ignited by the RMP impact at a velocity above 1062 m/s,and a novel interior ignition phenomenon which is closely related to the rupture effect of the fuel tank is observed.However,the traditional steel projectile with the same mass and dimension requires a velocity up to 1649 m/s to ignite the kerosene.Based on the experimental results,the radial pressure field is considered to be the main reason for the shear failure of weld.For mechanism considerations,the chemical energy released by the RMP enhances the hydrodynamic ram(HRAM)effect and provides additional ignition sources inside the fuel tank,thereby enhancing both rupture and ignition effects.Moreover,to further understand the enhanced ignition effect of RMP,the reactive debris temperature inside the kerosene is analyzed theoretically.The initiated reactive debris with high temperature provides effective interior ignition sources to ignite the kerosene,resulting in the enhanced ignition of the kerosene.     

Robust cubature Kalman filter method for the nonlinear alignment of SINS

Nonlinear initial alignment is a significant research topic for strapdown inertial navigation system(SINS).Cubature Kalman filter(CKF)is a popular tool for nonlinear initial alignment.Standard CKF assumes that the statics of the observation noise are pre-given before the filtering process.Therefore,any unpredicted outliers in observation noise will decrease the stability of the filter.In view of this problem,improved CKF method with robustness is proposed.Multiple fading factors are introduced to rescale the obser-vation noise covariance.Then the update stage of the filter can be autonomously tuned,and if there are outliers exist in the observations,the update should be less weighted.Under the Gaussian assumption of KF,the Mahalanobis distance of the innovation vector is supposed to be Chi-square distributed.Therefore a judging index based on Chi-square test is designed to detect the noise outliers,determining whether the fading tune are required.The proposed method is applied in the nonlinear alignment of SINS,and vehicle experiment proves the effective of the proposed method.