AFDX网络协议研究

介绍了AFDX网络的产生背景及发展历程;解析了ARINC664规范各个部分的功能及与开放式系统参考模型的关系;总结了AFDX网络相对于商用以太网的特点和AFDX网络与机载系统的关系,通过对AFDX在A380等飞机上的应用研究,归纳了基于AFDX网络的航空电子系统的特点;AFDX网络已成功应用于工程实践,该网络具有完整的协议结构,具有高实时性、高确定性和高可靠性的特点,是一种新型的机载网络总线。     

飞机振动特性激光测量与分析

飞机振动特性测量与分析,对于飞机识别和探测系统的设计与评估是至关重要的;在简要介绍了振动特性测量理论之后,针对外场环境条件,设计了飞机振动特性激光测量装置和测量方法,并经过实验室验证;在全尺寸飞机试验与测量过程中,获得了有效的原始测量数据,计算出飞机振动特征量:平均中心频率和二阶中心矩;同时指出了在飞机振动测量中应注意的问题;试验表明,飞机振动特性测量与分析方法正确、有效。     

聚甲基丙烯酰亚胺(PMI)泡沫的进展

聚甲基丙烯酰亚胺(Polymethacrylimide,PMI)泡沫是当今夹层结构复合材料最主要的芯材,具有密度低、力学性能和耐热性能突出、易于机加工、与热固性树脂黏结良好、适应于热压罐固化工艺等突出优点,已经在航空航天、交通运输、风电叶片、医疗器械、电子通讯等领域获得较广泛应用。本文对PMI泡沫的发展历史、制备技术、结构与性能进行了综述,并提出了国内PMI泡沫进一步发展亟待解决的问题。     

A combined DEM–FEM numerical method for Shot Peening parameter optimisation

A numerical modelling approach capable of simulating Shot Peening (SP) processes of industrial interest was developed by combining the Discrete Element Method (DEM) with the Finite Element Method (FEM).In this approach, shot–shot and shot–target interactions as well as the overall shot flow were simulated efficiently using rigid body dynamics. A new algorithm to dynamically adapt the coefficient of restitution (CoR) for repeated impacts of shots on the same spot was implemented in the DEM code to take into account the effect of material hardening. Then, a parametric study was conducted using the Finite Element Method (FEM) to investigate the influence of the SP parameters on the development of residual stresses.Finally, a two-step coupling method is presented to combine the output of DEM simulation with FEM analyses to retrieve the Compressive Residual Stresses (CRS) after multiple impacts with the aim to evaluate the minimum area required to be modelled to realistically capture the field of residual stresses. A series of such coupled analyses were performed to determine the effect of peening angle and the combination of initial velocity and mass flow rate on CRS.     

A marker-less assembly stage recognition method based on corner feature

Fast and robust product assembly stage recognition is a key step in human–machine cooperative assembly. To solve the recognition problem of similar adjacent assembly stages, a marker-less assembly stage recognition method is proposed based on corner feature between an assembling product and a digital model. Considering the geometric features of mechanical products, a corner identification method is proposed based on the circumferential angle difference (CADF). Then a corner matching method based on distance constraint is studied for ICP registration to realize the point cloud registration between the product and digital model. Based on the registration relationship, a similarity algorithm based on proximity point proportion is used to calculate the similarity between models and the input assembling product. The model with the greatest similarity is taken as the stage recognition result. In experiments on four group assembling products, the average stage recognition accuracy is 96.15%, which indicates that the proposed method can solve the stage recognition problem. The corner identification method based on the CADF outperforms the Harris-3D corner detection method in the efficiency of assembly stage recognition.     

Windows可信计算实现研究

描述Windows的可信计算实现架构—NGSCB;应用可信计算理论分析NGSCB的主要特性,剖析具有完整性度量、可信启动、TPM支撑架构的理论基础和主要实现方法;列举NGSCB现有可信计算产品存在的问题,指出NGSCB的发展前景和需要努力的方向。     

一种改进的组间互补码及其性能分析

在分析组间互补码、零相关区正交互补码的基础上,构造一种适合于多进制正交码扩频系统或准同步CDMA系统的正交码集――改进的组间互补码。通过理论分析与性能仿真表明,改进的组间互补码的集合数量多于组间互补码;零相关区长度大于组内组间互补码,但比组间的组间互补码小;在相同码长条件下,改进的组间互补码的自相关特性优于组间互补码,互相关特性与组间互补码相当。     

基于细菌进化及多属性决策的航迹规划方法研究

为了优化和完善航迹规划,将细菌进化算法和多属性决策理论相结合。对转弯角的编码考虑了飞行器过载限制;生成初始种群时初始角度分散选取,以保证种群多样性防止早熟;通过变异和基因转移,减少种群数目,加快进化速度;采用生存概率、路径长度、转弯角度综合评价航迹,应用多属性决策方法选择最优航迹。仿真结果表明,优化效率显著提高,规划的航迹有效地规避了威胁。     

目标机动导致导弹脱靶判别建模与仿真

针对目标机动能否逃脱导弹攻击的判断问题,根据比例导引法弹目相对运动方程组分析了目标机动逃脱导弹攻击的条件,推导了目标法向过载与导弹最大需用过载间的关系,建立了目标机动导致比例导引导弹脱靶判别的数学模型,运用该模型对算例进行了仿真与分析,仿真结果符合机动逃脱的运动学一般规律,说明该模型可以用于对抗仿真系统中飞机能否机动逃脱的判据。     

铝合金铸件成本报价速算法

以中等复杂一般要求的ZL101-T4典型铸件为案例,以铸件总成本中占主导地位的“单位铸件材料消耗定额”单项成本作为基准成本“A” (本案例A=18.16元/kg),以此求出其余各成本以及利润、应纳税费额等占基准成本A的比例系数,相加全部系数得到铸件报价系数F=2.0501.由于铸件复杂程度和工艺难度不同,其工艺成本亦不同,引入铸件调价系数K (K=0.90～1.30)以适应各类不同铸件的速算报价需要,其速算公式为:铸件总报价Q=2.0501AK(元/kg).