1553B总线监视器系统软件设计

1553B总线是一种集中式控制的串行总线型网络，其组成包括一个总线控制器、若干远置终端，还可以包括总线监视器。本文详细介绍了1553B总线监视器系统软件的设计，探讨了设计中需要注意的几个问题。     

A New Probabilistic Transformation in Generalized Power Space

The mapping from the belief to the probability domain is a controversial issue, whose original purpose is to make (hard) decision, but for contrariwise to erroneous widespread idea/claim, this is not the only interest for using such mappings nowadays. Actually the probabilistic transformations of belief mass assignments are very useful in modern multitarget multisensor tracking systems where one deals with soft decisions, especially when precise belief structures are not always available due to the existence of uncertainty in human being's subjective judgments. Therefore, a new probabilistic transformation of interval-valued belief structure is put forward in the generalized power space, in order to build a subjective probability measure from any basic belief assignment defined on any model of the frame of discernment. Several examples are given to show how the new transformation works and we compare it to the main existing transformations proposed in the literature so far. Results are provided to illustrate the rationality and efficiency of this new proposed method making the decision problem simpler.     

Static Analysis of Functionally Graded Sandwich Plates Using an Efficient and Simple Refined Theory

In this paper, a new displacement based high-order shear deformation theory is introduced for the static response of function-ally graded sandwich plate. Unlike any other theory, the number of unknown functions involved is only four, as against five in case of other shear deformation theories. The theory presented is variationally consistent, has strong similarity with classical plate theory in many aspects, does not require shear correction factor, and gives rise to transverse shear stress variation such that the transverse shear stresses vary parabolically across the thickness satisfying shear stress free surface conditions. Two common types of functionally graded sandwich plates, namely, the sandwich with functionally graded facesheet and homogeneous core and the sandwich with homogeneous facesheet and functionally graded core, are considered. Governing equations are derived from the principle of virtual displacements. The closed-form solution of a simply supported rectangular plate subjected to sinu-soidal loading has been obtained by using the Navier method. The validity of the present theory is investigated by comparing some of the present results with those of the classical, the first-order and the other higher-order theories. It can be concluded that the proposed theory is accurate and simple in solving the static bending behavior of functionally graded sandwich plates.     

Regularized Robust Filter for Spacecraft Attitude Determination

A modified regularized robust filter is proposed for spacecraft attitude determination in the presence of relative misalignment of attitude sensors. The filter is designed to minimize the worst-possible residual norm on condition that there is parametric uncertainty in the measurement model. The weighting matrix of the residual norm is designed to minimize the upper bound of the estimation error variance. The performance of the proposed attitude determination robust filter is illustrated with the use of real test data from a real three-floated gyroscope. Simulation results demonstrate that the attitude estimation accuracy is improved by using the proposed algorithm.     

多渐消因子Kalman滤波器在SINS初始对准中的应用(英文)

针对系统模型和统计信息不能精确已知的条件下Kalman滤波无法给出最优解这一问题,单一渐消因子Kalman滤波算法对于简单的系统是有效的,但是对于复杂的多变量系统,仅仅利用单个的渐消因子是不够的。本文提出了一种多渐消因子滤波算法,通过利用开窗法计算新息序列协方差的无偏估计获得渐消因子矩阵。利用渐消因子矩阵调节一步预测均方误差矩阵k|k1P,对不同的滤波通道提供不同的渐消速率。将该方法应用于SINS的初始对准中,仿真和试验结果表明:当真实系统噪声统计特性同设定参数不一致时,对准精度明显高于其他滤波算法。其对不确定性噪声具有较低的敏感度,对系统参数具有较好的滤波效果。因而,在实际应用中具有重要的参考价值。     

多电飞机作动系统的体系结构优化(英文)

多电技术的深入发展使得飞机上可选择的功率源和作动器种类越来越多,这导致在机载作动系统体系结构优化设计过程中出现了不同功率源和作动器组合的极端复杂性,传统的"试凑"法已无法完成设计任务。首先介绍了多电飞机飞控作动系统(Flight Control Actuation System,FCAS)的组成,计算了其可能的体系结构数量;其次提出了FCAS体系结构在安全性、重量和效率方面的评价指标,计算了全机各舵面均采用同类作动器时的评价指标值;最后对比分析了现有的各种多目标优化算法,采用遗传算法给出了多电飞机FCAS体系结构的多目标优化设计结果。对比传统的只采用阀控液压伺服作动器的作动系统体系结构,优化后的体系结构可以在满足安全可靠性要求的前提下使系统的重量减轻6%左右,效率提高30%左右。     

C/C复合材料等温CVI工艺T-S模糊系统研究

等温CVI是目前制备高性能碳／碳(C／C)复合材料的重要技术,其主要不足之处是周期长,成本高,建立CVI工艺参数与沉积速率或均匀性之间的关系模型,进而来指导工艺的设计与优化,是达到降低C／C复合材料开发成本的重要途径。本文提出基于模糊推理系统理论,建立等温CVI工艺基于实验的T—S模糊系统模型,来挖掘和表达实验中所积累的无法用公式来描述的经验,根据该模型得到了一类盘状制件CVI工艺主要沉积条件的作用机理,为工艺优化、设计和控制提供了理论上的指导。     

隐身飞机综述

介绍了隐身飞机的发展状况和特点,对美国现役的F-117、B-2和即将服役的F-22以及俄罗斯的米格1.44、苏-35进行了详述,分析了21世纪隐身飞机的发展趋势。     

某航空用扭转弹簧失效分析(英文)

某型扭转弹簧零件主要用于航空机构中,在装配过程中出现裂纹和发生断裂。通过视频显微镜、扫描电镜、金相显微镜等分析方法,对断裂弹簧裂纹、断口特征及其附近损伤形貌进行了宏、微观观察和覆盖物的能谱分析。在试验结果和数据的基础上,结合加工工艺综合分析失效的性质和原因。金相组织检查未发现材质异常,失效与材质无关。弹簧裂纹和断裂都起始于内表面,因此裂纹的萌生发生在弹簧绕制后镀镉前。裂纹张开方向与弹簧内表面的残余拉应力方向一致,而且绕制后、镀镉前接触氢介质。弹簧失效的原因是残余拉应力和氢共同作用下发生氢致延迟开裂。     

虚拟制造模式探讨

虚拟制造是对真实的制造系统的产品及过程的信息提取加工和逻辑功能抽象,是实现敏捷性的一种有效的手段。它包括两个方面的内容：产品生命全程仿真和企业行为仿真,阐述了虚拟制造的概念,对虚拟制造环境下的产品设计模式、生产模式和企业运行模式进行了探讨,并给出虚拟制造相关技术。