首都机场行李分拣统计分析系统的设计与实现

介绍了行李分拣统计分析系统的设计与实现过程,给出了实现该系统的软硬件环境。对一些主要的模块给出了详细的说明,给出了关键技术的解决方案。同时,还介绍了系统的主要功能,并对这项技术的实际应用效果做出总结。     

ACAS接收机S模式信号处理算法及其实现

ACAS接收机S模式信号处理主要包括前导码检测、位与位置信度的判决、错误检测以及纠错等主要算法,分别对这些算法进行了详细研究,并用FPGA实现了这些算法。仿真结果说明该实现能够对S模式接收信号成功地解调、纠错译码。     

工艺信息管理系统中工艺更改的实现

对工程实际中的工艺更改问题进行了分析 ,提出了工艺信息管理系统中工艺更改的两种实现方案 ,并对实现工艺更改的一些主要问题进行了讨论     

大规模测控站集中监控技术研究

详细介绍了测控站设备监控的发展历程和现状,对大规模测控站实施集中监控的意义、集中监控涉及的主要问题以及实现的主要技术途径进行了阐述,并对集中监控功能的进一步拓展给出了相应的建议。     

飞机配电系统中交流模拟固态功率控制器设计

主要介绍了一种交流模拟固态功率控制器（SSPC）的设计和实现。它主要使用了在嵌入式系统中广泛应用的单片机，来实现SSPC的基本功能。从核心器件到对负载电流通断控制以及对采入信号的调理都进行了详细的介绍与说明。     

机载红外搜索跟踪系统关键技术分析

概述了红外搜索跟踪系统的组成及主要技术特点,对红外成像系统中的红外望远光学系统、红外探测器组件等进行了分析;探讨了稳定与瞄准系统实现方案;对图像跟踪器中的跟踪算法及工程实现中采取的措施进行了论述。     

计算机飞行计划系统的设计与实现

介绍了计算机飞行计划系统的设计和实现过程,给出了实现该系统的软硬件环境,说明了其中的一些关键技术和解决方案,同时,还介绍了该系统的主要功能,并对进一步的工作和这项技术的应用前景作了展望。     

基于数字测相的DQPSK信号软件解调研究

提出了一种新的DQPSK信号差分解调的软件实现方法,通过瞬时测频实现位同步,利用正交测相实现解调。文中详细介绍了此种方法的基本原理和实现过程,分析了解调过程中引起测相误差的原因及对解调结果的影响,给出了主要部分的计算机仿真结果和实际应用效果。该方法简单,解调性能优越,便于软件编程,具有一定的应用价值。     

实现结构轻量化的新型平流层飞艇研究进展

平流层飞艇具有极高的实用价值,是国内外临近空间开发的研究热点。和中低空常规飞艇相比,由于单位体积所提供的浮力大大降低,使得平流层飞艇设计时存在艇体体积、阻力和重量之间的循环关系,飞艇结构轻量化成为平流层飞艇研发的首要课题,受到了各国研究机构的高度重视。本文对目前实现平流层飞艇结构轻量化的主要方法和技术进行了整理,给出了利用这些方法实现结构轻量化的平流层飞艇研究进展,比较了这些方法的优势和不足,并对新型的平流层展开飞艇技术进行了分析。分析结果认为改进蒙皮材料性能、改变飞艇的结构形式和利用新型的空中展开飞艇将是平流层飞艇实现结构轻量化的主要手段,新型空中展开飞艇能够有效地实现结构轻量化,具备较好的发展潜力。     

雷达中频信号数据录取与回放系统研制可行性分析

主要对雷达中频信号数据录取和回放分系统研制可行性进行了分析,把系统分为录取和回放两部分,对初步实现方案和工程可行性进行了论证。     

碳布叠层穿刺复合材料多尺度传热特性研究

为了深入认识复合材料的多尺度传热特性,预测复合材料宏观热物性参数,基于通用单胞思想和多尺度传热特性分析,建立了一种有效预测碳布叠层穿刺复合材料等效热物性参数的方法。基于电镜扫描分析了纤维束和编织结构的特征,采用通用单胞思想,建立了介/细观传热分析模型,通过数值仿真进行了一系列的多尺度传热特性分析,譬如:纤维体积分数对纤维束结构传热特性的影响、穿刺纤维束大小对编织结构传热特性的影响分析,在此基础上,建立了胞体模板扩展,初步将介/细观结构研究规律应用到宏观结构热物性预测,并进行多层胞体传热特性分析。验证实验表明:等效热物性预测值与实验值吻合较好,方法有效,为深入理解认识碳布叠层穿刺复合材料的介/细观传热特性提供了有效的分析手段。     

复合材料气囊成型工艺的质量缺陷研究

重点论述了气囊成型较大尺寸的复合材料制件时容易产生孔隙或气泡等工艺质量缺陷的原因,指出气囊的柔性不利于树脂的流动和气泡的排出.试验结果表明,尽可能地排出预浸料吸收的水分、低沸点溶剂及预浸料铺叠过程中夹裹的气体,进而减少固化时气泡的成核与长大,是解决气泡和孔隙等工艺质量缺陷的关键.     

机载总线控制管理计算机系统设计与研究

以某型飞机为模型,根据航空电子系统所要完成的多种飞行任务,机载总线控制管理计算机的功能和性能,进行了机载总线控制管理计算机的系统设计,并对该系统的可行性进行实验室的综合仿真试验研究,为机载计算机软硬件的模块化和层次化设计提供了设计依据。     

用保角转绘坐标解二维和轴对称可压流Euler方程

本文推导出用保角转绘正交曲线坐标表示的二维与轴对称Euler方程,方程中的未知量以曲线坐标方向的速度分量表示,并有不含未知量导数的源项。方程组的形式与直角坐标系中的接近,因而简化了计算。本文将该方程组用于计算二维任意翼型和旋成体轴对称绕流,采用分辨率较高的Eberle特征平均显式有限体积差分算法求解,在不同区域中用不同的显式推进步数加速收敛。本方法已分别对翼型和旋成体轴对称绕流编制了计算程序,可用于自由流为亚声速、跨声速和超声速的绕流计算。大量计算结果表明,本方法精度好,激波分辨率高,编程序简单。     

Flowgraph Techniques for Closed Systems

A two-port with both generator and load constitutes a closed system; it can be defined as a system with only interdependent variables or as a system containing no independent variables. The flowgraph describes the relationships between variables in a closed system as determined by the topology of its components. The corresponding closed flowgraph represents a zero-port network from which N-port networks can be generated as subsets by truncation of the closed system. A constraint governing any closed system expressing the properties of its cut-sets and tie-sets is referred to as the topology equation. The topology equation can be computed from the sum of loops in the closed flowgraph, and forms the key for the derivation of properties of closed systems and derived N-port subsets. Oscillators analyzed as zero-ports are discussed in detail to illustrate the rationale for the flowgraph approach to closed systems. To exploit the closed system model conceptually and computationally for N-ports, an approach is suggested and illustrated for N = 1 by an analysis of transfer functions and for N = 2 by a sensitivity analysis of stochastic networks.     

利用飞轮的航天器姿态跟踪与能量存储

研究航天器集成能量与姿态控制系统中飞轮的控制律。系统中飞轮是姿态控制的执行机构,同时也是储能装置。首先利用Lyapunov方法设计了航天器姿态跟踪的反馈控制律,然后研究一种力矩形式的飞轮控制律。利用奇异值分解方法把飞轮组的控制力矩向量分解为3部分相互正交的力矩向量,一部分用来提供姿态控制力矩,一部分用来以给定的功率储能,另一部分完成轮速平衡以避免由于各飞轮轮速差异过大引起的飞轮饱和。提出了一种基于动能反馈的储能功率规划方案来保证系统的能量平衡,可以避免由于过剩能量引起的飞轮饱和。数值仿真结果验证了控制方案的有效性。     

Thermal Evolution and Magnetic Field Generation in Terrestrial Planets and Satellites

Of the terrestrial planets, Earth and Mercury have self-sustained fields while Mars and Venus do not. Magnetic field data recorded at Ganymede have been interpreted as evidence of a self-generated magnetic field. The other icy Galilean satellites have magnetic fields induced in their subsurface oceans while Io and the Saturnian satellite Titan apparently are lacking magnetic fields of internal origin altogether. Parts of the lunar crust are remanently magnetized as are parts of the crust of Mars. While it is widely accepted that the magnetization of the Martian crust has been caused by an early magnetic field, for the Moon alternative explanations link the magnetization to plasma generated by large impacts. The necessary conditions for a dynamo in the terrestrial planets and satellites are the existence of an iron-rich core that is undergoing intense fluid motion. It is widely accepted that the fluid motion is caused by convection driven either by thermal buoyancy or by chemical buoyancy or by both. The chemical buoyancy is released upon the growth of an inner core. The latter requires a light alloying element in the core that is enriched in the outer core as the solid inner core grows. In most models, the light alloying element is assumed to be sulfur, but other elements such as, e.g., oxygen, silicon, and hydrogen are possible. The existence of cores in the terrestrial planets is either proven beyond reasonable doubt (Earth, Mars, and Mercury) or the case for a core is compelling as for Venus and the Moon. The Galilean satellites Io and Ganymede are likely to have cores judging from Galileo radio tracking data of the gravity fields of these satellites. The case is less clear cut for Europa. Callisto is widely taken as undifferentiated or only partially differentiated, thereby lacking an iron-rich core. Whether or not Titan has a core is not known at the present time. The terrestrial planets that do have magnetic fields either have a well-established inner core with known radius and density such as Earth or are widely agreed to have an inner core such as Mercury. The absence of an inner core in Venus, Mars, and the Moon (terrestrial bodies that lack fields) is not as well established although considered likely. The composition of the Martian core may be close to the Fe–FeS eutectic which would prevent an inner core to grow as long as the core has not cooled to temperatures around 1500 Kelvin. Venus may be on the verge of growing an inner core in which case a chemical dynamo may begin to operate in the geologically near future. The remanent magnetization of the Martian and the lunar crust is evidence for a dynamo in Mars’ and possibly the Moon’s early evolution and suggests that powerful thermally driven dynamos are possible. Both the thermally and the chemically driven dynamo require that the core is cooled at a sufficient rate by the mantle. For the thermally driven dynamo, the heat flow from the core into the mantle must by larger than the heat conducted along the core adiabat to allow a convecting core. This threshold is a few mW?m^?2 for small planets such as Mercury, Ganymede, and the Moon but can be as large as a few tens mW?m^?2 for Earth and Venus. The buoyancy for both dynamos must be sufficiently strong to overcome Ohmic dissipation. On Earth, plate tectonics and mantle convection cool the core efficiently. Stagnant lid convection on Mars and Venus are less efficient to cool the core but it is possible and has been suggested that Mars had plate tectonics in its early evolution and that Venus has experienced episodic resurfacing and mantle turnover. Both may have had profound implications for the evolution of the cores of these planets. It is even possible that inner cores started to grow in Mars and Venus but that the growth was frustrated as the mantles heated following the cessation of plate tectonics and resurfacing. The generation of Ganymede’s magnetic field is widely debated. Models range from magneto-hydrodynamic convection in which case the field will not be self-sustained to chemical and thermally-driven dynamos. The wide range of possible compositions for Ganymede’s core allows models with a completely liquid near eutectic Fe–FeS composition as well as models with Fe inner cores or cores in with iron snowfall.     

复杂空间四连杆传动系统的一种算法

1.引言 空间四连杆机构的运动关系是一个空间几何关系。确定四连杆相互位置时,存在着一球面与圆弧相交或两圆弧相交等情况,它们的运动与几何关系都以一些二次联立方程式表达。求解与根的判定都比较复杂,有时还要用迭代方法。本文所介绍的方法采用空间坐标变换,将空间四连杆机构的运动点转换到特定的平面内,利用平面三角形的几何关系求解。所用的方法都是典型的,简便易行,特别适用于计算机计算。     

三元流闭式叶轮组合电加工技术研究Ⅱ——数控电解预加工

数控电解预加工是组合电加工技术中不可或缺的关键工艺,本文专题论述了三元流闭式叶轮数控电解预加工中阴极及其运动轨迹设计等关键技术。提出了采用多个阴极分区域加工流道的方法,利用先层切再叠加的方法将三维问题简化为二维问题处理而实现阴极加工型面的数值求解。在完成阴极结构优化设计专用工装夹具设计和数控加工程序编制的基础上,以某型三元流闭式叶轮为研究对象进行了加工工艺试验,并加工了符合设计要求的三元流闭式叶轮。试验研究表明,采取数控电解预加工工艺方案能够满足实际生产要求,可提高效率40%,降低电火花加工的电极损耗50%。     

分析燃气轮机动态特性的“主导因素法”

本文利用伪随机二进制信号现场辨识的结果,与理论分析相结合,提出了分析燃气轮机动态特性的一种新设想——“主导因素法”。其基本思想是:在各个不同工况下,燃气轮机中的某个参数可以作为决定其动态响应的主导因素。这个方法对建立燃气轮机的简化数学模型有很大用处。先由设计工况点出发,取得该点的动态特性,然后根据“主导因素”的变化便可大致决定其他运行点(包括稳态工况和非稳态工况)的动态特性。实验结果和用“主导因素法”的计算结果基本吻合。