Maritime border control multisensor system

This focuses on the classification task performed into a multi-sensor system for the coastal surveillance. The system is composed of two platforms of sensors: a land-based platform equipped with a land based radar, an Automatic Identification System (AIS) and an infrared camera (IR); an airborne platform carrying an airborne radar that can operate in a spotlight Synthetic Aperture Radar (SAR) mode, a video camera, and a second IR camera. The tasks performed by the system are the detection, tracking, identification, and classification of multiple targets, the evaluation of their threat level, and the selection of an intervention on them. The classification algorithm implemented inside the system exploits an analytical approach based on the confusion matrix (CM) of the imaging sensors that belong to the system. Some measures of effectiveness (MoE) of the system are evaluated, considering both cases where an ideal error-free classification process and a non-ideal classification process are performed.     

A parallel computer architecture for continuous simulation

A parallel computer specifically designed for the solution of ordinary differential equations is described. The first version of the machine contains thirty-two processors, running in an asynchronous multiple-instruction/multiple-data mode, communicating with high-speed parallel busses. Synchronization is accomplished by a microprogrammable communication controller. A number of processors have been designed and built for the machine. The processor types offer a wide variation in solution speed and accuracy. To permit easy comparisons with analog and hybrid systems, performance is measured by finding the highest frequency sine wave which can be integrated in real time with an accuracy of 0.1% or higher. Using this performance measure the performance limit of the current machine is 2000 Hz. The structure is capable of solving systems described by differential equations up to order sixty-four at these performance limits     

仿真技术在涡喷发动机中的应用和发展

分析了仿真技术对于涡喷发动机研究和开发工作的重要意义,介绍了当前涡喷发动机仿真技术的发展状况、最新进展,以及关键技术,并提出了今后研究的重点.     

基于声学CT重建航空发动机燃烧室出口温度场的仿真研究

结合声波传感器与计算机断层成像技术,提出一种航空发动机燃烧室环形出口温度场重建的方法.首先确定了航空发动机燃烧室出口处声波速度与温度的数学模型,然后用最小二乘方法对航空发动机燃烧室环形出口温度场进行了重建.仿真结果表明,温度场重建结果的相对平均误差在3%以内,相对最大误差在6%以内,该方法具有测温范围宽,可测得航空发动机燃烧室环形出口截面温度分布等优点.     

仅油门控制试飞仿真研究

分析了国外仅油门控制(TOC)飞行事故案例,探讨了TOC飞行原理,进行了TOC仿真建模,设计了爬升与改平、转弯及着陆三个典型的试验点,并提出相应的评价方法。最后邀请多名试飞员在高级模拟器上进行了大量的仿真试验,验证了TOC飞行的可行性和评价方法的适用性,指出了TOC试飞研究和模拟训练对提高飞行安全的重要性。     

粉末涡轮盘力学性能的计算机预测

通过对采用直接热等静压工艺制备的粉末高温合金涡轮盘的性能与淬火冷速的关系分析,建立了盘件淬火计算机模拟分析的基本技术,可用于盘件的淬火冷速分析和组织性能预测.与实际比较,力学性能预测结果达到了很高的精度,为盘件材料的研制提供了强有力的工具.     

Issues in human/computer control of dexterous remote hands

Much research on dexterous robot hands has been aimed at the design and control problem associated with their autonomous operation, while relatively little research has addressed the problem of direct human control. While many of the issues in mixed computer/human control of dexterous hands parallel those found in supervisory control of traditional remote manipulators, the unique geometry and capabilities of dexterous hands pose many new problems. Among these are the control of redundant degrees of freedom, grasp stabilization and specification of nonanthromorphic behavior. An overview is presented of progress made at the MTI AI Laboratory in control of the Salisbury three-finger hand, including experiments in grasp planning and manipulation by controlled slip. The author also suggests how it might be possible to introduce human control into the process at a variety of functional levels     

等离子体控制边界层法流动仿真研究

使用泊松方程、漂移-扩散模型和N-S方程对介质阻隔面放电等离子体控制边界层流动进行了一体化数值模拟.仿真结果表明介质阻隔面放电等离子体通过推-拉空气可以对低速气流进行控制,正向推力和反向拉力均可以在距壁面一定高度处形成射流,正向射流自身增加边界层动量,更重要的是通过引射主流将主流中的能量输运到边界层中,从而减小边界层厚度;反向射流与来流相撞后形成回流区将边界层向外推,能够增加边界层厚度.     

驾驶员模糊控制模型与仿真分析

根据飞机驾驶员的控制行为,建立了驾驶员的基本模糊控制模型,然后利用李雅普洛夫综合法设计了两种自适应算法,来调整基本模糊控制模型的某些参数,建立了两类自适应模糊控制模型。对风切变大气环境下飞机进场下滑过程进行了仿真计算,结果表明,所建立的模型是合理的,能在一定程度上反映驾驶员的操纵情况。     

磁悬浮系统的模糊控制仿真研究

以开环不稳定和强烈非线性的磁悬浮转台为研究对象,其控制器性能的好坏直接影响到磁悬浮转台的动态性能。模糊控制因其简单实用,不需要精确的数学模型等特点而成为磁悬浮控制系统的理想选择。采用模糊控制方法实现对磁悬浮转台的数字控制,利用M atlab模糊逻辑工具箱中的FIS(Fuzzy Inference System)编辑器,结合S imu link工具箱建立了模糊控制系统的仿真模型,并对整个系统进行了仿真和实验。仿真结果表明模糊控制器在磁悬浮转台起动和悬浮时响应速度快,稳定性好,抗干扰能力强。     

基于 GPS 和电子海图的落水人员搜救定位系统

现阶段我国的海上搜救工作仍然采用救生衣方式的被动求救和大面积搜索的模式,搜救效率较低.为了解决了这个问题,本文设计实现了基于全球定位系统(GPS)和电子海图的落水人员搜救定位系统.该系统将 GPS、地理信息系统(GIS)、数据库同步、无线传输技术有机结合,有效保障了落水人员的精确定位,为救援船舶及时追踪落水人员提供了可靠的依据     

Space and Maritime Strategy

A globally deployed Navy requires and uses space systems and services. Specific mission support areas of communications, navigation, environmental data, and surveillance are discussed in terms of requirements and program developments. Navy role in pioneering space systems combined with threat assessment validates Navy position of space system acquisition and operation in the future.     

某 Bump 进气道流动控制计算研究

以某 Bump(凸包)进气道为研究对象,采用 CFD 数值模拟技术对其内、外流场进行计算,重点研究超声速来流马赫数 M∞=1.60下进气道气动、流场特性;根据进气道内、外流场特点,分别设计机身棱线涡扰流片、进气道抽吸及射流流动控制装置,目的在于提高飞机 M∞=1.60来流、进/发匹配点条件下进气道总压恢复、降低出口流场畸变;采用 CFD 技术对各流动控制装置效能进行计算,基于计算结果,对各流动控制装置效能及典型装置流动控制机理进行了分析。研究表明,M∞=1.60来流、负迎角下,扰流片作用不明显;采用进气道抽吸或射流控制措施,对提高进气道总压恢复有效。研究结果可为类似 F-35那样的隐身战机 Bump 进气道流动控制或工程发展提供一定的技术参考。     

Maritime Containers Tracking Trial Results

There are approximately 7 million maritime-style containers within Canada, and 70 million within the US. The interiors of such containers are rarely inspected. With market globalization, a large amount of these containers enter North America on a daily basis. Such containers may include contraband or dangerous items that present an economic or security risk. Despite significant security improvements, only 3 to 5 % of the maritime containers, that arrive in, or transition through, North America, go through physical inspection. Current container tracking technologies based on GPS consume high DC power, are costly, require line-of-sight with satellites, and are often too large to be covert. It is possible to overcome some of these limitations by basing the tracking system on the FM broadcast signal which is an alternative man-made signal that is reasonably ubiquitous, provides a geographically-unique frequency spectrum and is about 100,000 times as strong as a GPS satellite signal. This allows the development of a low-cost, low-power and miniature FM receiver that can record frequency spectrums and compare them to known data in order to trace the path that the container has taken for less than $10 per container. This presents the first results of highway trials (train and sea trials are currently being conducted) of such a low-cost, covert, non-GPS based technology (called FM Tag) that records the worldwide displacement of containers and displays the path undertaken by the container while in transit. As an added security benefit, the tag is also capable of detecting container door openings. In addition to presenting the first trial results, this covers the innovative engineering aspects of using the metal enclosure of a maritime container as a VBF antenna, thereby eliminating the need to add an external antenna and achieving the goal of being 100% covert.     

美国海军打造制海网络中心战

大型反潜飞机在制海网络中心战中起着重要作用,它既可以长时间地飞行,搜索和分析敌情,捕获来自海上和陆上的计算机系统、防空系统和机动弹道导弹系统发出的电子信息,又能将关键数据传送到诸如F/A-22、EA-18G等作战飞机上,使之用高杀伤力的弹药杀伤力的弹药或非致命的定向能武器进行攻击.     

IFSTA自主着舰控制律仿真研究

针对舰载机的自动着舰系统,以IESTA原型机K8飞机为研究对象建立了着舰环境模型,设计了自动着舰控制律,对在着舰阶段的控制作用及影响着舰精度的因素进行了分析和研究,并分别进行了数值仿真和半实物地面仿真验证.研究结果表明,为了使飞机成功完成着舰任务,需满足海况、大气扰动、控制系统带宽频率的最低要求.     

喷流流动控制增升效应数值模拟

飞机的增升系统是影响其起降性的重要因素,为了研究飞机下表面喷流流动控制增升效应,采用数值模拟方法与结构网格求解不可压Navier-Stokes方程,对NACA0012翼型和机翼进行研究。通过改变喷气口的参数来研究其对翼型和机翼气动特性的影响。对于翼型,主要研究喷气口速度和位置对翼型气动特性的影响;对于机翼,主要研究喷气口区域沿展向分布和喷气速度对机翼气动特性和能量利用率的影响。计算结果表明:采用喷气控制可以获得较好的气动特性,增升效果也比较明显,控制效果和上述几个参数均有一定关系。本次研究为机翼喷气口设计以及机翼局部喷气控制展向分布的选取提供了依据。     

A method of obtaining signal components of residual carrier signalwith their power content and computer simulation

An algorithm for obtaining all signal components of a residual carrier signal with any number of channels is presented. The phase modulation type may be NRZ-L or split phase (Manchester). The algorithm also provides an easy way of obtaining the power contents of the signal components. Steps to recognize the signal components that influence the carrier tracking loop and the data tracking loop at the receiver are given. A computer program for numerical computation is also given