V／UHF空地数据链仿真试验研究

战术数据链是数据通信技术在军事方面的典型应用,机群协同空战过程中,拥有数据通信机群的作战效能远高于不具备数据通信的机群。本文介绍了V／UHF空地数据链的基本结构、通信链接控制模式和频分时分复用传输模式,最后,对空地数据链仿真试验状况及仿真系统的结构做了较为详细的叙述。     

战术数据链中纠错编码技术的设计

战术数据链是现代战场及时有效管理和了解高密集、快速变化的作战态势,传送信息的链路或网络,为作战飞机提供抗干扰、保密的数据通信和数字语音,同时要求信息的传输、处理、分发要做到安全、及时和有效,因此纠错编码技术在其中的作用显得尤为重要。本文讨论了战术数据链中的RS纠错编/译码的具体设计方法,对其纠错性能进行了研究,并进行了仿真。     

基于效能评估的航空作战进程预测

研究了航空对抗作战中空战双方的兵力变化问题。从飞机作战效能评估的角度出发,给出了在数据链支持下的作战飞机空战能力指数计算方法,并将其转化为平均战斗力水平,从数学原理上证明了二者具有等价性和一致性。建立了能够表征数据链效应的改进Lanchester方程航空作战模型,在考虑有增援的情形下对模型进行扩展。仿真分析了等效实力比和不同增援时刻对空战进程的影响,结果表明数据链具有提高作战效能和改变战局的作用。给出了有效增援时间范围,并指出了在增援作战时存在增援介入时间的"局部最优增援时刻点",为空战决策提供了参考依据。     

数据链对未来信息化作战的影响及建议

在目前众多的通信和指挥控制的技术手段中,数据链是表现突出、最具潜力的技术手段之一。文中主要概述了数据链的内涵和功能,分析了数据链对信息化作战的影响,并对加快我国军队数据链建设和发展提出了几点建议。     

航空数据链抗干扰技术

航空数据链是现代航空通信系统发展的主要方向,对弥补话音通信的不足、实现空地一体化的自动化指挥控制和提高航空兵整体作战能力意义重大.本文在对数据链概念、作用和特点分析的基础上,立足现代高技术条件下航空兵作战的信息保障需求,研究与探讨了军事航空数据链系统的抗干扰技术与体制.     

地面防天组网异构多源目标信息融合

时间空间配准(也称时间空间一致化),是数据链的关键基础技术之一。为解决作战平台和武器平台基于数据链的多传感器目标信息融合的高精度估计,实现传感器信息为其他运动平台用户所共享,数据链的用户需要统一时间和位置参考点。基于美军LINK16数据链应用的研究,我们主要在算法和工程环境中对实现数据链系统空间配准优化算法进行深入研究,通过半实物仿真环境验证,能够达到工程实用程度。而一般通信系统不考虑时间基准与空间位置的关系,对于高速移动的空中作战平台必然产生很大误差,但对于地面和海面移动平台影响较小。空中作战平台依靠数据链时空配准成为关键技术难点。     

战术数据链技术的发展和应用研究

以信息技术为根本动力的新军事变革,彻底改变了战争的作战形态和模式。享有"数字化战场中枢系统"之称的战术数据链因此成为现代战争中作战力量的"黏合剂"和"倍增器"。Link 4A、Link16、CDL 等战术数据链技术的发展代表了目前战术数据链技术的发展水平。而未来实现从"平台中心战"向"网络中心战"能力的转变中,战术数据链仍将发挥重大作用。     

反舰导弹协同攻击近岸目标数据链技术

针对近岸海区作战的特点,论述了反舰导弹攻击近岸海上目标的技术和战术策略,并得出数据链是实现反舰导弹协同攻击的前提条件。在分析了反舰导弹数据链的组成、类型和作用的基础上,从近岸攻击的角度,对弹载数据链技术进行了深入研究。     

未来机载数据链的网络结构研究

武器装备的不断更新和战场环境的日益复杂,要求机载数据链必须跟上未来作战形势的发展。本文在总结现有机载数据链网络结构的优点与不足的基础上,探讨未来机载数据链的网络结构发展方向及其实现的技术难点。     

未来战场上的Cable系统

美军战术数据链技术经过50多年的发展,形成了多种战术数据链并存的局面。由于它们采取的是不同的标准,彼此之间多数无法互联互通,从而造成了新-老-旧作战平台之间数据交换的障碍。为此,美国空军正在研制一种被称作目标网关(ObjectiveGateway)的数据传输机载中转设备,起到战场数据信号收集、信号格式转换和转发的数据中转站作用。目标网关数据传输中转设备将被安装到在一种远离     

Application of Ground/Air Data Link to General Aviation Operations

The Federal Aviation Administration (FAA) is currently upgrading secondary surveillance radars with systems which will have an integral data link capability, the Mode Select (Mode S) beacon system. These new systems will allow two-way data communications between ground systems (e.g., weather databases and Air Traffic Control (ATC) systems) and aircraft that are equipped with data link compatible Mode S transponders and suitable display and input devices. Initial data link services include both weather information and ATC advisories. The MITRE Corporation* is developing an in-house capability to perform end-to-end operational evaluation of data link services. Initially, a low-cost, portable pilot position man-machine interface is being developed for use in general aviation operations. The objective is to explore operational issues in laboratory and limited flight test environments, and to demonstrate these services on a data link I/O device, a laptop portable personal computer (PC) with touch panel. A group of pilots will bench test the interface design, and the results will be incorporated into the design used in flight testing. This paper describes the project's objectives and results to date, including implementation details and pilot test results.     

无人机数据链性能研究

简单介绍了无人机及其数据链,重点对无人机数据链性能进行了分析研究。研究分为地面试验和空中飞行两个阶段。在地面试验阶段,提出了一种研究数据链性能的方法和两个测试指标,初步了解了地面操纵性能;在空中飞行阶段,着重分析了数据链受干扰情况下对地面操纵的影响及一些应对策略,评价了地面遥控状态下的飞行性能。     

A GPA diagnostic system foraeroengine applications

In this research, a GPA(Gas Path Analysis) diagnostic system enhanced with GPA Index is described for gas path sensor and component fault diagnosis.A method of measurement correction is used in order that the measurement data obtained at un-standard ambient and operating conditions can be used for diagnostic analysis.The developed diagnostic system has been implemented into a Cranfield University gas turbine performance and diagnostic analysis software PYTHIA for gas turbine performance degradation analysis.The developed method and software have been applied to a model aero gas turbine engine to test the effectiveness of the system.The analysis shows that the developed diagnostic system can diagnose degraded sensor and components effectively using performance deviation measured at un-standard ambient and operational conditions.Theoretically, the idea of the diagnostic approach can be applied to different gas turbine engines.      

The W-band data collection experiment of the DAVID mission

The data collection experiment (DCE) of the scientific mission DAVID (DAta and Video Interactive Distribution) of the Italian Space Agency (ASI) will pioneer the use of the W-band for telecommunications experiments. In particular the collection of high volumes of data from remote or virtually remote sites will be achieved through the exploitation of a W-band link in a time window of a few minutes per satellite pass. The experiment will hence demonstrate the capability of the W-band channel to be used reliably for a telecommunication link. At the same time, the experiment will provide useful elements for the characterisation of the W-band channel, in order to be able to design properly future operational systems working at W-band.     

基于机器学习的飞机动力装置运行可靠性

为了研究分析飞机的动力装置在执行飞行任务过程中的运行可靠性,针对运行可靠性影响因素的多维、耦合的特点,采用机器学习方法对动力装置运行可靠性的时变规律及其相关影响因素进行分析。提出了考虑动力装置的工作状态、飞机的运行外界条件、飞机的飞行状态3类因素分析动力装置实时运行状态下的时变可靠性方法;并基于飞机实际运行的快速存取记录器（QAR）数据,梳理了动力装置运行可靠性分析相关的3类因素、16个主要特征。结合飞机运行的时空关系,采用数据包络分析（DEA）方法对飞机动力装置的工作状态特性与性能裕度进行非参数分析,基于提取的QAR数据特征,采用随机森林、多变量神经网络回归算法,建立2种基于机器学习的动力装置运行可靠性分析模型。以B737-800机型为例,对一次北京至珠海的飞行任务的动力装置相关运行数据进行分析,对2种机器学习分析模型进行训练与测试研究。分析结果表明：对动力装置工作状态特性贡献度最大的特征依次为计算空速、飞行时间与飞行高度;对动力装置性能裕度贡献度最大的特征依次为动力装置工作状态特性、雷达气象与飞行时间。所采用的2种机器学习方法能较好反映动力装置运行过程的时变可靠性规律,可为动力装置的运行与特情处理提供参考。     

A relative navigation system for formation flight

A relative navigation system based on both the Inertial Navigation System (INS) and the Global Positioning System (GPS) is developed to support situational awareness during formation flight. The architecture of the system requires an INS/GPS integration across two aircraft via a data link. A fault-tolerant federated filter is used to estimate the relative INS errors based on relative GPS measurements and a range measurement obtained from the data link. The filter is constructed based on a reduced-order model of the relative INS error process. A method for analyzing the filter performance is presented. A case involving two helicopters in formation flight is studied under three different night trajectories to account for the effect of vehicle motion on the INS state transition matrix. The results of the covariance analysis are compared with actual night results over an instrumented test range.     

Distributed decision fusion in the presence of link failures

The problem of optimal data fusion involving detector unit communication link failures is considered. Two strategies for decision making in presence of link failures are examined and an optimal decision making scheme in the sense of the Neyman-Pearson (N-P) test is proposed. The performance of q+1 reliable links versus q reliable links are examined theoretically, as well as, numerically using the receiver operating characteristics (ROCs)     

Near term approach to data relay for satellites under test

The increasing need for a continuous communications link with U.S. Department of Defense (DoD) spacecraft during test missions in low Earth orbit (LEG) has resulted in greater interest in geosynchronous data relay services. This may be a more economical alternative to building additional remote tracking stations for the Air Force Satellite Control Network (AFSCN), and avoids tying up operational assets for a test mission. A low-cost near-term approach for such a space-based data relay system would utilize two existing Defense Satellite Communication System III spacecraft, two existing ground terminals, and a small, standardized terminal using autonomous antenna pointing for the space vehicle under test. Such a system design is presented     

涡轮风扇发动机飞机性能换算方法研究

利用因次分析的方法，推导出了涡轮风扇发动机的换算系数，由此得出了涡轮风扇发动机飞机性能换算的基本准则及换算参数，即涡轮风扇发动机飞机的运动相似条件，并给出了部分换算公式。以此为基础，可以将实际条件上得到的涡轮风扇发动机飞机的性能参数换算例到标准条件。经某型收音机的试飞证明，该换算方法正确，结果可靠，完全能够为收音机定型及性能比较提供依据。     

Measuring the resilience of an airport network

Resilience is the ability of a system to withstand and stay operational in the face of an unexpected disturbance or unpredicted changes. Recent studies on air transport system resilience focus on topology characteristics after the disturbance and measure the robustness of the network with respect to connectivity. The dynamic processes occurring at the node and link levels are often ignored. Here we analyze airport network resilience by considering both structural and dynamical aspects. We develop a simulation model to study the operational performance of the air transport system when airports operate at degraded capacity rather than completely shutting down. Our analyses show that the system deteriorates soon after disruptive events occur but returns to an acceptable level after a period of time. Static resilience of the airport network is captured by a phase transition in which a small change to airport capacity will result in a sharp change in system punctuality. After the phase transition point, decreasing airport capacity has little impact on system performance. Critical airports which have significant influence on the performance of whole system are identified, and we find that some of these cannot be detected based on the analysis of network structural indicators alone. Our work shows that air transport system’s resilience can be well understood by combining network science and operational dynamics.