GPWS方式2数学模型的建立

在研究了机载语音近地警告系统(GPWS)的基础上,建立了方式2的数学模型,弥补了在研究GPWS系统时没有数学模型的不足。方式2的警戒与警告具有特殊性,警戒区是实边界,具有确定的函数关系;警告区是虚边界,函数不确定,是由程序根据时间数据和高度数据自动判断的。该数学模型对加深语音警告系统的理解、培训、开发以及维护提供了一个新的视角。     

增强型近地警告系统(EGPWS)

目前全球97%的民用飞机都安装了普通型近地警告系统(GP-WS),这使受控撞地(CFIT)事故明显减少,但因目前安装在飞机上GPWS存在设计的局限性,仍然有CFIT事故的发生。为了解决这一问题,1998年霍尼韦尔等公司推出了增强型近地警告系统(EnhancedGroundProximityWarningSystem,简称EGPWS)。另外,FAA要求在2005年1月1日以后终止使用GPWS,而安装EGPWS。目前部分航空公司已经开始改装EGPWS,本文主要介绍EGPWS的特点和功能以及与GPWS的区别。传统GPWS的特点从1970年年初开始,许多国家就着眼于频繁出现的CFIT事故的研究。所谓C…     

驾驶舱语音控制指令的设计问题讨论

文章以机载语音控制的实时性、准确性、方便性的实际应用要求为出发点,深入讨论既适合于机载语音人机交互特性,又符合机载语音识别技术特点的语音指令的设计思想.提出机载语音控制的命令语言应该是建立在在现有汉语陆空通话语言语法及驾驶舱显控系统按键功能提示信息词汇基础之上,通过修改补充,进而形成一套有功能完整、富有层次的机载语音控制指令系统.文章同时提出,通过恰当选择控制指令的词汇读音和发音力度,能够为语音识别器提供更充分的识别信息量,提高声音信号的信噪比,有助于其在机载噪声和变异的条件下发挥出最佳的识别性能.     

驾驶舱语音控制指令的设计问题讨论

文章以机载语音控制的实时性、准确性、方便性的实际应用要求为出发点,深入讨论既适合于机载语音人机交互特性,又符合机载语音识别技术特点的语音指令的设计思想.提出机载语音控制的命令语言应该是建立在在现有汉语陆空通话语言语法及驾驶舱显控系统按键功能提示信息词汇基础之上,通过修改补充,进而形成一套有功能完整、富有层次的机载语音控制指令系统.文章同时提出,通过恰当选择控制指令的词汇读音和发音力度,能够为语音识别器提供更充分的识别信息量,提高声音信号的信噪比,有助于其在机载噪声和变异的条件下发挥出最佳的识别性能.     

近地告警系统飞行试验技术

介绍了GPWS的发展历程及我国自主研制的某型EGPWS的组成和功能,分析了试飞风险和应采取的安全措施,详细阐述了飞行试验的方法,并给出了实际试飞结果,可为我国民机GPWS产品适航性试飞提供借鉴。     

增强型近地告警系统

美国联邦航空局(FAA)1975年规定121部的飞机需强制装备近地告警系统(GPWS),1994年4月又规定135部的飞机10座以上者也要装备GPWS。国际民航组织(ICAO)也赞成国际上所有最大起飞重量5700千克以上的商业飞机或9座以上客机均需装备GPWS。近期还利用终端雷达探测进近飞机,如发现它低于最低安全高度就给予警告。这些措施都有效地减少了可控飞行撞地事故(CFIT),但这种事故仍时有发生。     

增强型近地警告系统的特性及实现

增强型近地警告系统是预防可控飞行撞地事故的重要手段。形警戒”和“地形显示”2大功能及其实现原理和过程进行了分析。法进行了探讨。通过与GPWS系统的比较，对EGPWS新增的“前视地并对GPWS系统的改进和EGPWS新增功能实现的方     

空管模拟机的IBM ViaVoice技术实现研究

阐述了空管模拟机自动机长席位的实现方法。通过对语音识别技术的研究,在引进IBMViaVoice语音识别系统的基础上,根据空管模拟机的功能需求,通过对其主控软件的改进,使语音识别技术与管制训练控制系统有机结合,实现了自动机长席位对非特定管制学员、连续管制指令语言的识别和仿真模拟雷达显示控制。     

语音技术在智能仪器中的应用初探

在智能仪器中采用语音技术可改变传统仪器的“聋哑”状况 ,使仪器运行状况更为明晰 ,仪器操作更为可靠。本文介绍了语音的合成与输出技术 ,并就智能仪器中使用语音技术的方法进行了探讨。     

话语标记"好了 "的语法化过程及无标化分析

分析了现代汉语中＂好了＂虚化为话语标记的两种可能的途径：动词的省略和词汇化,并从句法层面分析了＂好了＂虚化的最终结果导致了句子结构简化,从而达到语言输出的无标记化。     

A fault-tolerant triple-redundant voice coil motor for direct drive valves: Design, optimization, and experiment

A direct drive actuator (DDA) with direct drive valves (DDVs) as the control device is an ideal solution for a flight actuation system. This paper presents a novel triple-redundant voice coil motor (TRVCM) used for redundant DDVs. The TRVCM features electrical/mechanical hybrid triple-redundancy by securing three stators along with three moving coils in the same frame. A permanent magnet (PM) Halbach array is employed in each redundant VCM to simplify the system structure. A back-to-back design between neighborly redundancies is adopted to decouple the magnetic flux linkage. The particle swarm optimization (PSO) method is implemented to optimize design parameters based on the analytical magnetic circuit model. The optimization objective function is defined as the acceleration capacity of the motor to achieve high dynamic performance. The optimal geometric parameters are verified with 3D magnetic field finite element analysis (FEA). A research prototype has been developed for experimental purpose. The experimental results of magnetic field density and force output show that the proposed TRVCM has great potential of applications in DDA systems.     

Use of heads-up displays, speech recognition, and speech synthesisin controlling a remotely piloted space vehicle

Experiments are reported in which heads-up displays and voice input/output were implemented on an experimental pilot console. These displays and controls were developed interactively during the simulation of remotely piloted space vehicles (RPSVs) and US Space Station operations. Demonstrated and evaluated were seven heads-up reticle displays, two heads-up data displays, selection of displays by voice command, use of voice command to call for range and rate data, and the voice annunciation of alarms. The simulation laboratory architecture is described     

Novel AC line conditioner for power factor correction

A new ac line conditioner is presented for high input power factor and clean ac output voltages for isolating the linear or nonlinear loads. A three-phase two-leg switching mode rectifier with neutral-point-clamped topology is proposed to draw the sinusoidal line currents from the ac mains. The carrier-based current controller is used in the inner control loop to track the line current commands with unity power factor. The dc bus voltage controller is adopted in the outer control loop to regulate the dc-link voltage. A voltage compensator is used to balance the neutral point voltage on the dc tank. A three-phase two-leg inverter with neutral-point-clamped topology is adopted in the system to provide the clean ac output voltages to the critical or sensitive loads. The carrier-based current control scheme is adopted to improve the instantaneous output voltages. Experimental results show the validity and effectiveness of the proposed control strategy.     

并行处理发动机/控制系统半实物仿真

以高速微信号处理器ＴＭＳ３２０Ｃ３０为阵元机,研制了８阵元总线并行处理计算机系统,建立了涡轴发动机非线性仿真模型,仿真模型在并行处理机上并行计算实现实时。该实时仿真器通过输入输出接口与涡轴发动机的实际控制系统进行连接,组成涡轴发动机／控制系统半实物闭环系统,并进行了稳态和动态仿真。     

Digital Frequency-Lock Generator

A digital frequency-lock generator has been developed which produces an output pulse train automatically locked to the pulse repetition rate, or frequency, of an input pulse train. This device, which exhibits a wide capture range and has no static output frequency drift, offers several advantages over a phase-lock loop in frequency-locking applications.     

低功耗数字气压计的设计

介绍了一种低功耗数字气压计的软硬件实现方法。通过气压传感器获得与大气压相对应的模拟电压值,并经过A/D变换输入到单片机进行处理,从而实时显示相应的气压值。通过休眠或掉电的方式降低了仪器的耗电量,使用一支高容量锂/亚硫酰氯电池供电可以连续使用8年以上。     

一种进气道流场畸变模拟装置的研究

提出了一种用于进/发匹配的畸变模拟板与紊流发生环组合畸变模拟技术,根据该技术所设计的畸变模拟装置由可调节角度的模拟板以及可换装的紊流环组成,轴向长度仅等于通道截面一倍当量直径。通过实验研究得到了可调畸变模拟板与可换紊流发生环的几何设计参数及其组合状态下的气动性能变化规律,为该组合模拟技术的进一步运用打下了基础。      

液体冲压发动机控制系统半实物仿真

运用小偏离线性化理论和Willoh方法，建立了液体冲压发动机和弹体动态数学模型。动态数学模型在微型计算上一体化运行，形成液体冲压发动机／弹体一体化实时数字仿真器。实时数字仿真器通过输入输出接口与液体冲压发动机的实际控制系统进行联接，组成液体冲压发动机、弹性和发动机控制系统半实物仿真系统。对冲压发动机飞行马赫数和控制 系统供油量的半实物仿真结果表明，系统能满足研制工作的需要。     

飞行模拟转台高精度数字重复控制器的设计

从工程的角度讨论了离散重复控制系统的设计,所提出的重复控制方法可保证速度跟踪误差快速收敛为零。在重复控制器中采用了高阶低通滤波器和动态补偿器,改善了跟踪精度,保证了系统的稳定性,减少了周期性扰动误差。将所提出的方法应用于飞行模拟转台伺服系统的速度控制中,仿真结果表明,针对周期指令信号和周期干扰信号可保证较高的跟踪精度和较强的稳定性和鲁棒性。     

Frequency-controlled series-resonant converter with synchronous rectifier

This paper presents an analysis and experimental results for a frequency-controlled series-resonant dc-dc converter that consists of a Class-D zero-voltage-switching (ZVS) series-resonant inverter and a center-tapped synchronous rectifier. If the dc output voltage is low, the efficiency of the converter is dominated by the efficiency of the rectifier. Low on-resistance metal-oxide-semiconductor field-effect transistors (MOSFETs) are used in the rectifier instead of diodes because the forward voltage drop across the rectifying device is low, resulting in a high efficiency. The dc output voltage is regulated against variations in the load resistance and the dc input voltage by varying the operating frequency. Experimental results are presented for a converter with a dc input voltage of 150 V, an output voltage of 5 V, and a dc load resistance ranging from 0.5 to 5.5 R. The measured efficiency was 86% for a 50 W output and 89% for a 25 W output. The theoretical results were in good agreement with the measured results.