共查询到20条相似文献,搜索用时 31 毫秒
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The avionics of current-day aircraft is termed as modular integrated full glass cockpit. Unlike lots of dials and gauges, the pilot will interact with Multi-Function Displays (MYD). This means that the systems are coupled with multi-function displays, communication and navigation radios with control units, multi-mode interactive instruments for control and navigation, recording and fault management systems, airframes and health monitoring diagnostic capabilities. Pilot Vehicle Interface (PVI) is an important measure of good avionics and cockpit layout, which implies the optimization of man-machine interface, enhancement of the economy, and safety of flight operations. This presents the avionics architecture of a 14-seat Light Transport Aircraft (LTA) for general aviation, which has multi-role commuter capabilities. LTA is a twin turbo-prop, multi-role aircraft, with air taxi and commuter services as its primary roles. The avionics is built on the digital communication mode for both command and control with current requirements of TCAS, digital Autopilot, and AMLCD multi-purpose glass displays. The LTA Avionics suite is grouped into six major groups based on functionality: Display System, Communication System, Navigation System, Recording System, Radar System, and Engine instruments and other cockpit displays. This paper also covers details about the extensive tests carried out to prove the avionics design in terms of functionality, inter-operability, interference, and compatibility. Various practical integration and flight-test issues, methodologies, and details of the scenarios is presented herein. 相似文献
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航电系统中的高速数字视频传输技术是一项有待解决的关键技术。FC-AV是FC的一个子集,提供数字音、视频至FC的映射格式,可实现航电系统中传感器和显示器网络的视频传输。本文讨论了FC-AV的层次结构、容器系统、帧头控制协议、简单内容移动架构;并针对航电系统的需求,提出了一种采用FC-AV的视频传输方案。 相似文献
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机载视频记录仪(DVR)是记录飞机视频信息的专用设备,用于完成对平显、下显、飞行员操作画面等多路视频信息的记录。分析了MPEG2系统层规定的传输流(TS)的码流格式,探讨了其在DVR中的应用的可能性及其优点。 相似文献
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The goal of advanced cockpit display systems is to present large amounts of information quickly and in an understandable format, enabling the aviator to improve mission performance. Current front-line cockpit display systems utilize low-resolution analog video to present two-dimensional (2-D) images on many separate displays. The future cockpit will be capable of integrating large picture digital video with three-dimensional (3-D) and 2-D color images. This system will be capable of rendering icons, maps, and world-views. It will be compatible with head mounted displays and multiple large displays to improve war-planning and combat aviator situational awareness. We are developing a massively parallel 3-D renderer which will be capable of updating 500,000 3-D triangles per second with shading, lighting, transparency, texture mapping, and hidden surface removal. The renderer design employs a massively parallel architecture with 1,024 ALUs per chip to display one million anti-aliased vectors per second. Current high end workstations are capable of these display goals, but fall far short of military reliability, size, and power requirements. The rendering system will be small enough to fit on one board, extensible to dual-seat configuration, and capable of up to eight windows per display channel 相似文献
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武光梁远东李畅 《民用飞机设计与研究》2014,(3):44-47
由于平视显示器(HUD)、视景增强系统(EVS)以及合成视景系统(SVS)优秀的情景显示能力,HUD与EVS、SVS结合使用将显著提高飞行机组情景识别以及态势感知能力。同时,HUD与自动着陆系统结合使用可降低着陆和起飞时的最低天气标准。随着机组情景识别能力的提高,必须提出高效的试飞方法来验证情景识别系统的适航符合性,在分析EVS、SVS与HUD结合使用的基础上,提出综合的优化的民用飞机机组情景识别系统试飞方法以及基于任务的符合性判据。 相似文献
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A flat panel multifunction display (MFD) that offers the size and reliability benefits of liquid crystal display technology while achieving near-CRT display quality is presented. Display generation algorithms that provide exceptional display quality are being implemented in custom VLSI components to minimize MFD size. A high-performance processor converts user-specified display lists to graphics commands used by these components, resulting in high-speed updates of two-dimensional and three-dimensional images. The MFD uses the MIL-STD-1553B data bus for compatibility with virtually all avionics systems. The MFD can generate displays directly from display lists received from the MIL-STD-1553B bus. Complex formats can be stored in the MFD and displayed using parameters from the data bus. The MFD also accepts direct video input and performs special processing on this input to enhance image quality 相似文献
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机载雷达综合显示器的仿真实现 总被引:1,自引:0,他引:1
雷达综合显示器是一种能够灵活地把雷达一次信息、二次信息、地图背景和各种表格数据综合在同一个显示界面进行显示的雷达终端系统,可以形象地提供雷达威力范围内比较全面的综合信息。本文对应用Visual C++程序设计来实现航空机载雷达综合显示器的仿真问题进行了探讨。 相似文献
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嵌入式电子飞行仪表系统软件设计 总被引:8,自引:0,他引:8
设计了一种基于嵌入式操作系统的电子飞行仪表系统软件。介绍了电子飞行仪表系统的基本构成,在嵌入式操作系统上设计并实现了主飞行模式、导航模式、发动机信息模式等功能。分析了电子飞行仪表系统软件设计的原则和结构,介绍了软件的类和消息机制。此外,通过在嵌入式系统的有限资源和三维处理的复杂算法间进行合理的折衷,实现了空间变换、立体投影和曲线消隐等算法模块,构成了自行设计的三维地形引擎。软件已经在基于Intel,Motorola等多种嵌入式处理器的系统上下载成功并且能够稳定运行。 相似文献
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The multifunction display (MFD) developed for use as the primary cockpit display system on the US Air Force C-17A military air transport is described. The 6-in by 6-in color cathode ray tube (CRT) display features a self-contained 1750 processor and vector generator capable of processing MIL-STD-1553B aircraft data and raster video into any of 10 formats as selected by the pilot or copilot. The MFD can display stroke, raster, or hybrid formats in 16 colors. Raster images are driven by sensor inputs with an RS-170 or RS-343 interface. The CRT uses a taut mask delta gun design and provides the best available brightness and line-width performance. The display features small size, low weight, low power, standard interface, and adaptable software. Reconfigurability in the aircraft is enhanced by using four identical cockpit displays 相似文献
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The demand for digital cartographic data and information is expanding rapidly, most dramatically in navigation. Electronic chart and map display systems are now reaching the market for land, sea and air navigation and rapid delivery of the latest data is absolutely essential. Commercial aviation is moving rapidly toward the automated cockpit with the new generation Flight Management Computer System. Marine navigation is experiencing a similar growth in integrated navigation systems and every major automobile manufacturer has plans for digital map navigation systems. The largest, most complete data bases to meet these requirements are Government held and difficult to access, thus most private sector firms re-digitize and agencies maintain near duplicate data. Present inefficiencies, introduced errors, and delays stem from lack of rapid access and delivery of digital data. Use of newly developed satellite data broadcast technology offers a solution. 相似文献
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All weather tactical aircraft recovery and high sortie generation rates from forward, possibly battle damaged landing areas will reqire autonomous landing guidance systems which are independent of ground-based cooperative aids. A recently completed study has examined the operational requirements and assessed current and near term technology for an answer to this need. The Landing Systems Requirements/Synthesis Study has defined the Pilot/vehicle Interface and imaging sensor suite required, based on the concept of augmenting pilot forward vision with sensor imagery and guidance symbology on a HUD during low visibility landings. Image processing technology was also assessed for potential enhancement of the information presented to the pilot. This paper summarizes the final report of the Study, which is in publication. 相似文献
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Detection information from conventional surveillance radars is frequently presented in the form of a display known as the plan position indicator map. In this display, new data are displayed while data from previous scans fade from the display. Target blips typically persist for several scans, making possible operator integration or correlation. However, the noise from previous scans often masks signals from small moving targets. To avoid the loss in signal-to-noise ratio caused by the addition of noise to signal plus noise, a digital signal processing display unit has been designed and is presented here. 相似文献