共查询到20条相似文献,搜索用时 140 毫秒
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本文介绍了北方航空公司机场客运CBT教学系统的总体结构,特点及其各部分功能,并介绍了系统的实现及性能维护。 相似文献
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计算机辅助训练简称CBT,是ComputerBasedTraining的缩写。CBT用于飞行员训练已经有比较长的时间,是一种行之有效的低成本的训练方法。世界上绝大多数航空公司都接受了这种训练飞行员的方法,波音、空客等世界著名的飞机公司也用CBT培训飞行员。可是,用CBT培训;飞机维护人员是否可行,国外目前的发展状况如何,下面将给予介绍。一、CBT能有效地用于飞行员培训的原因对从事飞行员培训的业内人士来说,CBT是一种极为优秀的训练方法,用户和管理人员都认为它可提供高水平的过渡训练。CBT之所以能有效地用于飞行员培训,最主要的原… 相似文献
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CBT在维修培训中的应用 总被引:1,自引:0,他引:1
《国际航空》1998,(1)
计算机辅助培训(CBT)用于飞行员训练已有比较长的时间了,它是一种行之有效的低成本的训练方法。世界上绝大多数航空公司都采用这种方法培训飞行员,但用CBT培训飞机维修人员是近年才开始的一项尝试。CBT没有广泛用于飞机维护人员培训的主要原因是:第一,飞机维护人员培训历来都是采用岗位培训(OJT)的方法进行机型改装培训,以致形成了对采用新方法的抵制态度;第二,这种守旧思想反映了害怕采用CBT技术而导致失业的心态;第三,绝大多数飞机维护人员仍然认为“师傅知道得最多”。 相似文献
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波音757飞机维护CBT课件的开发与研制 总被引:7,自引:0,他引:7
官颂 《中国民航学院学报》2001,19(1):58-62
简述了CXBT课件的基本概念和波音757飞机维护CBT飞机维护CBT课件的开发制作过程,以及利用Authorware开发软件制作多媒体课件的技术难点和实现方法,使用模板、知识对象、库、变量和函数等开发多媒体课件的技巧。 相似文献
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对航空公司来说,培训是一项复杂且耗资巨大的工程。因此,高效、低成本的培训方法一直是人们追求的目标。计算机辅助教学系统(CBT)的出现和使用,从某种意义上说满足了人们的这一愿望,已成为当今发展最迅速的先进教学手段之一。CBT的功能与应用过去,飞行员的基础教学往往是教员利用黑板、幻灯向教室里的学员传授知识。此时,学员仅仅是被动的观察者,而教员的教学进度不可能满足每位学员的情况。由高速处理器、大尺寸彩色触敏显示器、大容量存储磁盘及音频系统组成的CBT实际上是集视频、图形、动画、文本显示为一体的多媒体工作站,它可以独立工作亦可与文件服务系统联网。学员可根据自己的情况,选择学习内容。人机对话 相似文献
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本文讨论了航空维修企业的发展现状和趋势,探讨从企业资源管理系统(ERP)、办公自动化系统(OA)、计算机辅助培训(CBT)和客户关系管理(CRM)四个方面进行信息化,整合信息资源,以提高其核心竞争力。 相似文献
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无人机系统的使用日益广泛,因此将无人机系统并入到现有的空域管理系统中显得尤为迫切。在技术层面,无人机系统有一系列独特的适航特点。因此,应重点发展针对无人机系统的适航标准与验证。研究了有人驾驶飞行器的适航标准(CS-23),及其通过剪裁后成为专门适用于无人机系统的适航标准(STANAG4671),这将促进无人机系统的技术更加标准化,并有利于国内无人机系统民用适航标准的发展。 相似文献
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《中国航空学报》2020,33(11):2851-2863
Recent years have witnessed a booming of the industry of civil Unmanned Aircraft System (UAS). As an emerging industry, the UAS industry has been attracting great attention from governments of all countries and the aviation industry. UAS are highly digitalized, informationized, and intelligent; therefore, their integration into the national airspace system has become an important trend in the development of civil aviation. However, the complexity of UAS operation poses great challenges to the traditional aviation regulatory system and technical means. How to prevent collisions between UASs and between UAS and manned aircraft to achieve safe and efficient operation in the integrated operating airspace has become a common challenge for industry and academia around the world. In recent years, the international community has carried out a great amount of work and experiments in the air traffic management of UAS and some of the key technologies. This paper attempts to make a review of the UAS separation management and key technologies in collision avoidance in the integrated airspace, mainly focusing on the current situation of UAS Traffic Management (UTM), safety separation standards, detection system, collision risk prediction, collision avoidance, safety risk assessment, etc., as well as an analysis of the bottlenecks that the current researches encountered and their development trends, so as to provide some insights and references for further research in this regard. Finally, this paper makes a further summary of some of the research highlights and challenges. 相似文献
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《Aerospace and Electronic Systems Magazine, IEEE》1987,2(8):13-18
Naval aviation electronics (Avionics) systems are specified and procured using MIL-STD-461 to set the fundamental EMI requirements. MIL-STD-461 permits and encourages ``tailoring' the EMI specifications for each equipment to the anticipated usage. In this paper, the Naval Avionics Center Staff Engineer for Electromagnetic Effects presents a typical tailored EMI specification as used within the Naval Air Systems Command to procure carrier based aircraft avionics. Included are the rationale for and the explanation of each modification and an estimate of the electromagnetic environment found aboard the US Navy Aircraft carriers. 相似文献
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Xavier Prats Eduard Santamaria Luis Delgado Noel Trillo Enric Pastor 《Aerospace Science and Technology》2013,24(1):95-100
This paper presents a methodology to extend the guidance functionalities of Commercial Off-The-Shelf autopilots currently available for Unmanned Aircraft Systems (UAS). Providing that most autopilots only support elemental waypoint-based guidance, this technique allows the aircraft to follow leg-based flight plans without needing to modify the internal control algorithms of the autopilot. It is discussed how to provide Direct to Fix, Track to Fix and Hold to Fix path terminators (along with Fly-Over and Fly-By waypoints) to basic autopilots able to natively execute only a limited set of legs. Preliminary results show the feasibility of the proposal with flight simulations that used a flexible and reconfigurable UAS architecture specifically designed to avoid dependencies with a single or particular autopilot solution. 相似文献
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《中国航空学报》2021,34(3):200-224
Unmanned Aircraft Systems (UASs) have advanced technologically and surged exponentially over recent years. Currently, due to safety concerns, most civil operations of UAS are conducted in low-level uncontrolled area or in segregated controlled airspace. As the industry progresses, both operational and technological capabilities have matured to the point where UASs are expected to gain greater freedom of access to both controlled and uncontrolled airspace. Extensive technical and regulatory surveys have been conducted to enable the expanded operations. However, most surveys are derived from the perspective of UAS own operating mechanism and barely consider interactions of their non-segregated activities with the Air Traffic Management (ATM) system. Hence, to fill the gap, this paper presents a survey conducted from the perspective of Air Navigation Service Provider (ANSP), which serves to accommodate these new entrants to the overall national airspace while continuing flight safety and efficiency. The primary objectives of this paper are to: (A) describe what typical ANSP-supplied UAS Traffic Management (UTM) architecture is required to facilitate all types of civil UAS operations; (B) identify three major ANSP considerations on how UAS can be accommodated safely in civil airspace; (C) outline future directions and challenges related with UAS operations for the ANSP. 相似文献
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机载机电系统综合控制管理(简称公管系统)是机载机电设备发展的必然趋势,为了研究公管系统对机电子系统的控制、管理功能,需要对子系统进行建模仿真。本文针对某型飞机环控温度控制系统工作过程对环控温度控制系统关键附件进行了数学建模,同时针对某课题研究内容的需要,研究如何采用半物理仿真的方法对飞机环控温度控制系统进行系统建模和环境仿真并进行了系统仿真验证试验,最后给出结论。 相似文献
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