共查询到20条相似文献,搜索用时 203 毫秒
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综合化航电系统的安全问题将是系统设计者的主要挑战之一,密钥管理是解决安全问题的基础.综合化航电系统的密钥管理不同于联合式航电系统,不存在专用的安全模块和加密总线,因此密钥及保密数据的加载需要新的方式.从综合化航电系统的特点出发,从地面到空中全方位考虑密钥的生成、加载、分配、存储以及擦除的过程,给出了航电系统密钥管理的一个具体方案,并对该方案的优缺点进行了分析,表明该方案具有较好的安全性. 相似文献
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航空电子设备的支援方式正在发生变化.航空公司在接收装有最新数字式航电设备的新飞机的同时,还要继续运营一些安装了老的航电设备的飞机.随着新一代航电设备的日益复杂化,OEM(制造商)不愿意提供这些设备的专有数据,减少了航空公司选择非OEM维修的可能性,而OEM在向客户提供全寿命期支援时,也很难满足各航空公司独特的运营需求. 相似文献
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分析研究了开放式系统结构技术发展现状及典型装备应用案例,深入剖析国内外开放式系统结构标准情况,在此基础上,结合我国目前的开放式航电系统研究现状,提出构建我国开放式航电系统的标准体系,并针对重点标准进行分析,积极探索我国开放式系统结构标准建设之路. 相似文献
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航电系统在使用或升级改造过程中进行可靠性检测是必不可少的。特别是在当前批量航电系统大量投入使用的背景下,迫切需要能高效、快速、准确地对系统进行可靠性检测。由于航电系统安全性要求高,内置检测软件受限,需要外置检测设备通过航电系统指定接口进行检测,检测过程也不允许出现任何泄露等行为。检测设备与具体航电系统耦合,检测过程与具体检测设备耦合,难以实现批量航电系统并行检测。为此,通过引入逻辑检测设备,给出了一种航电系统并行检测分层框架,解决检测设备与被测系统耦合的问题,同时也保证了检测的安全性。通过逻辑检测设备、检测跳转机和被测主机上检测行为的描述,给出了一种面向通用航电系统并行检测的检测设备协同机制,解决检测过程与检测设备耦合的问题,从而支持多个航电系统并行检测。最后,实现了一个通用航电系统并行检测系统,并通过实际应用和实验对比验证所提方法的有效性。 相似文献
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分级式航空电子综合化仿真系统研究 总被引:2,自引:0,他引:2
介绍一个分级式航空电子综合化仿真系统。该系统以航空电子综合化工程中一个分系统为仿真目标,由两层双余度1553B总线和MBI(multiplex bus interface)将AVS(Avionics simulator)、SSCU(subsystem control unit)、若干个EQS(equipment simulator)以及部分真实设备连成的三级分布式计算机系统。一个面向实时控制的分布式操作系统和相应的仿真软件分布在三级仿真器中;其中,分布式操作系统实现两级总线的衔接、通信控制、并行多任务管理、错误检测、故障处理和实时内存数据库管理,仿真软件模拟航空电子上层环境、操作员控制与显示、分系统各设备数据产生与接收数据处理以及信息处理应用任务。系统研制成功为工程化实现打下了技术基础并提供了一个实验环境。 相似文献
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AlliedSignal Commercial Avionics Systems (ASCAS) and its partners have established the following business objectives: short term (forward-fit and retrofit with off-the-shelf products; co-development of integrated systems); mid term (co-production of avionics products in the CIS); long term (become an integrated element of CIS aerospace industry in partnership with local firms and to maintain the necessary focus to achieve these goals). ASCAS has formed a strategic business enterprise which is dedicated to developing the avionics market within the CIS. ASCAS was fortunate to find a joint venture partner who possesses skills that complement its present core competencies. The advantage of this business arrangement is that, while expanding their experience and expertise in the area of systems integration, they can directly benefit from the expertise and capabilities of indigenous airframe and equipment manufacturers (customer knowledge, simulation and integration experience, capable/skilled manpower) 相似文献
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《Aerospace and Electronic Systems Magazine, IEEE》2000,15(10):79-82
The emergence of a world-wide duopoly in the design and production of large commercial aircraft at the end of the 1990s and cutbacks in aerospace and defense has put significant pressure on the number of avionics manufacturers. A similar duopoly exists very nearly for US military aircraft. In 1999, mergers created two large avionic suppliers in the USA. European avionics suppliers have also been consolidating. At worst, these larger entities will have a negative effect upon US aerospace employment, and further discourage the best and brightest engineers. Commuter and general aviation, where competition still reigns (more than ten manufacturers exist in 2000), may lead the avionics charge into the future 相似文献
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Ketterling George W. Vogel Raymond C. Briggs Shirley M. 《Aerospace and Electronic Systems Magazine, IEEE》1986,1(4):17-26
Avionics and electronic equipment installed in aircraft and air breathing missiles are required to operate without upset or damage when subjected to EM environments caused by lightning, NEMP, and Intrasystems transients. To simplify the design effort required to protect electronic equipment and minimize overlapping transient requirements and qualification tests, unified test requirements and procedures are needed. The goal of these unified test procedures would be to insure a known susceptibility level for each newly designed electronic Line Replaceable Unit (LRU). Ten avionics equipments in current Air Force inventory were tested for the purpose of developing unified procedure test methods. Operating LRUs were subjected to transients using common mode cable current (CMCC), groung potentials and chatteriing relay cable injection methods. Based on observed test results and review of current test requirements, test methods and test levels for unified test procedures for power-on transient tests of avionics equipment have been formulated. 相似文献
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Parish D.J. Briggs R. Chambers D. Hunter C. Kelsall N. 《Aerospace and Electronic Systems Magazine, IEEE》1998,13(3):34-39
The issue of meeting the higher communications requirements of future aircraft avionics systems in an incremental manner is addressed. A communications architecture is proposed which is based upon a switched network technology from the telecommunications area asynchronous transfer mode (ATM). However, the major step of migrating all existing avionics equipment into an ATM compliant form is avoided by the process of “emulating” a current avionics data bus such as MIL-STD-1553B over an ATM network. This allows current 1553 subsystems to co-exist with ATM compliant equipment on a single physical ATM network 相似文献
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论述不完全弹道测量的数据融合处理问题。在惯性器件天地关系一致的前提下,导弹惯性器件误差补偿量变化规律,就反映了飞行中制导工具误差的变化规律,即遥外差的变化规律。因此,可以利用补偿量视速度的变化规律约束条件,内插出不完全测量段落的遥外差数据,在建立节省参数的弹道估计的联合模型基础上,融合少量的高精度测元来解算弹道参数。落点验算表明:利用该方法计算的落点接近实际落点。 相似文献
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简要叙述了航空电子发展的历程;重点介绍了2l世纪初期航空电子发展的特性及其发展中的不变因素;最后,提出了发展我国航空电子的某些建议. 相似文献
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在无线移动场合下,DDN中继信道的中断比固定场合下频繁得多,DDN设备中断恢复时间长的问题就变得突出起来,这使得DDN电路的可用性远小于DDN中继信道的可用性。本文基于航天测控通信系统使用的DDN设备,分析了DDN设备中断恢复时间长的原因,提出了减少DDN设备中断恢复时间的方法。 相似文献