航空波形和集成模块化航空电子系统的效率改进

Tan Zheng Hui Ernest, A. Krishna, A. Madhukumar, Rajendra Prasad Sirigina
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引用次数: 2

摘要

未来十年,空中交通将出现前所未有的增长,飞机上将安装更多的航空电子系统,以满足新的服务、安全和可靠性要求。由于联邦架构下的空间限制,后者引发了航空电子架构向下一代集成模块化航空电子(IMA)的演变。此外,新的航空电子系统和通信需求将加剧本已受限频谱的数据容量需求。因此,必须提高现有航空电子通信系统的频谱效率,或者必须确定新的高数据容量通信技术,以便在饱和的航空频段内与其他航空电子无线电共存。本文讨论了航空电子通信波形的效率改进和IMA结构。提出了一种新的航电波形调制技术,并对其在航空通信信道中的应用进行了评价。此外,IMA第二代(IMA 2G)将通信、导航和监视无线电以及其他航空电子应用集成到ARINC 653标准中,该标准支持分区操作系统,提出并讨论了更高效架构的概念。这包括在独立的IMA分区内运行的航空电子波形的集成。优化整个IMA系统框架中的应用程序将减少航空电子硬件(IMA模块)的数量。减少航空电子硬件的数量,加上灵活或可重构的硬件,将减少电缆和相关连接器的数量,从而有助于减少飞机的总重量。因此,从航空电子设备的角度来看,这将提高燃油效率。
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On the efficiency improvements to aeronautical waveforms and integrated modular avionics systems
The coming decade will see an unprecedented air traffic growth and the installation of more avionic systems onboard aircrafts, in response to new services, safety and reliability requirements. The latter has triggered the evolution of avionic architecture towards the next generation Integrated Modular Avionics (IMA), due to space constraints under the Federated architecture. Furthermore, newer avionic systems and communication requirements will exasperate data capacity demands in the already constrained spectrum. Therefore, the spectral efficiency of existing avionic communication systems must be improved or new high data capacity communications technologies must be identified that can coexist with other avionic radios in the saturated aeronautical bands. In this paper, the efficiency improvements to avionic communication waveforms and the IMA architecture are addressed. In particular, a new modulation technique is proposed for avionic waveform and is evaluated for aeronautic communication channels. Also, a concept for a more efficient architecture is proposed and discussed within the IMA second generation (IMA 2G) that integrates the communication, navigation and surveillance radios together with other avionic applications into an ARINC 653 standard, which supports a partitioned Operating System. This includes the integration of the avionic waveforms to run within an independent IMA partition. Optimization of applications in the overall IMA system framework will reduce the number of avionics hardware (IMA Modules). Reducing the number of avionics hardware, coupled with flexible or reconfigurable hardware, will result in reduced cabling and associated connectors, thus contributing to the reduction in the overall weight of the aircraft. This will consequently boost fuel efficiency from an avionics perspective.
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