符合DO-178B标准的距离测量设备的软件定义架构和前端优化

Farzan Farhangian, Behnam Shakibafar, Bobda Cedric, R. Landry
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引用次数: 0

摘要

在空中导航技术中,有许多技术能够提高航空的可持续性和精度,特别是在替代定位、导航和定时(APNT),特别是航空电子测距设备(DME)、甚高频全向测距(VOR)等方面。这些空中导航解决方案的集成可以在空中机动、空中交通管理和自主操作方面实现强大而高效的准确性。设计合适的射频前端、功率放大器和软件定义应答器可以为实现优化的航空电子导航解决方案铺平道路。在本文中,为了实现一种新颖的软件定义DME架构,研究了与单个低成本软件定义无线电(SDR)一起使用的最佳前端的可能性。我们的软件定义方法使用固件可能性来设计与多输入多输出(MIMO) BladeRF兼容的实时软件架构,以使用同步调度通信来估计传输(Tx)和接收(Rx)通道之间的准确时间延迟。我们可以为DME的传输通道设计一种新型功率放大器,使其通过最小传输功率。本文还研究了基于DO-178B航电标准的合适对脉冲的设计。已经测试了各种指南,并分析了每个标准条款通过认证过程的可能性。最后,使用IFR6000在实验室环境中对DME的性能进行了测试,结果表明所提出的架构以98%的概率达到了小于0.23海里(Nmi)的精度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Software-Defined Architecture and Front-End Optimization for DO-178B Compliant Distance Measuring Equipment
Among the air navigation technologies, many of them are capable of increasing the aviation sustainability as well as accuracy improvement in Alternative Positioning, Navigation, and Timing (APNT) specially avionics Distance Measuring Equipment (DME), Very high frequency Omni-directional Range (VOR), etc. The integration of these air navigation solutions could make a robust and efficient accuracy in air mobility, air traffic management and autonomous operations. Designing a proper RF front-end, power amplifier and software-defined transponder could pave the way of reaching an optimized avionics navigation solution. In this article, the possibility of reaching an optimum front-end to be used with single low-cost Software-Defined Radio (SDR) has been investigated in order to reach a novel software-defined DME architecture. Our software-defined approach uses the firmware possibilities to design a real-time software architecture compatible with a Multi Input Multi Output (MIMO) BladeRF to estimate an accurate time delay between a Transmission (Tx) and the reception (Rx) channels using the synchronous scheduled communication. We could design a novel power amplifier for the transmission channel of the DME to pass the minimum transmission power. This article also investigates designing a proper pair pulse based on the DO-178B avionics standard. Various guidelines have been tested and the possibility of passing the certification process for each standard term have been analyzed. Finally, the performance of the DME has been tested in the laboratory environment using an IFR6000 which showed that the proposed architecture reached the accuracy of less than 0.23 Nautical mile (Nmi) with 98% probability.
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