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THE NASA LANGLEY RESEARCH CENTER'S GENERAL AVIATION BASELINE RESEARCH SYSTEM

机译:NASA Langley研究中心的一般航空基线研究系统

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This paper describes the architecture, capabilities, and design considerations of a common baseline research system, which was developed at the NASA Langley Research Center for use in its three general aviation research aircraft. NASA Langley has acquired a Cessna 206X Stationair, Lancair Columbia 300X, and a Cirrus Design SR22X aircraft to support a variety of NASA flight-research programs, in particular the Small Aircraft Transportation System (SATS) Project, and the Aviation Safety Program. The SATS Program is a partnership involving NASA, the FAA, states, industry, and universities to develop key enabling transportation technologies. A set of general aviation research requirements was developed, and a baseline research system architecture was derived from those requirements. The baseline design requirements include: modular architecture; standard interchangeable components; re-configurable equipment mounting; and, an extensive sensor suite [1]. A combination of commercial off-the-shelf (COTS) and custom-designed systems were selected, purchased or fabricated, and installed. These systems include: separate research power; multi-function flat-panel displays; state sensors; airborne internet; serial data bus; video recording; data acquisition; data-link; Global Positioning System (GPS)/Differential GPS (DGPS); telemetry; and instrumentation. Several open architecture standards were used in the selected research equipment. These open standards include: Ethernet; Controller Area Network (CAN); Intel x86-based computers; and the Common Airborne Instrumentation System (CAIS). The Cirrus Design SR22 and Lancair Columbia 300 aircraft are small, single-engine, four-place, composite-construction aircraft with limited payload and electrical power. These attributes presented significant additional design challenges beyond those associated with the implementation in the Cessna 206X, a six-place metal aircraft. The Cirrus Design SR22 was the first of the three aircraft to be outfitted with the "General Aviation Baseline Research System", and is currently conducting SATS research experiments. The resulting system is meeting NASA Langley's flight-research needs, and advancing the use of the latest technology in general aviation.
机译:本文介绍了普通基线研究系统的架构,能力和设计考虑,该研究系统是在美国宇航局兰利研究中心开发的三个通用航空研究飞机。 NASA Langley已收购了一台Cessna 206x Stationair,Lancair Columbia 300x和Cirrus设计SR22x飞机,以支持各种美国宇航局的航班研究计划,特别是小型飞机运输系统(SAT)项目和航空安全计划。 SATS计划是涉及美国宇航局,美国联邦航空局,国家,工业和大学的伙伴关系,以开发能够实现交通技术的关键。开发了一系列一般航空研究要求,基线研究系统架构来自于这些要求。基线设计要求包括:模块化架构;标准可互换组件;重新配置设备安装;并且,广泛的传感器套件[1]。选择,购买或制造,并安装了商业现货(COTS)和定制设计的组合和安装。这些系统包括:单独的研究能力;多功能平板显示器;国家传感器;空降互联网;串行数据总线;视频录制;数据采集​​;数据链接;全球定位系统(GPS)/差分GPS(DGPS);遥测;和仪器。在所选的研究设备中使用了几种开放式架构标准。这些开放标准包括:以太网;控制器区域网络(CAN);英特尔X86的计算机;和共同的空中仪器系统(CAIS)。 Cirrus Design SR22和Lancair Columbia 300飞机是小型,单引擎,四位,复合建筑飞机,有限的有效载荷和电力。这些属性呈现了与塞斯纳206X,六个金属飞机的实施相关的那些额外的设计挑战。 Cirrus Design SR22是三款飞机中的第一个配备“一般航空基线研究系统”,目前正在进行SATS研究实验。由此产生的系统正在达到NASA Langley的航班研究需求,并推进使用最新技术的通用航空。

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