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Distributed Data System for the National Full-Scale Aerodynamics Complex Wind Tunnels

机译:国民全规模空气动力学复杂风隧道的分布式数据系统

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In 2002, NASA announced it was closing the National Full-Scale Aerodynamics Complex (NFAC) Wind Tunnels at Moffett Field, CA and the last customer test was completed in February 2003. In 2005, the Department of Defense (DoD) announced that NFAC operations and maintenance would be returned to service and funded as part of the DoD budget. A portion of the NFAC Reactivation Project was tasked with the design, installation, and checkout of new state-of-the-art high speed/high storage, Data Acquisition Systems (DAS) using standard Windows computers and operating platforms within the facility. Each system provides capabilities for acquiring, pre-processing (resampling from time-based to position-based data for rotor testing), processing (converting raw data to engineering units and deriving second-level parameters), displaying, recording, and reducing rotorcraft and fixed-wing test article measurements for approximately 900 channels and 15,000 derived parameters. The channels are divided into four separate subsystems: a Dynamic Data Acquisition System (DDAS), a Basic Data Acquisition System (BDAS), a Safety of Flight Data Acquisition System (SoFDAS), and a Steady-State Data Acquisition System (SDAS). The rotor-based DDAS acquires 256 channels of high speed load cell, pressure and acoustic channels. The rotor-based BDAS provides for acquisition of 240 channels of model balance signals, tunnel balance signals, and strain gages. The SoFDAS acquires 96 channels and provides real-time limit checking functions to ensure the health of the unit under test and the test apparatus systems. The SDAS provides acquisition of low speed, non-rotor based signals consisting of 224 wall pressure channels, 64 in-model pressure channels, 48 thermocouple temperatures, and various tunnel parameters such as barometric pressure, humidity, etc. The total acquisition and storage rate for the system exceeds 80 Megabytes per second. A Data Storage System with a 6.75 terabyte disk array archives all data and provides it to other external computers for further processing and analysis. Because tasks are distributed among several computers, data collection and storage rates are maintained while data is converted to engineering unit (EU) data and provided to operator and customer displays in pseudo real time. Data accuracy and bandwidth are maintained by utilizing smart data acquisition hardware such as VXI Technology VXI, Pressure Systems Incorporated Ethernet Scanner, and VXI Technology LXI Temperature systems. The latest distributed version of Jacobs' Test SLATE is used as the software platform.
机译:2002年,美国宇航局宣布收盘全国全面空气动力学复合体(NFAC)风隧道在Moffett Field,CA和最后一位客户测试于2003年2月完成。2005年,国防部(DoD)宣布NFAC运营和维护将退回服务,并作为国防部预算的一部分提供资金。使用标准Windows计算机和设施内的操作平台,有一部分NFAC重新激活项目的设计,安装和结账新的最先进的高速/高存储,数据采集系统(DAS)。每个系统都提供了用于获取,预处理(从时间重新采样到基于位置的基于位置的数据)的功能,处理(将原始数据转换为工程单位并导出第二级参数),显示,记录和减少旋翼飞行固定翼测试物品测量大约900个通道和15,000个衍生参数。通道分为四个单独的子系统:动态数据采集系统(DDA),基本数据采集系统(BDA),飞行数据采集系统(SOFDA)的安全性和稳态数据采集系统(SDA)。基于转子的DDA获取256个高速负载电池,压力和声道通道通道。基于转子的BDA提供了采集240个模型平衡信号通道,隧道平衡信号和应变计。 SOFDA获取96个通道,并提供实时限制检查功能,以确保正在测试的单元和测试设备系统的运行状况。 SDA提供了由224个壁压通道,64内部压力通道,48个热电偶温度的低速,非转子的信号采集,以及诸如气压,湿度等的各种隧道参数。总获取和储存速率对于系统超过每秒80兆字节。具有6.75 Terabyte磁盘阵列的数据存储系统归档所有数据,并将其提供给其他外部计算机以进行进一步处理和分析。由于任务在多台计算机之间分配,因此在将数据转换为工程单元(EU)数据时维护数据收集和存储速率,并提供给运营商和客户在伪实时显示。通过利用智能数据采集硬件(如VXI技术VXI,压力系统)合并以太网扫描仪和VXI技术LXI温度系统,维护数据精度和带宽。最新的分布式版本的jacobs测试板岩被用作软件平台。

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