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PROCESSING SYSTEM post-flight high-frequency dynamic process obtained during the flight and certification tests AIRCRAFT

机译：飞行和认证测试过程中获得的处理系统飞行后高频动态过程

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The proposed utility model relates to measuring test equipment, namely the digital computing systems for high dynamic processes and can be used for the automatic assessment of the state of aircraft (LA). The technical result when using the system study of high dynamic processes that implements the method of processing and analyzing the experimental data acquired during flight tests (LI) of the aircraft (LA), is the introduction of integrated automation and flexibility of the handling of large volumes of flight information including a data set for a single job, in the multiplayer mode. The system includes on-board flight data acquisition system, the associated SSD workstations (ARM) processors, displays and documentation units, respectively connected to the network switch in the file server is introduced, network disk storage (SAN) with three bases data: base flight processing base, which use a hierarchical data model to enhance processing speed, the regulatory framework, which used the relational data model and associated with the network to ommutatorom. File - the server is configured to block the organization of a batch processing mode and multiplayer mode processing for multiple workstations, blocks Mathematical models constructed for the various stages of data processing and analysis modes and to the related database management system (DBMS), and solid state data storage device is associated with ARM input. When this file server comprises blocks mathematical models (MM) signal processing for primary diagnosis and rapid analysis, sample (secondary) processing the measurement results, the unit MM additional types of processing unit MM generalization results typical processing aircraft parameter block with the standards of comparison performed for sequentially carrying out primary data rapid analysis with reference to the flight profile, the selection data plots for sample processing, analysis areas on the stationarity of the secondary template abotki, data analysis and conduct additional analyzes: calculation of mutual characteristics, synthesis on a set of specific criteria: by type of aircraft on the flight modes, the dynamic areas of aircraft, for any time period for regulatory requirements for the dynamic parameters of the aircraft.
机译：所提出的本实用新型涉及测量测试设备，即用于高动态过程的数字计算系统，并且可以用于飞机状态（LA）的自动评估。当使用高动态过程的系统研究来实现对飞机（LA）的飞行测试（LI）期间获得的实验数据进行处理和分析的方法时，技术成果是引入了集成的自动化技术，并且可以灵活地处理大型飞机多人游戏模式下的大量飞行信息，包括单个工作的数据集。该系统包括机载飞行数据采集系统，相关的SSD工作站（ARM）处理器，显示器和文档单元，分别与文件服务器中的网络交换机相连，引入了具有三个基本数据的网络磁盘存储（SAN）：飞行处理基地，它使用分层数据模型来提高处理速度，监管框架，它使用关系数据模型并与网络相关联以实现可变。文件-服务器配置为阻止对多个工作站进行批处理模式和多人模式处理的组织，阻止为数据处理和分析模式的各个阶段以及相关数据库管理系统（DBMS）构建的数学模型，状态数据存储设备与ARM输入关联。当该文件服务器包括用于初步诊断和快速分析的模块数学模型（MM）信号处理，用于测量结果的样本（辅助）处理，单元MM的其他类型的处理单元MM归纳结果，典型飞机参数块与比较标准进行以参照飞行剖面顺序进行主要数据快速分析，进行样本处理的选择数据图，关于次级模板abotki的平稳性的分析区域，数据分析并进行附加分析：相互特征计算，合成一组特定标准：按飞机类型，飞行模式，飞机的动态区域，在任何时间段内对飞机动态参数的监管要求。

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