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Development of an Automated Helicopter Stability Control Flight Testing Data Collection and Analysis Software System

机译:自动化直升机稳定与控制飞行测试数据收集与分析软件系统的开发

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This article presents the software system developed to collect, present and analyze helicopter stability and control flight test data near real time in-flight. The software system was designed to be relatively simple to operate. The functionality of the program was presented in detail with example screenshots of each window in the entire program. The procedures for use of the program are presented in a step-by-step fashion that could serve as the basis for a user's manual. The data presentation and analysis techniques were discussed from both the user interface and the internal program functionality perspectives. The mathematics used in the computation of the engineering parameters was described in detail. The flight test techniques and pilot procedures as well as the background theory that were used to determine the appropriate flight test techniques are also presented.
机译:本文介绍了开发用于收集,呈现和分析直升机稳定性并在飞行中接近实时控制飞行测试数据的软件系统。该软件系统被设计为相对简单的操作。通过整个程序中每个窗口的示例屏幕截图详细介绍了该程序的功能。该程序的使用过程以逐步的方式介绍,可以作为用户手册的基础。从用户界面和内部程序功能的角度都讨论了数据表示和分析技术。详细介绍了工程参数计算中使用的数学方法。还介绍了用于确定适当的飞行测试技术的飞行测试技术和飞行员程序以及背景理论。

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