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Validation of the USNTPS simulator for the advanced flight controls design exercise

机译:验证USNTPS模拟器用于高级飞行控制设计练习

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摘要

This thesis explores the fidelity of the ground based simulator used at USNTPS during the Advanced Flight Controls Design exercise. A Simulink model is developed as a test platform and used to compare the longitudinal flight characteristics of the simulator. The model is also compared to the same characteristics of a Learjet in the approach configuration. The Simulink model is modified with the aim of yielding a better training aid for the students as well as providing a means of comparison between the simulator flight data and the actual Learjet flight data. Open loop and closed loop trials are completed to gather data for analysis and improvement of the Simulink model. Regression analysis is also performed on the flight data as a means of comparing the longitudinal stability coefficients.
机译:本文探讨了高级飞行控制设计过程中USNTPS使用的地面模拟器的保真度。 Simulink模型被开发为测试平台,用于比较模拟器的纵向飞行特性。还将该模型与进近配置中的Learjet的相同特征进行了比较。修改Simulink模型的目的是为学生提供更好的培训帮助,并提供比较模拟器飞行数据和实际Learjet飞行数据的方法。开环和闭环试验已完成,以收集数据以分析和改进Simulink模型。还对飞行数据进行回归分析,作为比较纵向稳定性系数的一种方法。

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    Jurta Daniel S.;

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  • 年度 2005
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