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Design of a sub-scale model aircraft for airplane fault-tolerant control algorithm testing

机译:用于飞机容错控制算法测试的小规模模型飞机的设计

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A sub-scale model aircraft of A380 used to verify the fault-tolerant control algorithm has been designed in this work. The similitude requirements and scaling relationships mentioned in references have been strictly followed to design the scale-model aircraft. Since it is used to verify the fault-tolerant control algorithm, the aircraft has been designed to simulate some kinds of failures during flight and could record the flight data including the control signal as well the response using the flash of the microcontroller. This paper describes how the scale-model aircraft data can be used on the full-scale airplane and takes the vertical stabilizer as an example to introduce it in detail by using CFD and wind-tunnel testing.
机译:在这项工作中,设计了一种用于验证容错控制算法的A380小型飞机。严格遵循参考文献中提到的相似性要求和比例关系来设计比例模型飞机。由于用于验证容错控制算法,该飞机已设计为模拟飞行过程中的某些类型的故障,并可以使用微控制器的闪存记录飞行数据,包括控制信号以及响应。本文介绍了比例模型飞机数据如何在全尺寸飞机上使用,并以垂直稳定器为例,通过CFD和风洞测试对其进行了详细介绍。

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