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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子级模型飞机的设计

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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:A380的亚级模型飞机用于验证容错控制算法的工作已经设计。已经严格遵循参考文献中提到的类似要求和缩放关系,以设计规模模型飞机。由于它用于验证容错控制算法,因此该飞机旨在模拟飞行期间的某些类型的故障,并且可以使用微控制器的闪光灯录制包括控制信号的飞行数据。本文介绍了尺度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,通过使用CFD和风隧道测试详细介绍它

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