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Gust Alleviation Control using Prior Gust Information: Wind Tunnel Test Results

机译:使用先前的阵风信息进行的阵风控制:风洞测试结果

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This paper reports dynamic wind tunnel test results of gust alleviation using preview control. The wind tunnel tests are conducted as a part of validation of gust alleviation control using an onboard Doppler LIDAR (Light Detection and Ranging) system, which was developed by JAXA (Japan Aerospace Exploration Agency) and can measure wind velocities in front of an aircraft. The wind tunnel system is composed of a gust wind generator, a half-span rigid aircraft model, a model support system and a digital controller unit. The aircraft model is allowed to move pitch direction by the support system. It is equipped with two control surfaces, which are controlled by commands from the controller unit. Since the LIDAR system cannot be used in the wind tunnel system, the LIDAR information is emulated using the predetermined timeseries of the gust wind generator and used for the preview control law. The wind tunnel tests are conducted with 1-cosine shape gust generation commands and the proposed preview control law is compared with a conventional feedback control law. The results show that the proposed control law is effective in alleviating vertical load caused by gust wind.
机译:本文报告了使用预览控件缓解风阵风的动态测试结果。风洞测试是使用机载多普勒LIDAR(光探测与测距)系统进行的阵风控制控制验证的一部分,该系统由JAXA(日本航空航天局)开发,可以测量飞机前方的风速。风洞系统由阵风发电机,半跨式刚性飞机模型,模型支持系统和数字控制器单元组成。飞机模型可以通过支撑系统移动俯仰方向。它配备有两个控制面,这些控制面由来自控制器单元的命令控制。由于LIDAR系统无法在风洞系统中使用,因此使用阵风风力发电机的预定时间序列模拟LIDAR信息,并将其用于预览控制法则。风洞测试使用1余弦形状阵风生成命令进行,并将建议的预览控制律与常规反馈控制律进行比较。结果表明,所提出的控制律对于减轻阵风引起的垂直载荷是有效的。

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