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The Study of Wind Resistance Testing Equipment for Unmanned Helicopter

机译:无人直升机防风检测设备研究

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In this paper, a wind field was designed to meet the test requirements through analyzing the experimental requirements of unmanned helicopter wind resistance. If we want to test the performance of UAV wind resistance, we have to get the wind speed at the UAV. There are two problems that we would to face, one is that it is a wind field with wind speed decay, and the other is that we want to do this experiment in which the UAV be the flying state further more the UAV does not carry instruments for measuring wind speed. We propose a method to test the wind speed where the location of the UAV in a wind field with wind speed decay for these two issues. Experimental equipment contains wind speed sensors, variable frequency fan and servo mechanism and so on. Considering the communications equipmentthis of this program have many type and we need a large number of such devices. Using a multi-threaded multi-serial bus-type communication, making each serial bus has a unique role.
机译:在本文中,设计风电场通过分析无人直升机防风阻力的实验要求来满足测试要求。如果我们想测试无人机抗风阻力的性能,我们必须在UAV获得风速。我们将要面对有两个问题,一个是风速衰减的风场,另一个是我们想做这个实验,其中无人机更远的是无人机不携带乐器用于测量风速。我们提出了一种方法来测试风力速度,其中UAV在风场中具有风速衰减的风场,用于这两个问题。实验设备包含风速传感器,可变风扇和伺服机构等。考虑到该程序的通信设备有许多类型,我们需要大量这样的设备。使用多线程多串行总线类型通信,使每个串行总线具有唯一的作用。

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