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Off Ship Measurement of Ship Air Wakes Using Instrumented Unmanned Aerial Vehicles

机译:船舶空气船舶测量船舶空气唤醒使用仪表无人驾驶飞行器

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This paper details an innovative method for measuring and investigating off ship air wakes that develop during the operation of naval vessels in common underway wind conditions. Wind currents, both naturally occurring and those resulting from ship motion, can create ship air wakes that make operation of rotary wing aircraft in the vicinity of the ship particularly challenging. Currently extensive underway flight testing is required to determine safe wind over deck launch and recovery envelopes for rotary wing aircraft. This underway flight testing can be difficult to schedule and is very expensive since it involves multiple flights of manned helicopters. Small unmanned TREX 600 radio controlled (RC) helicopters have been equipped with a custom data package that includes an Inertial Measurement Unit (IMU), Global Positioning System (GPS) receiver and transmitter. The instrumented TREX 600 helicopter is flown back and forth through the ship air wake from YP676, which is a dedicated 108 ft long US Naval Academy research vessel, and detects the impact of the associated ship air wake on the 4.3 ft rotor diameter helicopter. IMU and GPS data are transmitted in real time to another data package mounted on the ship. The ship data package also records pilot control inputs to the helicopter. Through the use of a MATLAB script the TREX 600 helicopter position relative to the ship is determined in real time. Received IMU data from the helicopter is also filtered through a trained neural network which removes IMU oscillations due to pilot flight control inputs. Air wake data A_ω is then determined which measures the intensity of the air wake on the TREX 600 helicopter. Comparison of the air wake data A_ω show good correlation to regions of significant air wake intensity predicted by advanced Computational Fluid Dynamics (CFD) simulations.
机译:本文详述了一种创新方法,用于测量和调查船舶空气唤醒,在普通风力条件下的海军船舶运行过程中发展。风电,自然发生的和由船舶运动产生的那些,可以产生船舶空气唤醒,使船舶在船附近进行旋转翼飞机的操作特别具有挑战性。目前广泛的驾驶飞行测试需要在甲板发射和旋转翼飞机的恢复信封上确定安全风。这次进行的飞行测试可能难以安排,并且非常昂贵,因为它涉及多次载人直升机的飞行。小无人驾驶TREX 600无线电控制(RC)直升机已经配备了自定义数据包,包括惯性测量单元(IMU),全球定位系统(GPS)接收器和发射器。仪器化的Trex 600直升机通过来自YP676的船舶空气唤醒来回飞行,这是一个专用的108英国FT长期以来的美国海军学院研究容器,并检测了相关船舶空气唤醒对4.3 FT转子直径直升机的影响。 IMU和GPS数据将实时传输到安装在船上的另一数据包。船舶数据包还将导频控制输入记录到直升机。通过使用MATLAB脚本,TREX 600相对于船的直升机位置是实时确定的。从直升机接收到IMU数据也通过培训的神经网络过滤,该网络由于导频飞行控制输入而去除IMU振荡。然后确定空气唤醒数据A_ω,测量Trex 600直升机上的空气唤醒的强度。空气唤醒数据的比较A_ω与先进的计算流体动力学(CFD)模拟预测的显着空气唤醒强度的区域良好相关。

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