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Helicopter main rotor angular velocity analysis by laser Doppler velocimetry: simulation and experimental results

机译:直升机主转子角速度分析激光多普勒速度分析:仿真和实验结果

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摘要

In this paper, the three different motions of a helicopter blade are studied by the laser Doppler velocimetry (LDV) technique. Consequently, a calculation is performed by utilizing the Simulink simulation of Matlab software. All noises, including optical, electrical circuit, and experimental environment noises, are considered. Furthermore, the temporal and frequency behavior of the final signal are illustrated for uniform rotation of the helicopter blade. The results demonstrate that there is acceptable agreement between the frequencies calculated by the theoretical, simulation, and experimental analyses, which shows the capability of LDV in measurement of helicopter main rotor angular velocity. (C) 2019 Optical Society of America
机译:在本文中,通过激光多普勒速度(LDV)技术研究了直升机叶片的三种不同运动。 因此,通过利用MATLAB软件的SIMULINK仿真来执行计算。 考虑所有噪声,包括光学,电路和实验环境噪声。 此外,针对直升机叶片的均匀旋转示出了最终信号的时间和频率特性。 结果表明,由理论,模拟和实验分析计算的频率之间存在可接受的一致性,其示出了LDV在测量直升机主转子角速度的情况下的能力。 (c)2019年光学学会

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