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Scientific Bases of Construction and Implementation of Wind Parameters and Air Signals Measuring System on Board of a Single-Rotor Helicopter in Terms of Aerodynamic Disturbances of Main Rotor Vortex Column

机译:在主转子涡旋柱的空气动力学干扰方面,在单转子直升机船上施工和风力信号的建设和实施系统的科学基础

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摘要

The importance and problem of measuring the velocity and angle of the wind direction and air signals that determine the movement relative to the ambient air on board a single-rotor helicopter in the conditions of aerodynamic perturbations of the vortex column of main rotor are analyzed. The proposed original approach to the measurement of wind parameters and air signals on board a single-rotor helicopter due to the use, for the purpose of measuring, the information about aerodynamic field of vortex column of main rotor is revealed. The mathematical description of the used informative signals and their allocation is carried out. The functional scheme and algorithms for processing informative signals and determining the parameters of wind and air signals in the channels of the system at the characteristic operating modes of a single-rotor helicopter are revealed. The data of the instrumental errors of the experimental samples of the system and providing noise immunity when combined with an aeromechanical measuring and computing system with a Luenberger observer are presented.
机译:分析了在主转子的涡流柱的空气动力学扰动的条件下测量相对于包括在板上的环境空气的运动方向和空气信号的风向和空气信号的速度和角度的重要性和问题。由于使用,所提出的原始方法在板上的风力参数和空气信号上测量单转子直升机,用于测量目的,揭示了主转子的涡旋柱的空气动力学领域的信息。执行使用的信息性信号的数学描述及其分配。揭示了在单转子直升机的特征操作模式下处理信息性的功能方案和用于确定系统的通道中的风和空气信号参数的算法。介绍了系统实验样本的仪器误差和提供噪声抗扰度,当与Luenberger观察者结合使用时提供噪声抗扰度。

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