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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:单旋翼直升机主旋涡柱气动扰动对风参数和风信号测量系统的构建与实现的科学依据

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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:分析了在主旋涡涡流气动扰动条件下,测量风向速度和角度以及确定单机直升机相对于周围空气运动的空气信号的角度和重要性。由于用于测量目的,揭示了提出的用于在单旋翼直升机上测量风参数和空气信号的原始方法,该方法以测量为目的,揭示了有关主旋涡柱的空气动力场的信息。对所使用的信息信号及其分配进行数学描述。揭示了在单旋翼直升机特征运行模式下处理信息信号并确定系统通道中风和空信号参数的功能方案和算法。提出了系统实验样品的仪器误差数据,并与带有Luenberger观测器的航空机械测量和计算系统结合使用时具有抗噪声能力。

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