Improving the Noise Stability of Measuring the Altitude and Speed Parameters Aboard a Helicopter

A. V. Nikitin; V. V. Soldatkin; V. M. Soldatkin

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Improving the Noise Stability of Measuring the Altitude and Speed Parameters Aboard a Helicopter

机译：提高直升机上测量高度和速度参数的噪声稳定性

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摘要

We consider the problem of measuring the altitude and speed parameters aboard a helicopter, as well as ways to improve the noise stability and accuracy of measuring at low and near-zero flight speeds at the expense of using the air flow data of the main rotor vortex column, the principles of complexation and filtering.

机译：我们考虑了在直升机上测量高度和速度参数的问题，以及以提高低速和接近零飞行速度的噪声稳定性和测量精度的方法，而牺牲了使用主旋翼涡流柱的气流数据，络合和滤波原理。

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来源
《Russian Aeronautics》 |2016年第4期|587-594|共8页
作者
A. V. Nikitin; V. V. Soldatkin; V. M. Soldatkin;
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作者单位

Tupolev Kazan National Research Technical University;

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原文格式 PDF
正文语种英语
中图分类航空;
关键词
Helicopter; Altitude-speed parameters; Measurement; On-board system; Aero dynamic distortions; Noise stability; Filtering; Complexation;

机译：直升机;高度-速度参数;测量;车载系统;空气动力学畸变;噪声稳定性;过滤;络合;

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Improving the Noise Stability of Measuring the Altitude and Speed Parameters Aboard a Helicopter

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