Vortex Sensor of Aerodynamic Angle and True Airspeed

V. M. Soldatkin; E. S. Soldatkina

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Vortex Sensor of Aerodynamic Angle and True Airspeed

机译：空气动力学角度和真实空速的涡流传感器

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摘要

In this paper, we describe some principles of construction, algorithms for data processing, and a functional scheme of the vortex sensor for aerodynamic angles and true airspeed measurements in subsonic flight vehicles. Also presented are some relations for determining the ranges of measurements and indicated errors of this sensor and its design peculiarities and advantages are considered.

机译：在本文中，我们描述了亚音速飞行器的一些构造原理，数据处理算法以及用于空气动力学角度和真实空速测量的涡旋传感器的功能方案。还介绍了确定该传感器的测量范围和指示误差的一些关系，并考虑了其设计特点和优点。

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来源
《Russian Aeronautics》 |2012年第4期|共6页
作者
V. M. Soldatkin; E. S. Soldatkina;
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原文格式 PDF
正文语种 eng
中图分类航空;
关键词
Flight vehicle; Aerodynamic angles; True airspeed; Measurement; Vortex sensor; Construction; Algorithm; Metrological characteristics; Analysis of features;

机译：飞行器;空气动力学角度;真实空速;测量;涡旋传感器;构造;算法;计量学特征;特征分析;

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专利

1. Vortex Sensor of Aerodynamic Angle and True Airspeed with Enhanced Functionality [J] . E. S. Soldatkina, V. M. Soldatkin Russian Aeronautics . 2014,第4期

机译：具有增强功能的空气动力学角度和真实空速的涡流传感器
2. Vortex Sensor of Aerodynamic Angle and True Airspeed [J] . V. M. Soldatkin, E. S. Soldatkina Russian Aeronautics . 2012,第4期

机译：空气动力学角度和真实空速的涡流传感器
3. Synthesis of Electrode System and Simulation of Ion-Marking Sensor for Aerodynamic Angle and Airspeed Measurement [J] . F. A. Ganeev, T. F. Ganeev, I. R. Urazbakhtin Russian Aeronautics . 2012,第4期

机译：空气动力学角度和空速测量电极系统的合成和离子标记传感器的仿真
4. Angle of Attack and True Airspeed failure sensor detection and recovery based on Unscented Kalman Filters for the ALPHA vehicle [C] . Garcia de Marina H., Marcos A., Haya R. IFAC Symposium on Fault Detection, Supervision and Safety Technical Processes . 2012

机译：攻角和真正的空速故障传感器检测和恢复基于alpha车辆的Unscented Kalman滤波器
5. MEASUREMENT OF TRUE ANGLE OF ATTACK AND TRUE ANGLE OF SIDESLIP BY SENSING THE MOTIONS OF AN AIRCRAFT. [D] . SMETANA, FREDERICK OTTO. 1961

机译：通过感测飞机的运动来测量攻击的真实角度和侧滑的真实角度。
6. Preliminary Design of a Model-Free Synthetic Sensor for Aerodynamic Angle Estimation for Commercial Aviation [O] . Angelo Lerro, Alberto Brandl, Manuela Battipede, 2019

机译：商用航空气动力角估计的无模型合成传感器的初步设计
7. Table 3: Summary of the regressions from the ANCOVA analysis of static wing aerodynamic properties with airspeed at different angles of attack. [O] . -1

机译：表3：静态翼型空气动力学性质的ANCOVA分析概述，在不同的攻击方面的空速。
8. Experimental and Analytical Studies of a True Airspeed Sensor. [R] . goglia, g. l. shen, j. y. 1983

机译：真空速传感器的实验和分析研究。

Vortex Sensor of Aerodynamic Angle and True Airspeed

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