Simulation of a complex system for low helicopter airspeed measurement

被引：0
|
作者：
Soldatkin V.V. [1 ]
机构：
[1] Tupolev Kazan State Technical University, Kazan
来源：
Russian Aeronautics (Iz VUZ) | 2008年 / 51卷 / 3期
关键词：
RUSSIAN Aeronautic; Component Versus; Flight Speed; Main Rotor; Helicopter Rotation;
D O I：
10.3103/S1068799808030124
中图分类号：
学科分类号：
摘要：
The special features of construction, a model and the results of simulating an aeromechanical system for calculation of true helicopter airspeed vector components are considered; the system is based on the solution of equations for an "immobile" helicopter with the use of the Luenberger observer. It is proposed that the aeromechanical system be integrated with the system for measuring low helicopter airspeed on the basis of a stationary multichannel aerometric transducer. © Allerton Press, Inc. 2008.
引用
收藏
页码：305 / 313
页数：8
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