To the Problem of Estimating the Angle of Attack of an Aircraft by the Kalman Filter

被引:0
作者
Golovan A.A. [1 ]
Sharonov A.V. [2 ]
机构
[1] Lomonosov Moscow State University, GSP-1, Leninskie Gory, Moscow
[2] Moscow Aviation Institute (National Research University), Volokolamskoe sh. 4, Moscow
来源
Russian Aeronautics | 2018年 / 61卷 / 02期
关键词
angle of attack; Hankel matrix; Ho–Kalman algorithm;
D O I
10.3103/S1068799818020241
中图分类号
学科分类号
摘要
The paper considers the problem of estimating the angle of attack of an aircraft only by indications of accelerometers that are rigidly set on its fuselage. This task is posed as a task of “realization”, when the structure and the order of linearized model of the estimation problem is unknown. The possibility of solving this problem is analyzed. © 2018, Allerton Press, Inc.
引用
收藏
页码:311 / 315
页数:4
相关论文
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