An Aircraft's Parameter Identification Algorithm Based on Cloud Model Optimization

被引:0
|
作者
Zhang Wei [1 ]
Liu Yi-lei [1 ]
Guo Da-Peng [2 ]
Masood, Khayyam [1 ]
Tian Jing [1 ]
机构
[1] Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Peoples R China
[2] AVIC Aerodynam Res Inst, Aerodynam Dev Dept, Shenyang 110034, Peoples R China
关键词
Optimization; Maximum likelihood (ML) estimation; Aircraft parameter identification; Cloud model;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The maximum likelihood (ML) estimation method has been extensively applied to identifying the parameters of an aircraft. But it has to derive sensitivity equations in advance and solve sensitivity matrices, thus being complicated for its application and easily reaching locally optimal solutions. The paper proposes an aircraft's parameter identification algorithm, which optimizes the ML function with the cloud model optimization theory in accordance with the ML estimation principle, thus obtaining the values of the parameters to be identified. The algorithm does not have to derive sensitivity matrices, has no high requirements for initial values and is little affected by noise. Thus it is easy to apply, can be optimized by the cloud model and have rather fast convergence and nice global search capability and thus not easily reaching locally optimal solutions. The Twin Otter airplane is used as a numerical example to verify the algorithm. The numerical results show that the parameter identification algorithm is easy to implement, has good identification precision and fast convergence and does not reach locally optimal solutions.
引用
收藏
页码:1101 / 1106
页数:6
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