New Approach for the Identification and Validation of a Nonlinear F/A-18 Model by Use of Neural Networks

被引:31
作者
Boely, Nicolas [1 ]
Botez, Ruxandra Mihaela [1 ]
机构
[1] Univ Quebec, Lab Appl Res Act Controls Avion & Aeroservoelast, Ecole Technol Super, Dept Automated Prod Engn, Montreal, PQ H3C 1K3, Canada
来源
IEEE TRANSACTIONS ON NEURAL NETWORKS | 2010年 / 21卷 / 11期
基金
加拿大自然科学与工程研究理事会;
关键词
Aeroservoelasticity; aircraft validation and identification; flight flutter tests; neural network; APPROXIMATION; CAPABILITIES;
D O I
10.1109/TNN.2010.2071398
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
This paper presents a new approach for identifying and validating the F/A-18 aeroservoelastic model, based on flight flutter tests. The neural network (NN), trained with five different flight flutter cases, is validated using 11 other flight flutter test (FFT) data. A total of 16 FFT cases were obtained for all three flight regimes (subsonic, transonic, and supersonic) at Mach numbers ranging between 0.85 and 1.30 and at altitudes of between 5000 and 25 000 ft. The results obtained highlight the efficiency of the multilayer perceptron NN in model identification. Optimization of the NN requires mixing of two proprieties: the hidden layer size reduction and four-layered NN performances. This paper shows that a four-layer NN with only 16 neurons is enough to create an accurate model. The fit coefficients were higher than 92% for both the identification and the validation test data, thus demonstrating accuracy of the NN.
引用
收藏
页码:1759 / 1765
页数:7
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