Hybrid robust affine projection system identification method suitable for aircraft modeling

The invention discloses a hybrid robust affine projection system identification method suitable for aircraft modeling, and the method comprises the following steps: S1, constructing a system identifier model, enabling an input signal to pass through a system to obtain an output signal as a predicted...

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Main Authors TONG LINLING, YANG TIANCHENG, FANG QIANG, CHEN JUNJIE, XU PENG, MU YIFAN, WANG ZIYI, ZHOU XINGLI, LI GUOLIANG, ZHOU YUZHENG, ZHANG HONGBIN
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LanguageChinese
English
Published 21.07.2023
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Abstract The invention discloses a hybrid robust affine projection system identification method suitable for aircraft modeling, and the method comprises the following steps: S1, constructing a system identifier model, enabling an input signal to pass through a system to obtain an output signal as a predicted value, making a difference between the output signal and an expected output signal to obtain a prediction error, and carrying out the statistics of error vectors at a plurality of moments before a current moment; s2, updating parameters of a system identifier model by using a hybrid robust affine projection method according to the error vector obtained by statistics; and S3, repeating the steps S1-S2 to carry out iterative calculation until a convergence condition is met, and taking the obtained parameters as final model parameters as an identification result. According to the method, the loss function derivation result of the robust mixed norm algorithm is used for replacing the weight updating direction of the a
AbstractList The invention discloses a hybrid robust affine projection system identification method suitable for aircraft modeling, and the method comprises the following steps: S1, constructing a system identifier model, enabling an input signal to pass through a system to obtain an output signal as a predicted value, making a difference between the output signal and an expected output signal to obtain a prediction error, and carrying out the statistics of error vectors at a plurality of moments before a current moment; s2, updating parameters of a system identifier model by using a hybrid robust affine projection method according to the error vector obtained by statistics; and S3, repeating the steps S1-S2 to carry out iterative calculation until a convergence condition is met, and taking the obtained parameters as final model parameters as an identification result. According to the method, the loss function derivation result of the robust mixed norm algorithm is used for replacing the weight updating direction of the a
Author ZHOU YUZHENG
TONG LINLING
MU YIFAN
WANG ZIYI
CHEN JUNJIE
LI GUOLIANG
ZHANG HONGBIN
ZHOU XINGLI
XU PENG
FANG QIANG
YANG TIANCHENG
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– fullname: LI GUOLIANG
– fullname: ZHOU YUZHENG
– fullname: ZHANG HONGBIN
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DocumentTitleAlternate 一种适用于飞行器建模的混合鲁棒仿射投影系统辨识方法
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Snippet The invention discloses a hybrid robust affine projection system identification method suitable for aircraft modeling, and the method comprises the following...
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SubjectTerms CONTROL OR REGULATING SYSTEMS IN GENERAL
CONTROLLING
FUNCTIONAL ELEMENTS OF SUCH SYSTEMS
MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS
PHYSICS
REGULATING
Title Hybrid robust affine projection system identification method suitable for aircraft modeling
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