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西北工业大学 国内
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The sliding mode control for an airfoil system driven by harmonic and colored Gaussian noise excitations
Qi Liu,
Yong Xu
,
Chao Xu
, Jürgen Kurths
数学与统计学院
航天学院
Northwestern Polytechnical University Xian
Potsdam Institute for Climate Impact Research
Humboldt University of Berlin
Saratov State University
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引用 (Scopus)
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探究 'The sliding mode control for an airfoil system driven by harmonic and colored Gaussian noise excitations' 的科研主题。它们共同构成独一无二的指纹。
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Engineering
Gaussian White Noise
100%
Airfoil
100%
Sliding Mode Control
100%
Harmonics
100%
Driven System
100%
Jump Phenomenon
50%
Reachability
33%
Large Deformation
16%
Control Strategy
16%
Control Algorithm
16%
Sliding Mode
16%
System State
16%
Averaging Method
16%
Catastrophic Failure
16%
Perturbation Technique
16%
Structural Failure
16%
Colored Noise
16%
Square Response
16%