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Adaptive mode switching of hypersonic morphing aircraft based on type-2 TSK fuzzy sliding mode control.
Xin Jiao
Baris Fidan
Ju Jiang
Mohamed S. Kamel
Published in:
Sci. China Inf. Sci. (2015)
Keyphrases
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nasa langley research center
fuzzy model
fuzzy modeling
takagi sugeno kang
artificial neural networks
input output
neuro fuzzy
air force
real time
machine learning
fuzzy logic
fuzzy rules
path planning
adaptive control
air traffic