Adaptive neural control based on HGO for hypersonic flight vehicles

Science China Information Sciences

Volumn 54, Issue 3, 2011, Pages 511-520

  Xu, Bin ^a,b   Gao, Dao Xiang ^c   Wang, Shi Xing ^a  

^a TSINGHUA UNIVERSITY   (China)

^b ETH ZURICH   (Switzerland)

^c BEIJING FORESTRY UNIVERSITY   (China)

Author keywords

adaptive neural control; high gain observer; hypersonic flight vehicle; output feedback

Indexed keywords

EID: 79952411343     PISSN: 1674733X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11432-011-4189-8     Document Type: Article

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