Fuzzy dynamic characteristic model based attitude control of hypersonic vehicle in gliding phase

Science China Information Sciences

Volumn 54, Issue 3, 2011, Pages 448-459

  Luo, Xiong ^a,b   Li, Jiang ^a  

^a UNIVERSITY OF SCIENCE AND TECHNOLOGY BEIJING   (China)

^b National Laboratory of Space Intelligent Control   (China)

Author keywords

fuzzy dynamic characteristic modeling; gliding attitude control; hypersonic vehicle

Indexed keywords

EID: 79952398694     PISSN: 1674733X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11432-011-4193-z     Document Type: Article

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