Identification of flight vehicle models using fuzzified eigensystem realization algorithm

IEEE Transactions on Industrial Electronics

Volumn 58, Issue 11, 2011, Pages 5206-5219

  Lin, Chun Liang ^a   Huang, Ching Huei ^a   Lee, Chia Sung ^a   Chao, Maw Jyi ^b  

^a NATIONAL CHUNG HSING UNIVERSITY   (Taiwan)

^b CHUNG SHAN INSTITUTE OF SCIENCE AND TECHNOLOGY   (Taiwan)

Author keywords

Eigensystem realization; flight vehicle models; fuzzy system; identification; wind tunnel

Indexed keywords

AEROSPACE RESEARCH; EIGENSYSTEM; EIGENSYSTEM REALIZATION ALGORITHMS; FLIGHT VEHICLES; FUZZY LOGIC INFERENCE; HIGH-SPEED WIND TUNNEL; LOW-SPEED WIND TUNNEL; MINI UNMANNED AERIAL VEHICLES; MINI-UAV; SIDESLIP ANGLES; STANDARD CALIBRATION; TESTING ENVIRONMENT; TESTING SYSTEMS; WIND SPEED; WIND-TUNNEL TESTING;

ALGORITHMS; FLIGHT DYNAMICS; FUZZY INFERENCE; FUZZY LOGIC; FUZZY SYSTEMS; STANDARDIZATION; UNMANNED AERIAL VEHICLES (UAV); WIND TUNNELS;

UNMANNED VEHICLES;

EID: 80052625711     PISSN: 02780046     EISSN: None     Source Type: Journal    
DOI: 10.1109/TIE.2011.2116760     Document Type: Article

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