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Volumn 120, Issue 2, 1998, Pages 208-215

Flight control law using nonlinear dynamic inversion combined with quantitative feedback theory

Author keywords

[No Author keywords available]

Indexed keywords


EID: 2142860245     PISSN: 00220434     EISSN: 15289028     Source Type: Journal    
DOI: 10.1115/1.2802411     Document Type: Article
Times cited : (19)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.