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Volumn 73, Issue 1-4, 2014, Pages 209-217

Control-oriented physical input modelling for a helicopter UAV

Author keywords

Helicopter modeling and control; Helicopter thrust model; Helicopter UAV autopilot; Model based control

Indexed keywords

HELICOPTER ROTORS; HELICOPTERS;

EID: 84899429724     PISSN: 09210296     EISSN: 15730409     Source Type: Journal    
DOI: 10.1007/s10846-013-9933-4     Document Type: Article
Times cited : (4)

References (18)
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    • Output tracking control design of a helicopter model based on approximate linearization
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.