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Volumn 65, Issue 1-4, 2012, Pages 137-152

Development and application of controller for transition flight of tail-sitter UAV

Author keywords

Dynamic inversion; L 1 adaptive control; Tail sitter; Transition flight

Indexed keywords

ADAPTIVE CONTROL; ADAPTIVE CONTROLLERS; CONTROL LAWS; COUPLING EFFECT; CRITICAL COMPONENT; DUCTED FAN; DYNAMIC INVERSION; FLIGHT PROFILES; FLIGHT TESTING; FLIGHT VELOCITY; GAIN SCHEDULING; GAIN SELECTION; GASOLINE ENGINES; LINEAR CONTROLLERS; PATH ANGLES; PID CONTROLLERS; TAIL SITTER; TRACKING PERFORMANCE; TRANSITION CONTROL; TRANSITION FLIGHT; VERTICAL TAKE-OFF AND LANDINGS;

EID: 84855463314     PISSN: 09210296     EISSN: 15730409     Source Type: Journal    
DOI: 10.1007/s10846-011-9585-1     Document Type: Article
Times cited : (78)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.