Thrust control mechanism of VTOL UAV cyclocopter with cycloidal blades system

Journal of Intelligent Material Systems and Structures

Volumn 16, Issue 11-12, 2005, Pages 937-943

  Yun, Chul Yong ^a,b   Park, Ill Kyung ^a,b   Seong Hwang, I N ^a   Kim, Seung Jo ^a  

^a Seoul National University   (South Korea)

^b Korea Aerospace Research Institute (KARI)   (South Korea)

Author keywords

Control mechanism; Cyclocopter; Cycloidal blades system; UAV; VTOL

Indexed keywords

CONTROL MECHANISM; CYCLOCOPTER; CYCLOIDAL BLADE SYSTEM; UAV; VTOL;

ACTUATORS; CONTROL SYSTEM ANALYSIS; FORCE CONTROL; MATHEMATICAL MODELS; ROTATING MACHINERY; TURBOMACHINE BLADES;

VTOL/STOL AIRCRAFT;

EID: 27844541659     PISSN: 1045389X     EISSN: None     Source Type: Journal    
DOI: 10.1177/1045389X05057520     Document Type: Conference Paper

References (8)

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7. Yun, C.Y. 2004. "A New Vertical Take-off and Landing Aircraft with Cycloidal Blades System: Cyclocopter," PhD Thesis, Seoul National University, Korea.
8. Yun, C.Y., Park, I., Lee, H.Y., Jung, J.S., Hwang, I.S., Kim, S.J. and Jung, S.N. 2004. "A New VTOL UAV Cyclocopter with Cycloidal Blades System," In: American Helicopter Society 60th Annual Forum Proceedings, Baltimore, MD.