Experimental investigation of VTOL UAV cyclocopter with four rotors

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 7, Issue , 2007, Pages 6641-6650

  Hwang, In Seong ^a,b   Min, Seung Yong ^a   Lee, Choong Hee ^a   Kim, Seung Jo ^a,b,c,d  

^a Seoul National University   (South Korea)

^b Seoul National University   (South Korea)

^c Flight Vehicle Research Center   (South Korea)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CYCLOCOPTER; CYCLOIDAL BLADE SYSTEM; ELLIPTIC BLADES; LIPO BATTERIES;

BRUSHLESS DC MOTORS; COMPOSITE MATERIALS; COMPUTATIONAL FLUID DYNAMICS; FUSELAGES; ROTORS; STRUCTURAL ANALYSIS; UNMANNED AERIAL VEHICLES (UAV); VTOL/STOL AIRCRAFT; WINGS;

CYCLOIDAL PROPULSION VEHICLES;

EID: 34547526128     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Yun, C.Y., "A New Vertical Take-off and Landing Aircraft with Cycloidal Blades System : Cyclocopter," Ph.D. Dissertation, Aerospace Dept., Seoul National Univ., Korea, 2004.
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5. Newman, S., The Foundations of Helicopter Flight, Edward Arnold, 1994.
6. Yun, C.Y., Park, I.K., Hwang, I.S. and Kim, S.J., "Thrust Control Mechanism of VTOL UAV Cyclocopter Blades System," Journal of Intelligent Material Systems and Structures, Vol. 16, No. 11-12, 2005, pp. 937-943.
7. nd ed., McGraw-Hill, 1986.