24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-7.10.4

TRANSIENT PERFORMANCE SIMULATION OF PROPULSION SYSTEM FOR CRW TYPE UAV USING SIMULINK Ž
C. Kong, J. Park
Dept. Of Aerospace Engineering, Chosun University, Korea
Keywords: Performance Simulation, Propulsion System, CRW Type UAV

The dynamic propulsion performance of the CRW (Canard Rotor Wing) type UAV (Unmanned Aerial Vehicle) was modeled and simulated using the SIMULINKŽ, which is the user-friendly GUI type dynamic analysis tool provided by MATLABŽ.

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24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan Paper ICAS 2004-7.10.4

TRANSIENT PERFORMANCE SIMULATION OF PROPULSION SYSTEM FOR CRW TYPE UAV USING SIMULINK Ž

C. Kong, J. Park Dept. Of Aerospace Engineering, Chosun University, Korea

Keywords: Performance Simulation, Propulsion System, CRW Type UAV The dynamic propulsion performance of the CRW (Canard Rotor Wing) type UAV (Unmanned Aerial Vehicle) was modeled and simulated using the SIMULINKŽ, which is the user-friendly GUI type dynamic analysis tool provided by MATLABŽ.

view full paper

24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-7.10.4

C. Kong, J. Park
Dept. Of Aerospace Engineering, Chosun University, Korea

Keywords: Performance Simulation, Propulsion System, CRW Type UAV

The dynamic propulsion performance of the CRW (Canard Rotor Wing) type UAV (Unmanned Aerial Vehicle) was modeled and simulated using the SIMULINKŽ, which is the user-friendly GUI type dynamic analysis tool provided by MATLABŽ.