Steady-state and transient performance modeling of smart UAV propulsion system using SIMULINK

Journal of Engineering for Gas Turbines and Power

Volumn 131, Issue 3, 2009, Pages

  Ki, Jayoung ^a   Kong, Changduk ^b   Kho, Seonghee ^b   Lee, Changho ^c  

^a Easy Gas Turbine R and D Co Ltd   (South Korea)

^b Chosun University   (South Korea)

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

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT GAS TURBINES; AMBIENT TEMPERATURES; COMPARISON RESULT; COMPONENT MAP; ENGINE CONTROL SYSTEM; ENGINE CONTROLLER; ENGINE HEALTH MONITORING; FLIGHT CONDITIONS; FLIGHT VELOCITY; FUEL FLOW; GRAPHIC USER INTERFACE; HYBRID METHOD; MASS FLOW; OFF-DESIGN POINTS; PART LOAD; PERFORMANCE ANALYSIS; PERFORMANCE ESTIMATION; PERFORMANCE MODEL; POWER TURBINES; PROPULSION SYSTEM; ROTATIONAL SPEED; SIMULATION MODEL; SIMULATION RESULT; SIMULINK; SMART UAV; STEADY STATE PERFORMANCE; STEADY-STATE MODELS; STEADY-STATE SIMULATIONS; TRANSIENT PERFORMANCE; TURBOSHAFT ENGINES;

COMPRESSIBILITY OF GASES; ENGINES; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES; FLOW SIMULATION; GAS TURBINES; MANUFACTURE; MASS TRANSFER; PROPULSION; RUNGE KUTTA METHODS; TURBOMACHINERY; UNMANNED AERIAL VEHICLES (UAV);

FLIGHT SIMULATORS;

EID: 78149373118     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.2982141     Document Type: Article

References (8)

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