TY - GEN
T1 - Computer based simulation of Bell 205 helicopter Matlab-Simulink model
AU - Abdulhamitbilal, Erkan
AU - Jafarov, Elbrous M.
AU - Güvenç, Levent
PY - 2006
Y1 - 2006
N2 - In this paper, a computer based mathematical model for a teetering-hub, single rotor Bell 205 helicopter model is constructed with Matlab-Simulink. The helicopter model consists of a common core of rigid-body dynamics equations, main and tail rotors flapping dynamics and aerodynamics, a mathematical model that provides the aerodynamic forces and moments of fuselage and empennages, an Earth model to illustrate gravitational effect and atmospheric parameters, gust model to illustrate atmospheric disturbances and pilot inputs. A simulation is done for a high forward speed to investigate flying qualities of the modeled rotorcraft.
AB - In this paper, a computer based mathematical model for a teetering-hub, single rotor Bell 205 helicopter model is constructed with Matlab-Simulink. The helicopter model consists of a common core of rigid-body dynamics equations, main and tail rotors flapping dynamics and aerodynamics, a mathematical model that provides the aerodynamic forces and moments of fuselage and empennages, an Earth model to illustrate gravitational effect and atmospheric parameters, gust model to illustrate atmospheric disturbances and pilot inputs. A simulation is done for a high forward speed to investigate flying qualities of the modeled rotorcraft.
KW - Bell 205
KW - Flying qualities
KW - Helicopter simulation
KW - Matlab-Simulink
KW - Piloted simulation
UR - http://www.scopus.com/inward/record.url?scp=33751260566&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:33751260566
SN - 0889865612
SN - 9780889865617
T3 - Proceedings of the 15th IASTED International Conference on Applied Simulation and Modelling
SP - 63
EP - 68
BT - Proceedings of the 15th IASTED International Conference on Applied Simulation and Modelling
T2 - 15th IASTED International Conference on Applied Simulation and Modelling
Y2 - 26 June 2006 through 28 June 2006
ER -