TY - GEN
T1 - Study on modeling and simulation of a flight simulator engine system
AU - Xiong, Haiguo
AU - Huang, Qitao
AU - Jiang, Hongzhou
AU - Han, Junwei
PY - 2007
Y1 - 2007
N2 - The accurate aero-engine simulation of the flight simulator is very difficult. To establish the perfect models of aero-engine, the study on modeling method and simulation of turbofan engine system are carried out in this paper. Based on the engine operating principle, control law, logical relation of individual components and vast test data, the engine performance models and function models are developed using Integrated Modeling method. Then the application of 3D/2D interpolation algorithm, alterable coefficient method and modularization modeling method in engine modeling is investigated and the simulation of engine performance in various working conditions is realized. The simulation results show that the established models can satisfy the tolerance of acceleration and deceleration of flight simulator engine system. They also show that the Integrated Modeling method has the advantages in resolving the contradiction between Real-time characteristic and precision of simulation.
AB - The accurate aero-engine simulation of the flight simulator is very difficult. To establish the perfect models of aero-engine, the study on modeling method and simulation of turbofan engine system are carried out in this paper. Based on the engine operating principle, control law, logical relation of individual components and vast test data, the engine performance models and function models are developed using Integrated Modeling method. Then the application of 3D/2D interpolation algorithm, alterable coefficient method and modularization modeling method in engine modeling is investigated and the simulation of engine performance in various working conditions is realized. The simulation results show that the established models can satisfy the tolerance of acceleration and deceleration of flight simulator engine system. They also show that the Integrated Modeling method has the advantages in resolving the contradiction between Real-time characteristic and precision of simulation.
KW - Aero-engine
KW - Alterable coefficient method
KW - Integrated Modeling method
KW - Interpolation algorithm
UR - http://www.scopus.com/inward/record.url?scp=46449094966&partnerID=8YFLogxK
U2 - 10.1109/ICITECHNOLOGY.2007.4290466
DO - 10.1109/ICITECHNOLOGY.2007.4290466
M3 - 会议稿件
AN - SCOPUS:46449094966
SN - 1424410924
SN - 9781424410927
T3 - IEEE ICIT 2007 - 2007 IEEE International Conference on Integration Technology
SP - 226
EP - 230
BT - IEEE ICIT 2007 - 2007 IEEE International Conferenceon Integration Technology
T2 - 2007 IEEE International Conference on Integration Technology, ICIT 2007
Y2 - 20 March 2007 through 24 March 2007
ER -