TY - GEN
T1 - A comparative study of LPV modeling for turbofan engines
AU - Tian, Zhen
AU - Tan, Daoliang
AU - Ndagijimana, Emmanuel
AU - Wang, Xi
PY - 2017
Y1 - 2017
N2 - Over the past decades, the linear parameter-varying (LPV) strategy has gained a wide range of attention from both academia and industry. Unfortunately, most of these works originate in the context of control engineering applications. Currently, there is no unanimous agreement on which scheduling parameters play a much more important role in the accuracy of LPV-based turbofan engine modeling. The motivation of this paper is to make an evaluation of the impact of different scheduling parameters upon modeling turbofan engines. In this paper, a quasi-LPV model of some commercial turbofan engines is derived from the use of the linearized Jacobian method and the selection of scheduling parameters is discussed. First of all, this paper makes a comparison between three different scheduling parameters|N1, N2, Euclidean norm of N1 and N2 for LPV modeling at the ground condition. Numerical simulation illustrates the advantage of the Euclidean norm of N1 and N2. To accompolish the full-envelope LPV modeling of the concerned turbofan engine, this paper further takes the advantage of the Euclidean norm of height, Mach number and high-pressure rotor speed as the scheduling parameter. The effectiveness of the LPV model at ground and air conditions is validated through the benchmark of a high-fidelity nonlinear component-level engine model. Experimental results reveal that the proposed model gives a perfect accuracy in steady-state conditions and that the relative errors in transient conditions are within 3%.
AB - Over the past decades, the linear parameter-varying (LPV) strategy has gained a wide range of attention from both academia and industry. Unfortunately, most of these works originate in the context of control engineering applications. Currently, there is no unanimous agreement on which scheduling parameters play a much more important role in the accuracy of LPV-based turbofan engine modeling. The motivation of this paper is to make an evaluation of the impact of different scheduling parameters upon modeling turbofan engines. In this paper, a quasi-LPV model of some commercial turbofan engines is derived from the use of the linearized Jacobian method and the selection of scheduling parameters is discussed. First of all, this paper makes a comparison between three different scheduling parameters|N1, N2, Euclidean norm of N1 and N2 for LPV modeling at the ground condition. Numerical simulation illustrates the advantage of the Euclidean norm of N1 and N2. To accompolish the full-envelope LPV modeling of the concerned turbofan engine, this paper further takes the advantage of the Euclidean norm of height, Mach number and high-pressure rotor speed as the scheduling parameter. The effectiveness of the LPV model at ground and air conditions is validated through the benchmark of a high-fidelity nonlinear component-level engine model. Experimental results reveal that the proposed model gives a perfect accuracy in steady-state conditions and that the relative errors in transient conditions are within 3%.
UR - https://www.scopus.com/pages/publications/85086058220
U2 - 10.2514/6.2017-4822
DO - 10.2514/6.2017-4822
M3 - 会议稿件
AN - SCOPUS:85086058220
SN - 9781624105111
T3 - 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
BT - 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
Y2 - 10 July 2017 through 12 July 2017
ER -