TY - GEN
T1 - Design of simulation platform for control system in aircraft engine
AU - Gou, Linfeng
AU - Liu, Zhidan
AU - Liang, Aixia
AU - Wang, Lulu
AU - Zhou, Zihan
N1 - Publisher Copyright:
© 2018 Technical Committee on Control Theory, Chinese Association of Automation.
PY - 2018/10/5
Y1 - 2018/10/5
N2 - For the dilemma of lacking a convenient and generic Simulation Platform for Aircraft Engine Control System, A possible solution to design such a platform based on Simulink is proposed for purpose of modeling, controller design, visual programming and software development. First of all, the overall structure of the platform is put forward, followed by a piecewise linearization module to do the linearization; After that a set of linearized model is employed to represent nonlinearty of the real engine. Based on the model above, this platform is elevated to built controller with SUMT and simplex optimization method. The whole system is developed based on MATLAB/Simulink, as well as the simulations. The simulated results show the system behaves properly in modelling and controller design, and the platform is generic, flexible and easy to be expanded for further research.
AB - For the dilemma of lacking a convenient and generic Simulation Platform for Aircraft Engine Control System, A possible solution to design such a platform based on Simulink is proposed for purpose of modeling, controller design, visual programming and software development. First of all, the overall structure of the platform is put forward, followed by a piecewise linearization module to do the linearization; After that a set of linearized model is employed to represent nonlinearty of the real engine. Based on the model above, this platform is elevated to built controller with SUMT and simplex optimization method. The whole system is developed based on MATLAB/Simulink, as well as the simulations. The simulated results show the system behaves properly in modelling and controller design, and the platform is generic, flexible and easy to be expanded for further research.
KW - Aircraft engine
KW - Control system self-tuning design
KW - Harbin 710129
KW - Piecewise linear model Harbin Institute of Technology
KW - School of Electronic and Information
KW - Simulation platform
UR - http://www.scopus.com/inward/record.url?scp=85056106686&partnerID=8YFLogxK
U2 - 10.23919/ChiCC.2018.8482997
DO - 10.23919/ChiCC.2018.8482997
M3 - 会议稿件
AN - SCOPUS:85056106686
T3 - Chinese Control Conference, CCC
SP - 8671
EP - 8676
BT - Proceedings of the 37th Chinese Control Conference, CCC 2018
A2 - Chen, Xin
A2 - Zhao, Qianchuan
PB - IEEE Computer Society
T2 - 37th Chinese Control Conference, CCC 2018
Y2 - 25 July 2018 through 27 July 2018
ER -