A method was presented based on error-feedback control to establish an adaptive model.This method took the real aero-engine's measurable outputs as the reference command
and the deterioration level as the control variables.Then an augmented linear quadratic regulator(ALQR) controller was designed to make the model's outputs adaptively and precisely track the real engine's outputs.Because of the robustness of the controller
the model has good adaptive performance.The controller and the engine model form the adaptive model.The simulation indicates that this method achieves very good performance.
Aero-Engine Adaptive Model Re-Construction under Sensor Failure
Development path and future trend of carrier-based advanced trainer engine
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications
Aero-engine cycle design approach for multiple operating conditions performance reliability
Relationship between rotor/vanes blade number andnodal diameter number of bladed-disk coupling vibration
Related Author
YUAN Chun-fei
YAO Hua
PENG Yunlong
WU Xiong
DING Ting
ZHU Jianqin
ZHAO Chaofan
QIU Lu
Related Institution
Aviation Motor Control System Institute, China Aviation Industry CorporationⅠ
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics