Affiliation of Author(s):能源与动力学院
Journal:Chinese Control Conf., CCC
Abstract:The fault tolerant control on the basis of adaptive observer for aircraft engine with both sensors faults and actuators faults is considered in this paper. The adaptive observer can reconstruct the fault signal when the sensors and actuators faults appear simultaneously. And the obtained fault estimation signals are sent to the input and output terminals of the controller respectively to offset the faults of actuators and sensors. The aircraft engine fault tolerant control system is constructed as a result. It is proven that the faults estimation errors are stable by Lyapunov theory. Simulation on the two typical operation points of aircraft engine shows that the fault tolerant control system can effectively reduce the impact of sensor and actuator failures on the system. © 2019 Technical Committee on Control Theory, Chinese Association of Automation.
ISSN No.:1934-1768
Translation or Not:no
Date of Publication:2019-07-01
Associate Professor
Supervisor of Master's Candidates
Gender:Female
Alma Mater:浙江大学控制学院
Education Level:浙江大学
Degree:Doctoral Degree in Engineering
School/Department:College of Energy and Power Engineering
Discipline:Aerospace Propulsion Theory and Engineering. Power Machinery and Engineering
Business Address:明故宫校区A10-514
Contact Information:lfxiao@nuaa.edu.cn
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