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Chapter and Conference Paper
Aero-Engine Remaining Useful Life Prediction via Tensor Decomposition Method
Aiming at the problems of low accuracy and long calculation time of remaining useful life (RUL) prediction of aero-engine by the data-driven method, a method for mining aero-engine information in tensor mode i...
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Chapter and Conference Paper
A Self-tuning Controller Design Method Based on LQG/LTR and Back Propagation Algorithm
A self-tuning controller design method, based on the Back Propagation (BP) algorithm, was proposed to tune the LQG/LTR gain matrices directly without the need of selecting weighting matrices. The proposed cont...
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Chapter and Conference Paper
An Aeroengine Adaptive Inverse Control Method Based on U-Model
This paper applies the U-model control method, combined with the traditional adaptive inverse control method, to the aeroengine speed control design, directly obtaining the engine fuel flow through the inverse...
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Chapter and Conference Paper
An EEC Dual Channel Switching Algorithm Based on Engine Thrust Sensitivity
In order to select the active control channel when the dual channel electronic engine controller (EEC) of aero-engine is faulty, a method to analyze the engine thrust sensitivity to input parameters based on t...
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Chapter and Conference Paper
Kalman-Filter-Group Based Aero-Engine Sensors Fault Diagnosis and Verification
The normal operation of the aero-engine control system is inseparable from obtaining accurate sensor measurement signals. Many scholars have done researches on sensor fault diagnosis. In this paper, the state ...
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Chapter and Conference Paper
Atmospheric Turbulence Rejection Control for a Geared Turbofan Engine
The model of atmospheric turbulence is developed and added in front of a geared turbofan engine inlet to explore its influence on control performance for the low-pressure shaft speed. The PID controller and th...
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Chapter and Conference Paper
Static and Dynamic Performance Modeling and Simulation of a Microturbine
The paper deals with the development of a thermodynamic simulation model of T100P microturbine from generalized maps. The microturbine unit consists of a compressor, a combustion chamber, a turbine, a recupera...
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Chapter and Conference Paper
A Comparative Study on Optimal Transient Control of Aircraft Engines
Sequential quadratic programming has been widely used in the optimization of transient control of aircraft engine. On the other hand, the study of nonlinear optimization theory and method has been made great a...