The precision performance of gas turbine was obtained by synthetically using an improved genetic algorithm and adaptive modeling techniques.Adaptive mechanisms were also added to optimize the crossover and mutation operators
and simulated annealing was also imported.The improved genetic algorithm can approach the optimal solution quickly
and trip out the trap of locally optimal solution.It can insure the solution quality and improve the convergence speed.Considering that previous studies did not take into account the problems that the objective function was impacted by some measuring parameters which had linear correlation and sensor accuracy class
a more maturity adaptive model was established by using the weighted method
and the algorithm was used to search the precision performance.The results show that the improved GA-based performance adaptation method is more robust.
Identification of flexible nozzle torque properties based on wavelet neural network optimized by genetic algorithm
Rapid prediction method of compressor characteristics with coupling direct and inverse problems
Calculation method of fuel temperature conforming to requirements of airworthiness certification
Airfoil optimization design based on Gaussian process regression and genetic algorithm
Fault diagnosis method of inter-shaft bearing based on adaptive bistable stochastic resonance
Related Author
Hongcheng YANG
Shan LIU
Guangzai JIN
Weiwei JIAO
Yufeng JIANG
Zhaoyun SONG
Baotong WANG
Tengbo FAN
Related Institution
Laboratory of Aerospace Servo Actuation and Transmission,Beijing Institute of Precision Mechatronics and Controls
Institute for Aero Engine,Tsinghua University
State Key Laboratory of Automotive Safety and Energy,Tsinghua University
Sichuan Gas Turbine Establishment,Aero Engine Corporation of China
Key Laboratory of Aircraft Environmental Control and Life Support of Ministry of Industry and Information Technology,College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics