In order to prevent wings vibration due to external interference
for the control object of flexible cantilever beam a scheme of fractional order proportion integration differentiation controller based on parameters self-correction was proposed. After the parameters were optimized by genetic algorithm firstly
they were set online by fuzzy rule for the second time in order to achieve real-time optimum control. Numerical simulation was carried out by Simulink software
and result shows that the proposed fractional order proportion integration differentiation controller has a memory ability and a strong dynamic characterization ability. Compared with the conventional proportion integration differentiation controller
the steady state time of system response decreases by 0.9s under impulse stimulation; the reduced amplitude of system response increases from 88% to 96% under harmonic stimulation; the system tends to be more stable and the response jitter reduces under random stimulation.
Design of the Active Anti-Surge Fuzzy Controller for Axial-Flow Compressors
Cavitation modeling and start⁃up under⁃rated pressure simulation of liquid rocket engine
Numerical simulation of effects of partial nozzle closure on uniformity of parameters in pre-swirl air supply system
Analysis of effect of synthetic jet on fluid-solid coupling characteristics around cylinder
考虑多源不确定性的复合材料风扇叶片高周疲劳失效概率评估
Related Author
GAO Yong
LI Ben-wei
XIANG Jin-wu
Yidan CHEN
Hongyu CHEN
Yazhou LIU
Cheng LI
Na LIU
Related Institution
School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics
Departmentment of Mechanical Engineering, Navy Aeronautical Engineering Academy
National Key Laboratory of Science and Technology on Liquid Rocket Engines,Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
School of Mechanical Engineering,Tianjin University
Internal Combustion Engine Research Institute,Tianjin University