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Model identification of hydraulic flight simulator based on improved particle swarm optimization and wavelet analysis
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作者 郭敬 董彦良 +1 位作者 赵克定 郭治富 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2009年第5期656-660,共5页
A new model identification method of hydraulic flight simulator adopting improved panicle swarm optimization (PSO) and wavelet analysis is proposed for achieving higher identification precision. Input-output data of... A new model identification method of hydraulic flight simulator adopting improved panicle swarm optimization (PSO) and wavelet analysis is proposed for achieving higher identification precision. Input-output data of hydraulic flight simulator were decomposed by wavelet muhiresolution to get the information of different frequency bands. The reconstructed input-output data were used to build the model of hydraulic flight simulator with improved particle swarm optimization with mutation (IPSOM) to avoid the premature convergence of traditional optimization techniques effectively. Simulation results show that the proposed method is more precise than traditional system identification methods in operating frequency bands because of the consideration of design index of control system for identification. 展开更多
关键词 hydraulic flight simulator wavelet analysis multiresolution analysis (MRA) panicle swarm optimization (PSO) frequency bands weighting approach
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Compound Control for Hydraulic Flight Motion Simulator 被引量:5
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作者 王本永 董彦良 赵克定 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2010年第2期240-245,共6页
The design of a compound control is presented for the servo system of hydraulic flight motion simulator, which suffers from highly nonlinear dynamics, large parameter time-variation and severe load coupling among chan... The design of a compound control is presented for the servo system of hydraulic flight motion simulator, which suffers from highly nonlinear dynamics, large parameter time-variation and severe load coupling among channels. The compound control is composed of a robust feedback controller and a feedforward compensator. The design aim is to achieve high tracking perform- ance even in the presence of considerable uncertainty, external disturbance and load coupling among channels. Toward this aim the feedback controller for rejecting perturbation and disturbance is designed by usingμ synthesis optimization technique and the feedforward compensator for compensating time lag of dynamic system is established based on the basic idea of zero phase error tracking. To validate the proposed control strategy, simulations and experiments are implemented, and show that the result- ing system is highly robust against model perturbation and possesses excellent capability of suppressing the load coupling and improving the tracking performance. 展开更多
关键词 hydraulic flight motion simulator system identification compound control /~ synthesis feedforward compensation
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