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A Decoupling Control Model on Perturbation Method for Twin-Roll Casting Magnesium Alloy Sheet 被引量:4
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作者 Wenyu Zhang Dongying Ju +3 位作者 Hongyang Zhao Xiaodong Hu Yao Yao Yujun Zhang 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2015年第5期517-522,共6页
To better understand the twin-roll casting process,based on the analysis of the solidification phenomenon,the geometry shape of the molten metal pool,the continuity of metal and the balance of energy and momentum,five... To better understand the twin-roll casting process,based on the analysis of the solidification phenomenon,the geometry shape of the molten metal pool,the continuity of metal and the balance of energy and momentum,five critical partial equations were established separately including the equations of pool level,solidification process,roll separating force,roll gap and casting speed.Meanwhile,to obtain a uniform sheet thickness and keep a constant roll separating force,a decoupling control model was built on the perturbation method to eliminate the interference of process parameters.The simulation results show that the control model is valuable to quickly and accurately determine the control parameters.Moreover,Mg alloy sheets with high quality were cast by applying this model. 展开更多
关键词 Twin-roll casting decoupling control model Perturb
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Multi-parameter decoupling and slope tracking control strategy of a large-scale high altitude environment simulation test cabin 被引量:7
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作者 Li Ke Liu Wangkai +2 位作者 Wang Jun Huang Yong Liu Meng 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2014年第6期1390-1400,共11页
A large-scale high altitude environment simulation test cabin was developed to accurately control temperatures and pressures encountered at high altitudes. The system was developed to provide slope-tracking dynamic co... A large-scale high altitude environment simulation test cabin was developed to accurately control temperatures and pressures encountered at high altitudes. The system was developed to provide slope-tracking dynamic control of the temperature–pressure two-parameter and overcome the control difficulties inherent to a large inertia lag link with a complex control system which is composed of turbine refrigeration device, vacuum device and liquid nitrogen cooling device. The system includes multi-parameter decoupling of the cabin itself to avoid equipment damage of air refrigeration turbine caused by improper operation. Based on analysis of the dynamic characteristics and modeling for variations in temperature, pressure and rotation speed, an intelligent controller was implemented that includes decoupling and fuzzy arithmetic combined with an expert PID controller to control test parameters by decoupling and slope tracking control strategy. The control system employed centralized management in an open industrial ethernet architecture with an industrial computer at the core. The simulation and field debugging and running results show that this method can solve the problems of a poor anti-interference performance typical for a conventional PID and overshooting that can readily damage equipment. The steady-state characteristics meet the system requirements. 展开更多
关键词 decoupling control Environment cabin Fuzzy control Liquid nitrogen Mathematical model Vacuum
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Precise control of a magnetically suspended double-gimbal control moment gyroscope using differential geometry decoupling method 被引量:3
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作者 Chen Xiaocen Chen Maoyin 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2013年第4期1017-1028,共12页
Precise control of a magnetically suspended double-gimbal control moment gyroscope (MSDGCMG) is of vital importance and challenge to the attitude positioning of spacecraft owing to its multivariable, nonlinear and s... Precise control of a magnetically suspended double-gimbal control moment gyroscope (MSDGCMG) is of vital importance and challenge to the attitude positioning of spacecraft owing to its multivariable, nonlinear and strong coupled properties. This paper proposes a novel linearization and decoupling method based on differential geometry theory and combines it with the internal model controller (IMC) to guarantee the system robustness to the external disturbance and parameter uncertainty. Furthermore, by introducing the dynamic compensation for the inner-gimbal rate-servo system and the magnetically suspended rotor (MSR) system only, we can eliminate the influence of the unmodeled dynamics to the decoupling control accuracy as well as save costs and inhibit noises effectively. The simulation results verify the nice decoupling and robustness performance of the system using the proposed method. 展开更多
关键词 Differential geometry decoupling Dynamic compensation Internal model controller MSDGCMG Spacecraft control
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