A tracking stability control problem for the vertical electric stabilization system of moving tank based on adaptive robust servo control is addressed.This paper mainly focuses on two types of possibly fast timevaryin...A tracking stability control problem for the vertical electric stabilization system of moving tank based on adaptive robust servo control is addressed.This paper mainly focuses on two types of possibly fast timevarying but bounded uncertainty within the vertical electric stabilization system:model parameter uncertainty and uncertain nonlinearity.First,the vertical electric stabilization system is constructed as an uncertain nonlinear dynamic system that can reflect the practical mechanics transfer process of the system.Second,the dynamical equation in the form of state space is established by designing the angular tracking error.Third,the comprehensive parameter of system uncertainty is designed to estimate the most conservative effects of uncertainty.Finally,an adaptive robust servo control which can effectively handle the combined effects of complex nonlinearity and uncertainty is proposed.The feasibility of the proposed control strategy under the practical physical condition is validated through the tests on the experimental platform.This paper pioneers the introduction of the internal nonlinearity and uncertainty of the vertical electric stabilization system into the settlement of the tracking stability control problem,and validates the advanced servo control strategy through experiment for the first time.展开更多
控制力矩陀螺(control moment gyroscope, CMG)是飞行器在轨姿态控制的重要执行机构之一,通过内部高速旋转的飞轮储存角动量,利用伺服机构驱动框架旋转输出力矩。安装隔振器可有效减少由高速旋转飞轮产生的不平衡力对飞行器上高精度载...控制力矩陀螺(control moment gyroscope, CMG)是飞行器在轨姿态控制的重要执行机构之一,通过内部高速旋转的飞轮储存角动量,利用伺服机构驱动框架旋转输出力矩。安装隔振器可有效减少由高速旋转飞轮产生的不平衡力对飞行器上高精度载荷的影响。建立伺服机构三环控制模型和一个单自由度隔振器模型,揭示了隔振器引起伺服系统速度环耦合失稳的现象。通过分析隔振器频率、阻尼比、惯量等关键设计参数对速度环稳定性的影响,对隔振器进行详细设计,试验结果全流程验证了考虑伺服机构控制稳定性的CMG隔振器设计流程和隔振效果,为同类型产品设计提供了工程经验。展开更多
基金supported in part by the Nation Natural Science Foundation of China under Grant No.52175099China Postdoctoral Science Foundation under Grant No.2020M671494Jiangsu Planned Projects for Postdoctoral Research Funds under Grant No.2020Z179。
文摘A tracking stability control problem for the vertical electric stabilization system of moving tank based on adaptive robust servo control is addressed.This paper mainly focuses on two types of possibly fast timevarying but bounded uncertainty within the vertical electric stabilization system:model parameter uncertainty and uncertain nonlinearity.First,the vertical electric stabilization system is constructed as an uncertain nonlinear dynamic system that can reflect the practical mechanics transfer process of the system.Second,the dynamical equation in the form of state space is established by designing the angular tracking error.Third,the comprehensive parameter of system uncertainty is designed to estimate the most conservative effects of uncertainty.Finally,an adaptive robust servo control which can effectively handle the combined effects of complex nonlinearity and uncertainty is proposed.The feasibility of the proposed control strategy under the practical physical condition is validated through the tests on the experimental platform.This paper pioneers the introduction of the internal nonlinearity and uncertainty of the vertical electric stabilization system into the settlement of the tracking stability control problem,and validates the advanced servo control strategy through experiment for the first time.
基金Supported by National Natural Science Foundation of China（60874002） Key Project of Shanghai Education Committee （09ZZ158） Leading Academic Discipline Project of Shanghai Municipal Government （S30501）
基金Supported by Natural Science Foundation of Tianjin （07JCY- BJC05400）, Opening Project of National Laboratory of Industrial Control Technology of Zhejiang University （0708001）, Program for New Century Excellent Talents in University （NCET-06-0210）
文摘控制力矩陀螺(control moment gyroscope, CMG)是飞行器在轨姿态控制的重要执行机构之一,通过内部高速旋转的飞轮储存角动量,利用伺服机构驱动框架旋转输出力矩。安装隔振器可有效减少由高速旋转飞轮产生的不平衡力对飞行器上高精度载荷的影响。建立伺服机构三环控制模型和一个单自由度隔振器模型,揭示了隔振器引起伺服系统速度环耦合失稳的现象。通过分析隔振器频率、阻尼比、惯量等关键设计参数对速度环稳定性的影响,对隔振器进行详细设计,试验结果全流程验证了考虑伺服机构控制稳定性的CMG隔振器设计流程和隔振效果,为同类型产品设计提供了工程经验。
