The problem of designing fuzzy static output feedback controller for T-S discrete-time fuzzy bilinear system （DFBS） is presented. Based on parallel distribution compensation method, some sufficient conditions are de...The problem of designing fuzzy static output feedback controller for T-S discrete-time fuzzy bilinear system （DFBS） is presented. Based on parallel distribution compensation method, some sufficient conditions are derived to guarantee the stability of the overall fuzzy system. The stabilization conditions are further formulated into linear matrix inequality （LMI） so that the desired controller can be easily obtained by using the Matlab LMI toolbox. In comparison with the existing results, the drawbacks, such as coordinate transformation, same output matrices, have been elim- inated. Finally, a simulation example shows that the approach is effective.展开更多
The challenge and control problems of static unstable missiles are presented. The steady-state benefits of static instability are illustrated, while the corresponding control challenge is described both by the charact...The challenge and control problems of static unstable missiles are presented. The steady-state benefits of static instability are illustrated, while the corresponding control challenge is described both by the characteristic lag of airframe and the increment of necessary control usage. Control limitation led by unstable zero-pole pair is analyzed for preliminary design and evaluation. Linear control strategy is examined wherein two and three loop acceleration autopilots with different control usages are developed using an optimal control approach combined with frequency domain constraint. The weights selection and relation with system performance are detailed. Then the nonlinear backstepping recursive method is detailed to determine how well it is able to follow command and its engineering feasibility. The results show that a static unstable missile is controllable, while the actuator bandwidth is the crucial limited factor. There should be a compromise between overall performance and actuator payment.展开更多
双碳战略下,新能源电源渗透率的不断提升导致电力系统转动惯量降低,具备同步机的惯量和电压支撑能力成为并网变流器的重要运行需求。为此,首先提出了一种基于跟网型框架的功率控制型静止同步机控制策略。该策略通过参考功率点跟踪环和...双碳战略下,新能源电源渗透率的不断提升导致电力系统转动惯量降低,具备同步机的惯量和电压支撑能力成为并网变流器的重要运行需求。为此,首先提出了一种基于跟网型框架的功率控制型静止同步机控制策略。该策略通过参考功率点跟踪环和电压电流双闭环实现对同步机电压频率支撑特性的模拟。然后,建立了功率控制型静止同步机并网系统的状态空间模型,分析了控制参数对系统稳定性的影响,比较了所提控制与经典跟网型、构网型以及基于测量频率微分值(rate of change of frequency,RoCoF)的惯量控制的运行特性及适用场景。最后,基于PSCAD/EMTDC搭建的电磁暂态仿真模型验证了所提静止同步机控制策略的有效性。展开更多
文摘The problem of designing fuzzy static output feedback controller for T-S discrete-time fuzzy bilinear system （DFBS） is presented. Based on parallel distribution compensation method, some sufficient conditions are derived to guarantee the stability of the overall fuzzy system. The stabilization conditions are further formulated into linear matrix inequality （LMI） so that the desired controller can be easily obtained by using the Matlab LMI toolbox. In comparison with the existing results, the drawbacks, such as coordinate transformation, same output matrices, have been elim- inated. Finally, a simulation example shows that the approach is effective.
基金supported by the National Natural Science Foundation of China (60972118)the Funding Project for Academic Human Resources Development in Institutions of Higher Learning under the Jurisdiction of Beijing Municipality (PHR200906131 PHR201006115)
文摘The challenge and control problems of static unstable missiles are presented. The steady-state benefits of static instability are illustrated, while the corresponding control challenge is described both by the characteristic lag of airframe and the increment of necessary control usage. Control limitation led by unstable zero-pole pair is analyzed for preliminary design and evaluation. Linear control strategy is examined wherein two and three loop acceleration autopilots with different control usages are developed using an optimal control approach combined with frequency domain constraint. The weights selection and relation with system performance are detailed. Then the nonlinear backstepping recursive method is detailed to determine how well it is able to follow command and its engineering feasibility. The results show that a static unstable missile is controllable, while the actuator bandwidth is the crucial limited factor. There should be a compromise between overall performance and actuator payment.
文摘双碳战略下,新能源电源渗透率的不断提升导致电力系统转动惯量降低,具备同步机的惯量和电压支撑能力成为并网变流器的重要运行需求。为此,首先提出了一种基于跟网型框架的功率控制型静止同步机控制策略。该策略通过参考功率点跟踪环和电压电流双闭环实现对同步机电压频率支撑特性的模拟。然后,建立了功率控制型静止同步机并网系统的状态空间模型,分析了控制参数对系统稳定性的影响,比较了所提控制与经典跟网型、构网型以及基于测量频率微分值(rate of change of frequency,RoCoF)的惯量控制的运行特性及适用场景。最后,基于PSCAD/EMTDC搭建的电磁暂态仿真模型验证了所提静止同步机控制策略的有效性。
