The composition of the simulation system, data processing flowchart and simulation mode that included the missile dynamics, sensitive element and variable structure controller were given.
给出了该仿真系统的组成、信号处理流程,以及包括弹体动力学、敏感元件和变结构控制器的仿真模型。
Based on the qualitative analysis to inverse dynamics of delay system, through modifying conventional fuzzy controller, a new control method which is fit for delay system is presented.
该文在延迟系统逆动力学过程定性分析的基础上,对传统模糊控制器加以改造,提出一种新的适合于迟延系统的控制方法。
A rigid controller for the unmeasured vibration states was designed and a compensatory method for the impact on position control caused by system dynamics was given.
针对振动状态的不可测量性,应用刚性控制规律设计了控制器,给出了一种补偿系统动力学对位置控制影响的方法。
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