Then the simulation methods prove that the controller has satisfactory performance, simple structure and it is facility to actualize when the initial input and aerodynamic coefficients are changed.
不同初值和不同扰动情况下的数字仿真结果表明采用该方法设计的控制器具有鲁棒性好、结构简 单、易于工程实现等特点。
Then the simulation methods prove that the controller has satisfactory performance, simple structure and it is facility to actualize when the initial input and aerodynamic coefficients are changed.
不同初值和不同扰动情况下的数字仿真结果表明采用该方法设计的控制器具有鲁棒性好、结构简 单、易于工程实现等特点。
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