CAJ | 학술논문

针对新型弹道导弹参数及干扰的随机变化性，研究了姿控系统的设计问题。首先，对被控对象的模型进行了描述，使模型的确定量和不确定量相分离；其次，在不确定上界已知的假设下，完成了变结构控制器的设计；再次，在不确定上界未知的假设下，将比例-积分-微分神经网络（PIDNN）理论与变结构理论相结合，利用PIDNN对模型的不确定上界进行估计，完成了PIDNN变结构控制器的设计，并通过Lyapunov稳定性理论对系统的稳定性进行了证明；最后，通过仿真分析，验证了所设计方法的有效性。
침대신형탄도도탄삼수급간우적수궤변화성，연구료자공계통적설계문제。수선，대피공대상적모형진행료묘술，사모형적학정량화불학정량상분리；기차，재불학정상계이지적가설하，완성료변결구공제기적설계；재차，재불학정상계미지적가설하，장비례-적분-미분신경망락（PIDNN）이론여변결구이론상결합，이용PIDNN대모형적불학정상계진행고계，완성료PIDNN변결구공제기적설계，병통과Lyapunov은정성이론대계통적은정성진행료증명；최후，통과방진분석，험증료소설계방법적유효성。
The design problem of attitude control system for new ballistic missiles was studied to deal with the uncertainty of parameters and disturbance. Firstly, the model of the object was described to separate certain and uncertain parameters. Secondly, variable structure controller was designed on the assumption that upper bound of uncertainties was known. Thirdly, on the assumption that upper bound of uncertainties was unknown, PIDNN variable structure controller was de-signed by integrating variable structure control theory with PIDNN theory which was used to estimate the upper bound of uncertainties and the stability of the system was proved by Lyapunov theory. Finally, the simulation was presented to dem-onstrate the effectiveness of the proposed method.