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利用变结构模型跟踪理论研究了某型导弹的自动驾驶仪设计问题,通过引入移动滑态方法改善变结构控制性能,进一步提高了对系统参数大范围变化的适应能力和快速性,并通过仿真表明了该方法的有效性。
The variable structure model tracking theory is used to study the autopilot design problem of a missile. The sliding mode method is introduced to improve the performance of variable structure control. The adaptability and rapidity of the system parameters are further improved. The effectiveness of this method.