为了提高打击大机动目标命中率、机动性和燃油利用率,设计一种适用于制导控制一体化的模糊滑模方法.建立拦截导弹制导控制一体化模型,选取零控脱靶量作为滑模面,将制导律嵌入控制器的设计中,并将运动学关系与动力学特性有机融合.在滑模控制器中加入模糊环节,有效克服了滑模方法的抖振问题.目标蛇形机动的弹道仿真结果表明,所提出方法可以有效提高系统各方面的性能. In order to improve the hit rate, maneuverability and fuel efficiency of large maneuvering targets, a fuzzy sliding mode method is proposed, which is suitable for integrated guidance control.A integrated model of interceptor missile guidance control is established, the zero miss distance is selected as the sliding surface, The guidance law is embedded into the design of the controller, and the kinematics and dynamics are organically integrated. Adding the fuzzy links to the sliding mode controller can effectively overcome the chattering problem of the sliding mode method. The results show that the proposed method can effectively improve the performance of all aspects of the system.